Unformatted text preview: Solution Manual
to accompany Introduction to Electric Circuits, 6e
By R. C. Dorf and J. A. Svoboda 1 Table of Contents
Chapter 1 Electric Circuit Variables Chapter 2 Circuit Elements Chapter 3 Resistive Circuits Chapter 4 Methods of Analysis of Resistive Circuits Chapter 5 Circuit Theorems Chapter 6 The Operational Amplifier Chapter 7 Energy Storage Elements Chapter 8 The Complete Response of RL and RC Circuits Chapter 9 The Complete Response of Circuits with Two Energy Storage Elements Chapter 10 Sinusoidal SteadyState Analysis Chapter 11 AC SteadyState Power Chapter 12 ThreePhase Circuits Chapter 13 Frequency Response Chapter 14 The Laplace Transform Chapter 15 Fourier Series and Fourier Transform Chapter 16 Filter Circuits Chapter 17 TwoPort and ThreePort Networks 2 Errata for Introduction to Electric Circuits, 6th Edition Errata for Introduction to Electric Circuits, 6th Edition
Page 18, voltage reference direction should be + on the right in part B: Page 28, caption for Figure 2.31: "current" instead of "cuurent" Page 41, line 2: "voltage or current" instead of "voltage or circuit" Page 41, Figure 2.81 b: the short circuit is drawn as an open circuit. Page 42, line 11: "Each dependent source ..." instead of "Each dependent sources..." Page 164, Table 5.51: method 2, part c, one should insert the phrase "Zero all independent sources, then" between the "(c)" and "Connect a 1A source. . ." The edited phrase will read: "Zero all independent sources, then connect a 1A source from terminal b to terminal a. Determine Vab. Then Rt = Vab/1." Page 340, Problem P8.35: The answer should be Page 340, Problem P8.36: The answer should be . . Page 341, Problem P.8.41: The answer should be Page 546, line 4: The angle is instead of . Page 554, Problem 12.4.1 Missing parenthesis: Page 687, Equation 15.52: Partial t in exponent:
http://www.clarkson.edu/~svoboda/errata/6th.html (1 of 2)5/10/2004 7:41:43 PM Errata for Introduction to Electric Circuits, 6th Edition Page 757, Problem 16.57: Hb(s) = V2(s) / V1(s) and Hc(s) = V2(s) / Vs(s) instead of Hb(s) = V1(s) / V2 (s) and Hc(s) = V1(s) / Vs(s). http://www.clarkson.edu/~svoboda/errata/6th.html (2 of 2)5/10/2004 7:41:43 PM Chapter 1 Electric Circuit Variables
Exercises
Ex. 1.31 i (t ) = 8 t 2  4 t A q(t ) = Ex. 1.33 t 0 i d + q(0) = t 0 t 8 8 (8 2  4 ) d + 0 = 3 2 2 = t 3  2 t 2 C 0 3 3 q ( t ) = i ( ) d + q ( 0 ) = 4sin 3 d + 0 = 
0 0 t t 4 4 4 t cos 3 0 =  cos 3 t + C 3 3 3 Ex. 1.34 dq ( t ) i (t ) = dt 0 i (t ) = 2 2( t  2 ) 2e t <0 0< t < 2 t >2 Ex. 1.41 i1 = 45 A = 45 106 A < i2 = 0.03 mA = .03 103 A = 3 105 A < i3 = 25 104 A
Ex. 1.42 q = i t = ( 4000 A )( 0.001 s ) = 4 C Ex. 1.43 i= q 45 109 = = 9 106 = 9 A 3 t 5 10 Ex. 1.44
electron C 19 i = 10 billion 1.602 10 electron = s C 9 electron 19 1010 1.602 10 electron s electron C = 1010 1.602 1019 electron s C = 1.602 109 = 1.602 nA s 11 Ex. 1.61 (a) The element voltage and current do not adhere to the passive convention in Figures 1.61B and 1.61C so the product of the element voltage and current is the power supplied by these elements. (b) The element voltage and current adhere to the passive convention in Figures 1.61A and 1.61D so the product of the element voltage and current is the power delivered to, or absorbed by these elements. (c) The element voltage and current do not adhere to the passive convention in Figure 1.61B, so the product of the element voltage and current is the power delivered by this element: (2 V)(6 A) = 12 W. The power received by the element is the negative of the power delivered by the element, 12 W. (d) The element voltage and current do not adhere to the passive convention in Figure 1.61B, so the product of the element voltage and current is the power supplied by this element: (2 V)(6 A) = 12 W. (e) The element voltage and current adhere to the passive convention in Figure 1.61D, so the product of the element voltage and current is the power delivered to this element: (2 V)(6 A) = 12 W. The power supplied by the element is the negative of the power delivered to the element, 12 W. Problems
Section 13 Electric Circuits and Current Flow P1.31 i (t ) =
P1.32 d 4 1  e 5t = 20 e 5t A dt ( ) t t t t 4 4 q ( t ) = i ( ) d + q ( 0 ) = 4 1  e 5 d + 0 = 4 d  4 e5 d = 4 t + e5t  C 0 0 0 0 5 5 ( ) P1.33
q ( t ) = i ( ) d = 0 d = 0 C for t 2 so q(2) = 0. q ( t ) = i ( ) d + q ( 2 ) = 2 d = 2 2 = 2 t  4 C for 2 t 4. In particular, q(4) = 4 C.
t  t 2 t  t t t q ( t ) = i ( ) d + q ( 4 ) = 1 d + 4 =  4 + 4 = 8  t C for 4 t 8. In particular, q(8) = 0 C.
t 2 t q ( t ) = i ( ) d + q ( 8 ) = 0 d + 0 = 0 C for 8 t .
8 8 4 t 4 t 12 P1.34 i = 600 A = 600 C s C s mg Silver deposited = 600 20 min60 = 8.05105 mg=805 g 1.118 s min C Section 16 Power and Energy P1.61 a.) q = b.) P = v i = (110 V )(10 A ) = 1100 W c.) Cost =
P1.62 i dt = it = (10 A )( 2 hrs )( 3600s/hr ) = 7.210
0.06$ 1.1kW 2 hrs = 0.132 $ kWhr 4 C P = ( 6 V )(10 mA ) = 0.06 W t = 200 Ws w = = 3.33103 s 0.06 W P P1.63 for 0 t 10 s: v = 30 V and i = 30 t = 2t A P = 30(2t ) = 60t W 15 for 10 t 15 s: v ( t ) =  25 t + b v (10 ) = 30 V b = 80 V 5 v(t ) = 5t + 80 and i (t ) = 2t A P = ( 2t )( 5t +80 ) = 10t 2 +160t W for 15 t 25 s: v = 5 V and i (t ) =  i (25) = 0 P = ( 5 )( 3t + 75 ) = 15t + 375 W 30 t +b A 10 b = 75 i (t ) = 3t + 75 A 13 Energy = P dt = = 30t 2
10 0 10 0 60t dt + 10 (160t 10t 2 ) dt + 15 ( 37515t ) dt
15 25 15 25 + 80t 2  10 t 3 + 375t  15 t 2 = 5833.3 J 3 10 2 15 P1.64 a.) Assuming no more energy is delivered to the battery after 5 hours (battery is fully charged). 5( 3600 ) t 5 ( 3600 ) 0.5 0.5 2 2 11 + w = Pdt = 0 vi d = 0 d = 22 t + 3600 3600 0
= 441 103 J = 441 kJ b.) Cost = 441kJ 1 hr 10 = 1.23 3600s kWhr P1.65 p (t ) = 1 1 ( cos 3 t )( sin 3 t ) = sin 6 t 3 6 1 p ( 0.5 ) = sin 3 = 0.0235 W 6 1 p (1) = sin 6 = 0.0466 W 6 14 Here is a MATLAB program to plot p(t):
clear t0=0; tf=2; dt=0.02; t=t0:dt:tf; v=4*cos(3*t); i=(1/12)*sin(3*t); for k=1:length(t) p(k)=v(k)*i(k); end plot(t,p) xlabel('time, s'); ylabel('power, W') % % % % initial time final time time increment time % device voltage % device current % power P1.66 p ( t ) = 16 ( sin 3 t )( sin 3 t ) = 8 ( cos 0  cos 6 t ) = 8  8cos 6 t W Here is a MATLAB program to plot p(t):
clear t0=0; tf=2; dt=0.02; t=t0:dt:tf; v=8*sin(3*t); i=2*sin(3*t); for k=1:length(t) p(k)=v(k)*i(k); end plot(t,p) xlabel('time, s'); ylabel('power, W') % % % % initial time final time time increment time % device voltage % device current % power 15 P1.67 p ( t ) = 4 1  e 2 t 2 e 2 t = 8 1  e2 t e 2t ( ) ( ) Here is a MATLAB program to plot p(t):
clear t0=0; tf=2; dt=0.02; t=t0:dt:tf; v=4*(1exp(2*t)); i=2*exp(2*t); for k=1:length(t) p(k)=v(k)*i(k); end plot(t,p) xlabel('time, s'); ylabel('power, W') P1.68 % % % % initial time final time time increment time % device voltage % device current % power P = V I =3 0.2=0.6 W w = P t = 0.6 5 60=180 J 16 Verification Problems
VP 11 Notice that the element voltage and current of each branch adhere to the passive convention. The sum of the powers absorbed by each branch are: (2 V)(2 A)+(5 V)(2 A)+(3 V)(3 A)+(4 V)(5 A)+(1 V)(5 A) = 4 W + 10 W + 9 W 20 W + 5 W =0W The element voltages and currents satisfy conservation of energy and may be correct.
VP 12 Notice that the element voltage and current of some branches do not adhere to the passive convention. The sum of the powers absorbed by each branch are: (3 V)(3 A)+(3 V)(2 A)+ (3 V)(2 A)+(4 V)(3 A)+(3 V)(3 A)+(4 V)(3 A) = 9 W + 6 W + 6 W + 12 W + 9 W 12 W 0W The element voltages and currents do not satisfy conservation of energy and cannot be correct. Design Problems
DP 11 The voltage may be as large as 20(1.25) = 25 V and the current may be as large as (0.008)(1.25) = 0.01 A. The element needs to be able to absorb (25 V)(0.01 A) = 0.25 W continuously. A Grade B element is adequate, but without margin for error. Specify a Grade B device if you trust the estimates of the maximum voltage and current and a Grade A device otherwise. 17 DP12 p ( t ) = 20 1  e 8 t 0.03 e 8 t = 0.6 1  e8t e8t Here is a MATLAB program to plot p(t):
clear t0=0; tf=1; dt=0.02; t=t0:dt:tf; v=20*(1exp(8*t)); i=.030*exp(8*t); for k=1:length(t) p(k)=v(k)*i(k); end plot(t,p) xlabel('time, s'); ylabel('power, W') % % % % initial time final time time increment time ( ) ( ) % device voltage % device current % power Here is the plot: The circuit element must be able to absorb 0.15 W. 18 Chapter 2  Circuit Elements
Exercises
Ex. 2.31 m ( i1 + i 2 ) = mi1 + mi 2 superposition is satisfied m ( a i1 ) = a ( mi1 ) homogeneity is satisfied Therefore the element is linear. Ex. 2.32 m ( i1 + i 2 ) + b = mi1 + mi 2 + b ( mi1 + b ) + ( mi 2 + b ) superposition is not satisfied Therefore the element is not linear. Ex. 2.51
v 2 (10 ) P= = =1 W R 100
2 Ex. 2.52 P= Ex. 2.81 v 2 (10 cos t ) 2 = = 10 cos 2 t W R 10 ic =  1.2 A, v d = 24 A V id = 4 (  1.2) =  4.8 id and vd adhere to the passive convention so P = vd id = (24) (4.8) = 115.2 is the power received by the dependent source W 21 Ex. 2.82 vc = 2 V, id = 4 vc = 8 A and vd = 2.2 V id and vd adhere to the passive convention so P = vd id = (2.2) (8) = 17.6 W is the power received by the dependent source. The power supplied by the dependent source is 17.6 W. Ex. 2.83 ic = 1.25 A, vd = 2 ic = 2.5 V and id = 1.75 A id and vd adhere to the passive convention so P = vd id = (2.5) (1.75) = 4.375 W is the power received by the dependent source. 22 Ex. 2.91 = 45 , I = 2 mA, R p = 20 k
a= 45 (20 k) = 2.5 k aR = p 360 360 vm = (2 103 )(2.5 103 ) = 5 V Ex. 2.92 v = 10 V, i = 280 A, k = 1 A
K for AD590 K i = 280 K i = kT T = = (280A)1 A k Ex. 2.101 At t = 4 s both switches are open, so i = 0 A.
Ex. 2.10.2 At t = 4 s the switch is in the up position, so v = i R = (2 mA)(3 k) = 6V . At t = 6 s the switch is in the down position, so v = 0 V. Problems
Section 23 Engineering and Linear Models P2.31 The element is not linear. For example, doubling the current from 2 A to 4 A does not double the voltage. Hence, the property of homogeneity is not satisfied. P2.32 (a) The data points do indeed lie on a straight line. The slope of the line is 0.12 V/A and the line passes through the origin so the equation of the line is v = 0.12 i . The element is indeed linear. (b) When i = 40 mA, v = (0.12 V/A)(40 mA) = (0.12 V/A)(0.04 A) = 4.8 mV 4 (c) When v = 4 V, i = = 33 A = 33 A. 0.12
23 P2.33 (a) The data points do indeed lie on a straight line. The slope of the line is 256.5 V/A and the line passes through the origin so the equation of the line is v = 256.5i . The element is indeed linear. (b) When i = 4 mA, v = (256.5 V/A)(4 mA) = (256.5 V/A)(0.004 A) = 1.026 V 12 (c) When v = 12 V, i = = 0.04678 A = 46.78 mA. 256.5 Let i = 1 A , then v = 3i + 5 = 8 V. Next 2i = 2A but 16 = 2v 3(2i) + 5 = 11.. Hence, the property of homogeneity is not satisfied. The element is not linear.
P2.34 Section 25 Resistors P2.51 i = is = 3 A and v = Ri = 7 3 = 21 V v and i adhere to the passive convention P = v i = 21 3 = 63 W is the power absorbed by the resistor. P2.52 i = is = 3 mA and v = 24 V R = v 24 = = 8000 = 8 k i .003 P = (310 3 ) 24 = 7210 3 = 72 mW P2.53 v = vs =10 V and R = 5 v 10 = =2 A R 5 v and i adhere to the passive convention p = v i = 210 = 20 W is the power absorbed by the resistor i = 24 P2.54 v = vs = 24 V and i = 2 A R= v 24 = = 12 i 2 p = vi = 242 = 48 W P2.55 v1 = v 2 = vs = 150 V; R1 = 50 ; R2 = 25 v 1 and i1 adhere to the passive convention so v 1 150 = =3 A R 1 50 v 150 v2 and i 2 do not adhere to the passive convention so i 2 =  2 =  = 6 A R2 25 i1 = The power absorbed by R1 is P = v1 i1 = 150 3 = 450 W 1 The power absorbed by R 2 is P 2 =  v 2i 2 = 150(6) = 900 W P2.56 i1 = i 2 = is = 2 A ; R1 =4 and R2 = 8 v 1 and i 1 do not adhere to the passive convention so v 1 = R 1 i 1 =42=8 V. The power absorbed by R 1 is P1 =v 1i 1 =(8)(2) = 16 W. v2 and i 2 do adhere to the passive convention so v2 = R 2 i 2 = 8 2 = 16 V . The power absorbed by R 2 is P 2 = v 2i 2 = 16 2 = 32 W.
P2.57
Model the heater as a resistor, then (250) 2 v2 v2 R = = = 62.5 1000 R P v 2 (210) 2 = 705.6 W with a 210 V source: P = = R 62.5 with a 250 V source: P = 25 P2.58
The current required by the mine lights is: i = P 5000 125 A = = 3 v 120 Power loss in the wire is : i 2 R Thus the maximum resistance of the copper wire allowed is 0.05P 0.055000 = = 0.144 (125/3) 2 i2 now since the length of the wire is L = 2100 = 200 m = 20,000 cm R= thus R = L / A with = 1.7106 cm from Table 2.51 A= L
R = 1.7106 20,000 = 0.236 cm 2 0.144 Section 26 Independent Sources P2.61
v s 15 2 = = 3 A and P = R i 2 = 5 ( 3 ) = 45 W R 5 (b) i and P do not depend on is . (a) i = The values of i and P are 3 A and 45 W, both when i s = 3 A and when i s = 5 A.
P2.62 v 2 102 = 20 W (a) v = R i s = 5 2 = 10 V and P = = R 5 (b) v and P do not depend on v s . The values of v and P are 10V and 20 W both when v s = 10 V and when v s = 5 V 26 P2.63 Consider the current source: i s and v s do not adhere to the passive convention, so Pcs =i s v s =312 = 36 W is the power supplied by the current source. Consider the voltage source: i s and v s do adhere to the passive convention, so Pvs = i s vs =3 12 = 36 W is the power absorbed by the voltage source. The voltage source supplies 36 W.
P2.64 Consider the current source: i s and vs adhere to the passive convention so Pcs = i s vs =3 12 = 36 W is the power absorbed by the current source. Current source supplies  36 W.
Consider the voltage source: i s and vs do not adhere to the passive convention so Pvs = i s vs = 3 12 =36 W is the power supplied by the voltage source. P2.65 (a) P = v i = (2 cos t ) (10 cos t ) = 20 cos 2 t mW
1 1 (b) w = 0 P dt = 0 20 cos t dt = 20 t + sin 2t = 10 + 5 sin 2 mJ 2 4 0
1 1 2 1 27 Section 27 Voltmeters and Ammeters P2.71 (a) R = v 5 = = 10 i 0.5 (b) The voltage, 12 V, and the current, 0.5 A, of the voltage source adhere to the passive convention so the power P = 12 (0.5) = 6 W is the power received by the source. The voltage source delivers 6 W.
P2.72 The voltmeter current is zero so the ammeter current is equal to the current source current except for the reference direction: i = 2 A The voltage v is the voltage of the current source. The power supplied by the current source is 40 W so 40 = 2 v v = 20 V 28 Section 28 Dependent Sources P2.81
r = vb 8 = =4 ia 2 P2.82
vb = 8 V ; g v b = i a = 2 A ; g = ia 2 A = = 0.25 vb 8 V i a 32 A = =4 ib 8 A P2.83
i b = 8 A ; d i b = i a = 32A ; d = P2.84
va = 2 V ; b va = vb = 8 V ; b = vb 8 V = =4 va 2 V Section 29 Transducers P2.91
a= 360 , = 360 vm Rp I = (360)(23V) = 75.27 (100 k)(1.1 mA) P2.92
AD590 : k =1 , K v =20 V (voltage condition satisfied) A 4 A < i < 13 A i T = k 4 K< T <13 K 29 Section 210 Switches P2.101 At t = 1 s the left switch is open and the right switch is closed so the voltage across the resistor is 10 V.
i= v 10 = = 2 mA R 5103 At t = 4 s the left switch is closed and the right switch is open so the voltage across the resistor is 15 V.
i= v 15 = = 3 mA R 5103 P2.102 At t = 1 s the current in the resistor is 3 mA so v = 15 V. At t = 4 s the current in the resistor is 0 A so v = 0 V. Verification Problems
VP21 vo =40 V and i s =  (2) = 2 A. (Notice that the ammeter measures  i s rather than i s .) So vo 40 V = = 20 2 A is Your lab partner is wrong.
VP22 vs 12 = 0.48 A. The power absorbed by = R 25 this resistor will be P = i vs = (0.48) (12) = 5.76 W. We expect the resistor current to be i = A half watt resistor can't absorb this much power. You should not try another resistor. 210 Design Problems
DP21 1.) 10 10 > 0.04 R < = 250 R 0.04 102 1 < R > 200 R 2 2.) Therefore 200 < R < 250 . For example, R = 225 .
DP22 1.) 2 R > 40 R > 20 15 2.) 2 2 R < 15 R < = 3.75 4 Therefore 20 < R < 3.75 . These conditions cannot satisfied simultaneously. DP23 P = ( 30 mA ) (1000 ) = (.03) (1000 ) = 0.9 W < 1 W 1
2 2 P2 = ( 30 mA ) ( 2000 ) = (.03) ( 2000 ) = 1.8 W < 2 W
2 2 P3 = ( 30 mA ) ( 4000 ) = (.03) ( 4000 ) = 3.6 W < 4 W
2 2 211 Chapter 3 Resistive Circuits
Exercises
Ex 3.31 Apply KCL at node a to get Apply KCL at node c to get Apply KCL at node b to get 2 + 1 + i3 = 0 i3 = 3 A 2 + 1 = i4 i4 = 3 A i3 + i6 = 1 3 + i6 = 1 i6 = 4 A Apply KVL to the loop consisting of elements A and B to get v2 3 = 0 v2 = 3 V Apply KVL to the loop consisting of elements C, E, D, and A to get 3 + 6 + v4 3 = 0 v4 = 6 V Apply KVL to the loop consisting of elements E and F to get v6 6 = 0 v6 = 6 V Check: The sum of the power supplied by all branches is (3)(2) + (3)(1) (3)(3) + (6)(3) (6)(1) + (6)(4) = 6  3 + 9  18  6 + 24 = 0 31 Ex 3.32 Apply KCL at node a to determine the current in the horizontal resistor as shown. Apply KVL to the loop consisting of the voltages source and the two resistors to get 4(2i) + 4(i)  24 = 0 i = 4 A Ex 3.33 18 + 0  12  va = 0 va = 30 V and im = 2 va + 3 im = 9 A 5 Ex 3.34 va  10 + 4va  8 = 0 va = 18 = 6 V and vm = 4 va = 24 V 3 Ex 3.41
From voltage division v3 = 12 3 = 3V 3+9 then
v i = 3 = 1A 3 The power absorbed by the resistors is: (12 ) ( 6 ) + (12 ) ( 3) + (12 ) ( 3) = 12 W The power supplied by the source is (12)(1) = 12 W. 32 Ex 3.42
P = 6 W and R1 = 6 i2 = P 6 = = 1 or i =1 A R1 6 v0 = i R1 =(1) (6)=6V + i (2 + 4 + 6 + 2) = 0 s v = 14 i = 14 V s from KVL:  v Ex 3.43 25 From voltage division v = (8) = 2 V m 25+75 25 From voltage division v = ( 8 ) = 2 V m 25+75 Ex 3.44 Ex. 3.51 1 R eq = 1 1 1 1 4 + 3+ 3+ 3= 3 3 10 10 10 10 10 R eq = 103 1 = k 4 4 By current division, the current in each resistor = 1 3 1 (10 ) = mA 4 4 Ex 3.52 10 From current division i = ( 5 ) =  1 A m 10+40 33 Problems
Section 33 Kirchoff's Laws P3.31 Apply KCL at node a to get 2 + 1 = i + 4 i = 1 A The current and voltage of element B adhere to the passive convention so (12)(1) = 12 W is power received by element B. The power supplied by element B is 12 W. Apply KVL to the loop consisting of elements D, F, E, and C to get 4 + v + (5) 12 = 0 v = 13 V The current and voltage of element F do not adhere to the passive convention so (13)(1) = 13 W is the power supplied by element F. Check: The sum of the power supplied by all branches is (2)(12) + 12 (4)(12) + (1)(4) + 13 (1)(5) = 24 +12 48 + 4 +13 5 = 0 34 P3.32 Apply KCL at node a to get Apply KCL at node b to get 2 = i2 + 6 = 0 i2 = 4 A 3 = i4 + 6 i4 = 3 A Apply KVL to the loop consisting of elements A and B to get v2 6 = 0 v2 = 6 V Apply KVL to the loop consisting of elements C, D, and A to get v3 (2) 6 = 0 v4 = 4 V Apply KVL to the loop consisting of elements E, F and D to get 4 v6 + (2) = 0 v6 = 2 V Check: The sum of the power supplied by all branches is (6)(2) (6)(4) (4)(6) + (2)(3) + (4)(3) + (2)(3) = 12  24 + 24 + 6 + 12 6 = 0 35 P3.33 KVL : 12  R 2 (3) + v = 0 (outside loop) v = 12 + 3R 2 or R 2 = KCL i+ v  12 3 12  3 = 0 (top node) R1 12 12 or R1 = 3i R1 i = 3 (a) v = 12 + 3 ( 3) = 21 V i = 3 12 =1 A 6 (b) R2 = 2  12 10 12 =  ; R1 = =8 3 3 3  1.5 (checked using LNAP 8/16/02) (c) 24 =  12 i, because 12 and i adhere to the passive convention. i =  2 A and R1 = 9 = 3v, v = 3V 12 = 2.4 3+ 2 because 3 and v do not adhere to the passive convention 3  12 = 3 3 and R 2 = The situations described in (b) and (c) cannot occur if R1 and R2 are required to be nonnegative. 36 P3.34 12 =2A i = 1 6 20 = 5A i = 2 4 i = 3i =  2 A 3 2 i = i +i = 3A 4 2 3
Power absorbed by the 4 resistor = 4 i 2 = 100 W 2 Power absorbed by the 6 resistor = 6 i 2 = 24 W 1 Power absorbed by the 8 resistor = 8 i 2 = 72 W 4 (checked using LNAP 8/16/02) P3.35 v1 = 8 V v2 = 8 + 8 + 12 = 12 V v3 = 2 4 = 8 V v2 4 : P = 3 = 16 W 4 2 v2 = 24 W 6 : P = 6 v2 8 : P = 1 = 8 W 8 (checked using LNAP 8/16/02) P3.36 P2 mA =  3 ( 2 103 ) = 6 103 = 6 mW P1 mA =  7 (1 103 ) = 7 103 = 7 mW (checked using LNAP 8/16/02) 37 P3.37 P2 V = + 2 (1 103 ) = 2 103 = 2 mW 3 P3 V = + 3 ( 2 10 ) = 6 103 = 6 mW (checked using LNAP 8/16/02) P3.38
KCL: iR = 2 + 1 iR = 3 A KVL: vR + 0  12 = 0 vR = 12 V R= vR 12 = =4 iR 3 (checked using LNAP 8/16/02) P3.39
KVL: vR + 56 + 24 = 0 vR = 80 V KCL: iR + 8 = 0 iR = 8 A R= vR 80 = = 10 iR 8 (checked using LNAP 8/16/02) 38 P3.310 KCL at node b: 5.61 3.71  5.61 12  5.61 1.9 = + 0.801 = + 1.278 7 R1 5 R1 R1 = 1.9 = 3.983 4 1.278  0.801 KCL at node a: 3.71 3.71  5.61 3.71  12 8.29 + + = 0 1.855 + ( 0.475 ) + =0 2 4 R2 R2 R2 = 8.29 = 6.007 6 1.855  0.475 (checked using LNAP 8/16/02) 39 Section 34 A SingleLoop Circuit The Voltage Divider P3.41
6 6 12 = 12 = 4 V v = 1 6+3+5+ 4 18 3 5 10 12 = 2 V ; v = 12 = V v = 2 18 3 18 3 4 8 v = 12 = V 4 18 3 (checked using LNAP 8/16/02)
P3.42 (a) R = 6 + 3 + 2 + 4 = 15 28 28 = = 1.867 A (b) i = R 15 ( c ) p = 28 i =28(1.867)=52.27 W (28 V and i do not adhere to the passive convention.) (checked using LNAP 8/16/02) 310 P3.43 i R2 = v = 8 V 12 = i R1 + v = i R1 + 8 4 = i R1 8 8 4 4 100 ; R1 = = = = 50 8 R 2 100 i 4 4 8 8 100 ; R2 = = = 200 (b) i = = 4 R1 100 i 4 8 ( c ) 1.2 = 12 i i = 0.1 A ; R1 = = 40 ; R2 = = 80 i i (a) i= (checked using LNAP 8/16/02)
P3.44 Voltage division 16 v1 = 12 = 8 V 16 + 8 4 v3 = 12 = 4 V 4+8 KVL: v3  v  v1 = 0 v = 4 V (checked using LNAP 8/16/02)
P3.45 100 v using voltage divider: v = 0 100 + 2 R s v R = 50 s  1 v o with v = 20 V and v > 9 V, R < 61.1 s 0 R = 60 with v = 28 V and v < 13 V, R > 57.7 s 0 311 P3.46 240 a.) 18 = 12 V 120 + 240 18 b.) 18 = 0.9 W 120 + 240 R c.) 18 = 2 18 R = 2 R + 2 (120 ) R = 15 R + 120 R d.) 0.2 = ( 0.2 )(120 ) = 0.8 R R = 30 R + 120 (checked using LNAP 8/16/02) 312 Section 35 Parallel Resistors and Current Division P3.51 i = 1 i = 2 i = 3 i = 4 1 1 1 6 4= 4= A 1 + 1 + 1 +1 1+ 2 + 3 + 6 3 6 3 2 1 1 2 3 4 = A; 1 + 1 + 1 +1 3 6 3 2 1 1 2 4 =1 A 1 + 1 + 1 +1 6 3 2 1 1 4=2 A 1 + 1 + 1 +1 6 3 2 P3.52 (a) (b) (c) 1 1 1 1 1 = + + = R = 2 R 6 12 4 2 v = 6 2 = 12 V p = 6 12 = 72 W P3.53 i= 8 8 or R1 = R1 i 8 8 or R 2 = 2i R2 8 = R 2 (2  i ) i = 2  (a) (b) 8 4 8 = A ; R1 = =6 4 12 3 3 8 2 8 i = = A ; R2 = =6 2 12 3 2 3 i = 2 313 ( c ) R1 = R 2
2 P3.54 R1 R 2 R1 + R 2 1 will cause i= 2 = 1 A. The current in both R1 and R 2 will be 1 A. 2 1 = 8 ; R1 = R 2 2 R1 = 8 R1 = 8 R1 = R 2 = 8 2 Current division: 8 i = 6 = 2 A 1 16 + 8 ( ) 8 i = 6 = 3 A 2 8+8( ) i = i i 1 2
P3.55 = +1 A R 1 i and current division: i = 2 R + R s 1 2 Ohm's Law: v = i R yields o 2 2 v R + R 2 i = o 1 s R R 2 1 plugging in R = 4, v > 9 V o 1 and R = 6, v < 13 V gives o 1 So any 3.15 A < i < 3.47 A s gives i > 3.15 A s i < 3.47 A s keeps 9 V < v < 13 V. o 314 P3.56 24 a) 1.8 = 1.2 A 12 + 24 R b) 2 = 1.6 2 R = 1.6 R + 1.6 (12 ) R = 48 R + 12 R c) 0.4 = ( 0.4 )(12 ) = 0.6 R R = 8 R + 12 Section 37 Circuit Analysis P3.71 (a) (b) (c) 48 24 = 32 48 + 24 32 32 v = 32 + 32 24 = 16 V ; 32 32 8+ 32 + 32 16 1 = A i= 32 2 48 1 1 = A i2 = 48 + 24 2 3 R = 16 + 315 P3.72 (a) R1 = 4 + (b) 1 Rp 3 6 =6 3+ 6 1 1 1 = + + R p = 2.4 then 12 6 6 R 2 = 8 + R p = 10.4 (c) KCL: i2 + 2 = i1 and  24 + 6 i2 + R 2i1 = 0 24+6 (i1 2)+10.4i1 = 0 36 =2.2 A v1 =i1 R 2 =2.2 (10.4)=22.88 V i1 = 16.4
1 6 (d ) i2 = ( 2.2 ) = 0.878 A, 1 1 1 + + 6 6 12 v2 = ( 0.878 ) (6) = 5.3 V (e) i3 = 6 2 i2 = 0.585 A P = 3 i3 = 1.03 W 3+ 6 316 P3.73 Reduce the circuit from the right side by repeatedly replacing series 1 resistors in parallel with a 2 resistor by the equivalent 1 resistor This circuit has become small enough to be easily analyzed. The vertical 1 resistor is equivalent to a 2 resistor connected in parallel with series 1 resistors: i1 = 1+1 (1.5 ) = 0.75 A 2 + (1 + 1) 317 P3.74 (a) 1 1 1 1 = + + R2 24 12 8 R2 = 4 and R1 = b (10 + 8) 9 = 6 10 + 8 + 9 g (b) First, apply KVL to the left mesh to get 27 + 6 ia + 3 ia = 0 ia = 3 A . Next, apply KVL to the left mesh to get 4 ib  3 ia = 0 ib = 2.25 A . (c) 1 8 2.25 = 1125 A . i2 = 1 1 1 + + 24 8 12 and v1 =  10 b gLM b10 +98g + 9 3OP = 10 V Q N 318 P3.75 30 v1 = 6 v1 = 8 V 10 + 30 R2 12 = 8 R2 = 20 R2 + 10 20 = R1 10 + 30 R1 + 10 + 30 b b g g R1 = 40 Alternate values that can be used to change the numbers in this problem: meter reading, V 6 4 4 4.8 Rightmost resistor, 30 30 20 20 R1, 40 10 15 30 319 P3.76 P3.77
1 103 = 24 12 103 + R p
3 R p = 12 103 = 12 k
3 12 10 = R p ( 2110 ) R = ( 2110 ) + R
3 R = 28 k P3.78 130 500 = 15.963 V Voltage division v = 50 130 500 + 200 + 20 100 10 v = v = (15.963) = 12.279 V h 100 + 30 13 v i = h = .12279 A h 100 320 P3.79 321 P3.710 Req = ia =  15 ( 20 + 10 ) = 10 15 + ( 20 + 10 ) 60 30 60 20 = 6 A, ib = = 4 A, vc = ( 60 ) = 40 V R Req 30 + 15 eq 20 + 10 P3.711 a) Req = 24 12 = (24)(12) =8 24 + 12 b) from voltage division: 100 5 20 100 v = 40 V i = 3 = A = x x 20 3 3 20 + 4 from current division: i = i 5 8 A = x 8+8 6 322 P3.712 9 + 10 + 17 = 36 a.) 36 (18 ) = 12 36+18 b.) 36 R = 18 18 R = (18 )( 36 ) R = 36 36+R P3.713 2 R( R ) 2 = R 2R + R 3 v 2 240 Pdeliv. = = =1920 W Req 2 R to ckt 3 Thus R =45 Req = P3.714 R = 2 + 1 + ( 6 12 ) + ( 2 2 ) = 3 + 4 + 1 = 8 eq
i = 40 40 = =5 A Req 8 6 5 1 i1 = i = ( 5) 3 = 3 A 6 + 12 2 5 1 i2 = i = ( 5) 2 = 2 A 2+2 ( ) from current division ( ) 323 Verification Problems
VP31 KCL at node a: i = i + i 3 1 2  1.167 =  0.833 + ( 0.333)  1.167=  1.166 OK KVL loop consisting of the vertical 6 resistor, the 3 and4 resistors, and the voltage source: 6i + 3i + v + 12 = 0 3 2 yields v = 4.0 V not v = 2.0 V VP32 reduce circuit: 5+5=10 in parallel with 20 gives 6.67 6.67 by current division: i = 5 = 1.25 A 20 + 6.67 Reported value was correct. VP33 320 v = ( 24 ) = 6.4 V o 320 + 650 + 230 Reported value was incorrect. 324 VP34 KVL bottom loop:  14 + 0.1iA + 1.2iH = 0 KVL right loop:  12 + 0.05iB + 1.2iH = 0 KCL at left node: iA + iB = iH This alone shows the reported results were incorrect. Solving the three above equations yields: iA = 16.8 A iH = 10.3 A iB = 6.49 A Reported values were incorrect. VP35 1 Top mesh: 0 = 4 i a + 4 i a + 2 i a +  i b = 10 ( 0.5 ) + 1  2 ( 2 ) 2 Lower left mesh: vs = 10 + 2 ( i a + 0.5  i b ) = 10 + 2 ( 2 ) = 14 V Lower right mesh: vs + 4 i a = 12 vs = 12  4 (0.5) = 14 V The KVL equations are satisfied so the analysis is correct. 325 VP36 Apply KCL at nodes b and c to get: KCL equations: Node e: 1 + 6 = 0.5 + 4.5 Node a: Node d: 0.5 + i c = 1 i c = 1.5 mA i c + 4 = 4.5 i c = 0.5 mA That's a contradiction. The given values of ia and ib are not correct. Design Problems
DP31 Using voltage division: vm = R1 + (1  a ) R p + R 2 + aR p R 2 + aR p 24 = R 2 + aR p R1 + R 2 + R p 24 vm = 8 V when a = 0 R2 R1 + R 2 + R p vm = 12 V when a = 1 R2 + R p R1 + R 2 + R p The specification on the power of the voltage source indicates 242 1 R1 + R 2 + R p 1152 R1 + R 2 + R p 2 = 1 3 1 2 = Try Rp = 2000 . Substituting into the equations obtained above using voltage division gives 3R 2 = R1 + R 2 + 2000 and 2 ( R 2 + 2000 ) = R1 + R 2 + 2000 . Solving these equations gives R1 = 6000 and R 2 = 4000 . With these resistance values, the voltage source supplies 48 mW while R1, R2 and Rp dissipate 24 mW, 16 mW and 8 mW respectively. Therefore the design is complete. 326 DP32 Try R1 = . That is, R1 is an open circuit. From KVL, 8 V will appear across R2. Using voltage 200 division, 12 = 4 R 2 = 400 . The power required to be dissipated by R2 R 2 + 200 82 1 = 0.16 W < W . To reduce the voltage across any one resistor, let's implement R2 as the is 400 8 series combination of two 200 resistors. The power required to be dissipated by each of these 42 1 = 0.08 W < W . resistors is 200 8 Now let's check the voltage: 190 210 11.88 < v < 12.12 0 190 + 420 210 + 380 3.700 < v0 < 4.314 4  7.5% < v0 < 4 + 7.85% Hence, vo = 4 V 8% and the design is complete.
DP33
Vab 200 mV 10 10 120 Vab = (120) (0.2) 10 + R 10 + R 240 R=5 let v = 16 = 10 + R 162 = 25.6W P= 10 v= DP34 N 1 N 1 = N i = G v = v where G = T T R R n = 1 Rn N= iR ( 9 )(12 ) = = 18 bulbs v 6 327 28 Chapter 4 Methods of Analysis of Resistive Circuits
Exercises
Ex. 4.31
v v v a a b + + 3 = 0 5 v  3 v = 18 a b 3 2 KCL at a: KCL at b: v v b a  3 1 = 0 v  v = 8 b a 2 Solving these equations gives: va = 3 V and vb = 11 V Ex. 4.32 KCL at a:
v v v a a b + + 3 = 0 3 v  2 v = 12 a b 4 2 v KCL at a: Solving: v v b a b  4=0 3 2  3 v + 5 v = 24 a b va = 4/3 V and vb = 4 V Ex. 4.41 Apply KCL to the supernode to get
v + 10 v 2+ b + b =5 20 30 Solving: v = 30 V and v = v + 10 = 40 V b a b 41 Ex. 4.42 ( vb + 8)  ( 12) + vb = 3
10 40 v = 8 V and v = 16 V b a Ex. 4.51 Apply KCL at node a to express ia as a function of the node voltages. Substitute the result into vb = 4 ia and solve for vb . 6 vb + =i 8 12 a 9 + vb v = 4i = 4 v = 4.5 V b a b 12 Ex. 4.52 The controlling voltage of the dependent source is a node voltage so it is already expressed as a function of the node voltages. Apply KCL at node a.
v 6 v 4v a a = 0 v = 2 V + a a 20 15 Ex. 4.61 Mesh equations:
12 + 6 i + 3 i  i  8 = 0 9 i  3 i = 20 1 2 1 1 2 8  3 i  i + 6 i = 0  3 i + 9 i = 8 1 2 2 1 2 Solving these equations gives:
13 1 i = A and i =  A 1 6 2 6 The voltage measured by the meter is 6 i2 = 1 V. 42 Ex. 4.71 3 Mesh equation: 9 + 3 i + 2 i + 4 i + = 0 4 The voltmeter measures 3 i = 4 V ( 3 + 2 + 4 ) i = 9  3 i= 12 A 9 Ex. 4.72 Mesh equation: 15 + 3 i + 6 ( i + 3) = 0 Ex. 4.73 ( 3 + 6 ) i = 15  6 ( 3) i= 33 2 = 3 A 9 3 3 3 = i1  i 2 i1 = + i 2 . 4 4 3 Apply KVL to the supermesh: 9 + 4i1 + 3 i 2 + 2 i 2 = 0 4 + i 2 + 5 i 2 = 9 9 i 2 = 6 4 2 4 so i 2 = A and the voltmeter reading is 2 i 2 = V 3 3 Express the current source current in terms of the mesh currents: 43 Ex. 4.74 Express the current source current in terms of the mesh currents: 3 = i1  i 2
1 A is the current measured by the ammeter. 3 Apply KVL to the supermesh: 15 + 6 i1 + 3 i 2 = 0 6 ( 3 + i 2 ) + 3 i 2 = 15 9 i 2 = 3 i1 = 3 + i 2 . Finally, i 2 =  Problems
Section 43 Node Voltage Analysis of Circuits with Current Sources P4.31 KCL at node 1:
0= v v v 4  4  2 1 1 2 + +i = + + i = 1.5 + i i = 1.5 A 8 6 8 6 (checked using LNAP 8/13/02) 44 P4.32 KCL at node 1: v v v 1 2 1 + + 1 = 0 5 v  v = 20 1 2 20 5 KCL at node 2: v v v v 1 2 2 3 +2=  v + 3 v  2 v = 40 1 2 3 20 10 KCL at node 3: v v v 2 3 3 +1 =  3 v + 5 v = 30 2 3 10 15 Solving gives v1 = 2 V, v2 = 30 V and v3 = 24 V. (checked using LNAP 8/13/02)
P4.33 KCL at node 1:
v v v 4  15 4 1 2 1 + =i i = + = 2 A 1 5 20 1 5 20 KCL at node 2:
v v v v 1 2 2 3 +i = 2 5 15 4  15 15  18 i =  =2A + 2 15 5 (checked using LNAP 8/13/02) 45 P4.34 Node equations:
.003 +  When v1 = 1 V, v2 = 2 V v1 v1  v2 + =0 R1 500 v1  v2 v2 +  .005 = 0 500 R2 1 1 1 + = 0 R1 = = 200 1 R1 500 .003 + 500 2 1 2  +  .005 = 0 R2 = = 667 1 500 R2 .005  500 .003 + (checked using LNAP 8/13/02) P4.35 Node equations: v1 v  v 2 v1  v3 + 1 + =0 500 125 250 v  v3 v  v2  1  .001 + 2 =0 125 250 v  v3 v1  v3 v3  2  + =0 250 250 500 Solving gives: v1 = 0.261 V, v2 = 0.337 V, v3 = 0.239 V Finally, v = v1  v3 = 0.022 V (checked using LNAP 8/13/02) 46 Section 44 Node Voltage Analysis of Circuits with Current and Voltage Sources P4.41 Express the branch voltage of the voltage source in terms of its node voltages: 0  va = 6 va = 6 V KCL at node b: va  vb v v +2= b c 6 10 KCL at node c: 6  vb v v +2= b c 6 10 1 vb v v +2= b c 6 10 vb = 9 vc 4 30 = 8 vb  3 vc vb  vc vc = 10 8 4 vb  4 vc = 5 vc Finally: 9 30 = 8 vc  3 vc 4 vc = 2 V (checked using LNAP 8/13/02) P4.42 Express the branch voltage of each voltage source in terms of its node voltages to get: va = 12 V, vb = vc = vd + 8 47 KCL at node b: vb  va = 0.002 + i 4000 vb  ( 12 ) = 0.002 + i vb + 12 = 8 + 4000 i 4000 KCL at the supernode corresponding to the 8 V source: v 0.001 = d + i 4 = vd + 4000 i 4000 vb + 4 = 4  vd ( vd + 8 ) + 4 = 4  vd vd = 4 V so Consequently vb = vc = vd + 8 = 4 V and i = 4  vd = 2 mA 4000 (checked using LNAP 8/13/02)
P4.43 Apply KCL to the supernode: va  10 va va  8 + +  .03 = 0 va = 7 V 100 100 100 (checked using LNAP 8/13/02)
P4.44 Apply KCL to the supernode: va + 8 ( va + 8 )  12 va  12 va + + + =0 500 125 250 500 Solving yields va = 4 V (checked using LNAP 8/13/02) 48 P4.45 The power supplied by the voltage source is v v v v 12  9.882 12  5.294 va ( i1 + i 2 ) = va a b + a c = 12 + 6 4 6 4 = 12(0.5295 + 1.118) = 12(1.648) = 19.76 W (checked using LNAP 8/13/02)
P4.46 Label the voltage measured by the meter. Notice that this is a node voltage. Write a node equation at the node at which the node voltage is measured. 12  v m v m v 8  + 0.002 + m =0 + 3000 6000 R That is 6000 6000 3 + v m = 16 R = 16 R 3 vm (a) The voltage measured by the meter will be 4 volts when R = 6 k. (b) The voltage measured by the meter will be 2 volts when R = 1.2 k. 49 Section 45 Node Voltage Analysis with Dependent Sources P4.51 Express the resistor currents in terms of the node voltages:
va  vc = 8.667  10 = 1.333 A and 1 v v 2  10 i 2= b c = = 4 A 2 2 i 1= Apply KCL at node c: i1 + i 2 = A i1  1.333 + ( 4 ) = A (1.333) A= 5.333 =4 1.333 (checked using LNAP 8/13/02)
P4.52 Write and solve a node equation: va  6 v v  4va + a + a = 0 va = 12 V 1000 2000 3000 ib = va  4va = 12 mA 3000 (checked using LNAP 8/13/02)
P4.53 First express the controlling current in terms of the node voltages: 2  vb i = a 4000 Write and solve a node equation:  2  vb v 2  vb + b  5 = 0 vb = 1.5 V 4000 2000 4000 (checked using LNAP 8/14/02) 410 P4.54 Apply KCL to the supernode of the CCVS to get 12  10 14  10 1 +  + i b = 0 i b = 2 A 4 2 2 Next
ia = 10  12 1 = 2 V =4 4 2 r = 1 A  r i a = 12  14 2 (checked using LNAP 8/14/02)
P4.55 First, express the controlling current of the CCVS in v2 terms of the node voltages: i x = 2 Next, express the controlled voltage in terms of the node voltages: v2 24 v2 = 12  v 2 = 3 i x = 3 V 2 5 so ix = 12/5 A = 2.4 A. (checked using ELab 9/5/02) 411 Section 46 Mesh Current Analysis with Independent Voltage Sources P 4.61 2 i1 + 9 (i1  i 3 ) + 3(i1  i 2 ) = 0 15  3 (i1  i 2 ) + 6 (i 2  i 3 ) = 0 6 (i 2  i 3 )  9 (i1  i 3 )  21 = 0 or 14 i1  3 i 2  9 i 3 = 0 3 i1 + 9 i 2  6 i 3 = 15 9 i1  6 i 2 + 15 i 3 = 21 so i1 = 3 A, i2 = 2 A and i3 = 4 A. (checked using LNAP 8/14/02) P 4.62 Top mesh: 4 (2  3) + R(2) + 10 (2  4) = 0 so R = 12 . Bottom, right mesh: 8 (4  3) + 10 (4  2) + v 2 = 0 so v2 = 28 V. Bottom left mesh v1 + 4 (3  2) + 8 (3  4) = 0 so v1 = 4 V. (checked using LNAP 8/14/02) 412 P 4.63 Ohm's Law: i 2 = 6 = 0.75 A 8 KVL for loop 1: R i1 + 4 ( i1  i 2 ) + 3 + 18 = 0 KVL for loop 2 + (6)  3  4 ( i1  i 2 ) = 0  9  4 ( i1  ( 0.75 ) ) = 0 R ( 3) + 4 ( 3  ( 0.75 ) ) + 21 = 0 R = 4 i 1 = 3 A (checked using LNAP 8/14/02)
P4.64 KVL loop 1: 25 ia  2 + 250 ia + 75 ia + 4 + 100 (ia  ib ) = 0 450 ia 100 ib = 2 KVL loop 2:
100(ia  ib )  4 + 100 ib + 100 ib + 8 + 200 ib = 0 100 ia + 500 ib =  4 ia =  6.5 mA , ib =  9.3 mA (checked using LNAP 8/14/02)
P4.65 Mesh Equations: mesh 1 : 2i1 + 2 (i1  i2 ) + 10 = 0 mesh 2 : 2(i2  i1 ) + 4 (i2  i3 ) = 0 mesh 3 :  10 + 4 (i3  i2 ) + 6 i3 = 0 Solving: 5 i = i2 i =  = 0.294 A 17 (checked using LNAP 8/14/02) 413 Section 47 Mesh Current Analysis with Voltage and Current Sources P4.71 mesh 1: i1 = 1 A 2 mesh 2: 75 i2 + 10 + 25 i2 = 0 i2 =  0.1 A ib = i1  i2 = 0.6 A (checked using LNAP 8/14/02)
P4.72 mesh a: ia =  0.25 A mesh b: ib =  0.4 A vc = 100(ia  ib ) = 100(0.15) =15 V (checked using LNAP 8/14/02)
P4.73 Express the current source current as a function of the mesh currents: i1  i2 =  0.5 i1 = i2  0.5 Apply KVL to the supermesh:
30 i1 + 20 i2 + 10 = 0 30 (i2  0.5) + 20i2 =  10 50 i2  15 =  10 i2 = i1 =.4 A and v2 = 20 i2 = 2 V (checked using LNAP 8/14/02) 5 = .1 A 50 414 P4.74 Express the current source current in terms of the mesh currents: ib = ia  0.02 Apply KVL to the supermesh: 250 ia + 100 (ia  0.02) + 9 = 0 ia =  .02 A =  20 mA vc = 100(ia  0.02) = 4 V (checked using LNAP 8/14/02) P4.75 Supermesh: 6 i1 + 3 i 3  5 ( i 2  i 3 )  8 = 0 6 i1  5 i 2 + 8 i 3 = 8 Lower, left mesh: 12 + 8 + 5 ( i 2  i 3 ) = 0 5 i 2 = 4 + 5 i 3 Eliminating i1 and i2 from the supermesh equation: 6 ( i 3  2 )  ( 4 + 5 i 3 ) + 8 i 3 = 8 9 i 3 = 24 24 The voltage measured by the meter is: 3 i 3 = 3 = 8 V 9 (checked using LNAP 8/14/02) Express the current source current in terms of the mesh currents: i 3  i 1 = 2 i1 = i 3  2 415 P4.76 Mesh equation for right mesh: 4 ( i  2 ) + 2 i + 6 ( i + 3) = 0 12 i  8 + 18 = 0 i =  10 5 A= A 12 6 (checked using LNAP 8/14/02)
P 4.77
i2 = 3 A i1  i2 = 5 i1  ( 3) = 5 2 ( i3  i1 ) + 4 i3 + R ( i3  i2 ) = 0 2 ( 1  2 ) + 4 ( 1) + R ( 1  ( 3) ) = 0 R=5 i1 = 2 A (checked using LNAP 8/14/02) 416 P 4.78 Express the controlling voltage of the dependent source as a function of the mesh current
v2 = 50 i1 Apply KVL to the right mesh: 100 (0.04(50i1 )  i1 ) + 50i1 + 10 = 0 i1 = 0.2 A v2 = 50 i1 = 10 V (checked using LNAP 8/14/02)
P 4.79 ib = 4ib  ia ib = 1 ia 3 1 100 ia + 200ia + 8 = 0 3 ia =  0.048 A (checked using LNAP 8/14/02)
P4.710 Express the controlling current of the dependent source as a function of the mesh current: ib = .06  ia Apply KVL to the right mesh: 100 (0.06  i a ) + 50 (0.06  i a ) + 250 i a = 0 Finally: vo = 50 i b = 50 (0.06  0.01) = 2.5 V ia = 10 mA (checked using LNAP 8/14/02) 417 P4.711 Express the controlling voltage of the dependent source as a function of the mesh current: vb = 100 (.006  ia ) Apply KVL to the right mesh: 100 (.006  ia ) + 3[100(.006  ia )] + 250 ia = 0 ia = 24 mA (checked using LNAP 8/14/02)
P4.712 apply KVL to left mesh :  3 + 10 103 i1 + 20 103 ( i1  i2 ) = 0 30 103 i1  20 103 i2 = 3 apply KVL to right mesh : 5 103 i1 + 100 103 i2 + 20 103 ( i2  i1 ) = 0 i1 = 8i2 Solving (1) & ( 2 ) simultaneously
Power delevered to cathode = (1) ( 2) i1 = 6 3 mA, i2 = mA 55 220 ( 5 i1 ) ( i2 ) + 100 ( i2 )2 = 5 6 ( 55)( 3 220) + 100 ( 3 220) 2 = 0.026 mW Energy in 24 hr. = Pt = ( 2.6 105 W ) ( 24 hr ) (3600 s hr ) = 2.25 J 418 P4.713 (a) vo =  g R L v and v = R2 R1 + R 2 vi RL R2 vo = g vi R1 + R 2 (b) vo = g vi (5 103 )(103 ) = 170
1.1103 g = 0.0374 S PSpice Problems
SP 41 419 SP 42 From the PSpice output file: VOLTAGE SOURCE CURRENTS NAME CURRENT V_V1 V_V2 3.000E+00 2.250E+00
V_V3 7.500E01 The voltage source labeled V3 is a short circuit used to measure the mesh current. The mesh currents are i1 = 3 A (the current in the voltage source labeled V1) and i2 = 0.75 A (the current in the voltage source labeled V3). SP 43 The PSpice schematic after running the simulation: The PSpice output file: **** INCLUDING sp4_2SCHEMATIC1.net **** * source SP4_2 V_V4 0 N01588 12Vdc 420 R_R4 V_V5 R_R5 V_V6 I_I1 I_I2 N01588 N01565 4k N01542 N01565 0Vdc 0 N01516 4k N01542 N01516 8Vdc 0 N01565 DC 2mAdc 0 N01542 DC 1mAdc VOLTAGE SOURCE CURRENTS NAME CURRENT V_V4 V_V5 V_V6 4.000E03 2.000E03 1.000E03 From the PSpice schematic: va = 12 V, vb = vc = 4 V, vd = 4 V. From the output file: i = 2 mA. SP 44 The PSpice schematic after running the simulation: The PSpice output file: VOLTAGE SOURCE CURRENTS NAME CURRENT V_V7 V_V8 5.613E01 6.008E01 The current of the voltage source labeled V7 is also the current of the 2 resistor at the top of the circuit. However this current is directed from right to left in the 2 resistor while the current i is directed from left to right. Consequently, i = +5.613 A. 421 Verification Problems
VP 41 Apply KCL at node b: vb  va v v 1  + b c = 0 4 2 5 4.8  5.2 1  4.8  3.0  + 0 4 2 5 The given voltages do not satisfy the KCL equation at node b. They are not correct. VP 42 Apply KCL at node a: v v v  b a  2 + a = 0 2 4 4 20  4  = 4 0 2+ 2 4 The given voltages do not satisfy the KCL equation at node a. They are not correct. 422 VP 43 Writing a node equation: 12  7.5 7.5 7.5  6  + =0 + R2 R1 R3 so 4.5 7.5 1.5 + + =0 R1 R3 R2 There are only three cases to consider. Suppose R1 = 5 k and R 2 = R 3 = 10 k. Then   4.5 7.5 1.5 0.9 + 0.75 + 0.15 + + = = 0 R1 R3 R2 1000 This choice of resistance values corresponds to branch currents that satisfy KCL. Therefore, it is indeed possible that two of the resistances are 10 kW and the other resistance is 5 kW. The 5 kW is R1. VP 44 KCL at node 1: 0= v1  v 2 20 + v1 5 +1 8  ( 20 ) 8 + +1 = 0 20 5 KCL at node 2: v1  v 2 20 = 2+ v 2  v3 10 8  ( 20 ) 20  ( 6 ) = 2+ 20 10 12 6 = 20 10 +1 = v3 15 20  ( 6 ) 6 4 6 +1 = = 10 15 10 15 KCL at node 3: v2  v3 10 KCL is satisfied at all of the nodes so the computer analysis is correct. 423 VP 45 Top mesh: 10 (2  4) + 12(2) + 4 (2  3) = 0 Bottom right mesh 8 (3  4) + 4 (3  2) + 4 = 0 Bottom, left mesh: 28 + 10 (4  2) + 8 (4  3) 0 (Perhaps the polarity of the 28 V source was entered incorrectly.) KVL is not satified for the bottom, left mesh so the computer analysis is not correct. 424 Design Problems
DP 41 Model the circuit as: a) We need to keep v2 across R2 as 4.8 v2 5.4
display is active 0.3 A For I = 0.1 A display is not active KCL at a: v2  15 v2 + +I =0 R1 R2 Assumed that maximum I results in minimum v2 and visaversa. Then 4.8 V v2 = 5.4 V when I = 0.3 A when I = 0.1 A Substitute these corresponding values of v2 and I into the KCL equation and solve for the resistances 4.8  15 4.8 + + 0.3 = 0 R1 R2 5.4  15 5.4 + + 0.1 = 0 R1 R2 R1 = 7.89 , R2 = 4.83 b)
15  4.8 = 1.292 A PR = (1.292)2 (7.89) = 13.17 W 1max 7.89 ( 5.4 )2 = 6.03 W 5.4 IR = = 1.118 A PR = 2max 2 max 4.83 4.83 maximum supply current = I R = 1.292 A IR
1max = 1max c) No; if the supply voltage (15V) were to rise or drop, the voltage at the display would drop below 4.8V or rise above 5.4V. The power dissipated in the resistors is excessive. Most of the power from the supply is dissipated in the resistors, not the display. 425 DP 42 Express the voltage of the 8 V source in terms of its node voltages to get vb  va = 8 . Apply KCL to the supernode corresponding to the 8 V source:
va  v1 R + va vb vb  ( v 2 ) + + = 0 2 va  v1 + 2 vb + v 2 = 0 R R R 2 va  v1 + 2 ( va + 8 ) + v 2 = 0 4 va  v1 + v 2 + 16 = 0 va = v1  v 2 4 4 Next set va = 0 to get 0= v1  v 2 4  4 v1  v 2 = 16 V For example, v1 = 18 V and v2 = 2 V. 426 DP 43 a) pply KCL to left mesh: Apply KCL to right mesh: Solving for I: 5 + 50 i1 + 300 (i1  I ) = 0
( R + 2) I + 300 ( I  i1 ) = 0 150 1570 + 35 R We desire 50 mA I 75 mA so if R = 100 , then I = 29.59 mA fi l amp so the lamp will not light. I= b) From the equation for I, we see that decreasing R increases I: try R = 50 I = 45 mA (won't light) try R = 25 I = 61 mA will light Now check R10% to see if the lamp will light and not burn out: 10% 22.5 I = 63.63 mA lamp will +10% 27.5 I = 59.23 mA stay on
DP 44 Equivalent resistance: R = R1  R 2  ( R 3 + R 4 ) R ( 25 ) 10 + R We require vab = 10 V. Apply the voltage division principle in the left circuit to get: Voltage division in the equivalent circuit: v1 = 427 10 = R1 R 2 ( R3 + R4 ) R4 R4 25 v1 = R3 + R4 R3 + R4 10 + R1 R 2 ( R3 + R4 ) ( ( ) ) This equation does not have a unique solution. Here's one solution: choose R1 = R2 = 25 and R3 + R4 = 20 then 10 = (12.5 20 ) 25 R = 18.4 R4 4 20 10 + (12.5 20 )
and R3 + R4 = 20 R3 = 1.6 DP 45 Apply KCL to the left mesh: (R 1 + R 3 ) i1  R 3 i2  v1 = 0 Apply KCL to the left mesh:  R 3 i1 + Solving for the mesh currents using Cramer's rule:  R3 v1 ( R1 + R 3 ) v2 ( R 2 + R 3 ) and i =  R 3 i1 = 2 2 where = ( R1 + R 3 ) ( R 2 + R 3 )  R 3 v1  v2 (R 2 + R 3 ) i2 + v2 = 0 Try R1 = R2 = R3 = 1 k = 1000 . Then = 3 M. The mesh currents will be given by
i 3 10 3 10 Now check the extreme values of the source voltages:
1 6 = [ 2v1  v2 ] 1000 and i 2 = [ 2v2 + v1 ] 1000
6 i = i1  i2 = v1 + v2 3000 mA 3 if v1 = v2 = 2 V i = 4 mA 3 if v1 = v2 = 1 V i = 2 okay okay 428 Chapter 5 Circuit Theorems
Exercises
Ex 5.31 R = 10 and is = 1.2 A. Ex 5.32 R = 10 and is = 1.2 A. Ex 5.33 R = 8 and vs = 24 V. Ex 5.34 R = 8 and vs = 24 V. Ex 5.41 vm = Ex 5.42 20 10 2 (15) + 20  ( 2 ) = 6 + 20( ) = 2 V 10 + 20 + 20 5 10 + (20 + 20) im =
Ex 5.43 25 3  ( 5) = 5  3 = 2 A 3+ 2 2+3 3 3 vm = 3 ( 5)  (18 ) = 5  6 = 1 A 3 + (3 + 3) 3 + (3 + 3) 51 Ex 5.51 52 Ex 5.52 ia = i a = 3 A 6 voc = 2 i a = 6 V 2 i a  12 12 + 6 i a = 2 i a 3 i sc = 2 i a i a = 3 A 2 ( 3 ) =  2 A 3 i sc = Rt = 6 =3 2 Ex 5.61 53 Ex 5.62 ia = i a = 3 A 6 voc = 2 i a = 6 V 2 i a  12 12 + 6 i a = 2 i a 3 i sc = 2 i a i a = 3 A 2 ( 3 ) =  2 A 3 i sc = Rt = 6 =3 2 54 Ex 5.63 12 24 12 24 = = 8 12 + 24 36 24 voc = ( 30 ) = 20 V 12 + 24 Rt = i= 20 8+ R Ex 5.71 voc = 6 (18) = 12 V 6+3 Rt = 2 + ( 3)( 6 ) = 4 3+ 6 For maximum power, we require R L = Rt = 4 Then
pmax = voc 122 = =9 W 4 Rt 4 ( 4 )
2 55 Ex 5.72 1 50 3 i sc = ( 5.6 ) = ( 5.6 ) = 5 A 1 1 1 50 + 1 + 5 + + 3 150 30 150 ( 30 ) Rt = 3 + = 3 + 25 = 28 150 + 30 2 R t i sc ( 28 ) 52 = 175 W pmax = = 4 4 Ex 5.73 10 R L 100 R L p=iv= (10 ) = 2 Rt + R L Rt + R L ( Rt + R L ) The power increases as Rt decreases so choose Rt = 1 . Then pmax = i v = 100 ( 5 ) = 13.9 W (1 + 5) 2 Ex 5.74 From the plot, the maximum power is 5 W when R = 20 . Therefore: and
pmax v = oc 4 Rt
2 Rt = 20 voc = pmax 4 Rt = 5 ( 4 ) 20 = 20 V 56 Problems
Section 53: Source Transformations P5.31 (a) 57 Rt = 2 (b) (c) 9  4i  2i + (0.5) = 0 9 + (0.5) i = = 1.58 A 4+2 v = 9 + 4 i = 9 + 4(1.58) = 2.67 V ia = i =  1.58 A vt =  0.5 V (checked using LNAP 8/15/02)
P5.32 Finally, apply KVL: 10 + 3 ia + 4 ia  16 =0 3 ia = 2.19 A (checked using LNAP 8/15/02) 58 P5.33 Source transformation at left; equivalent resistor for parallel 6 and 3 resistors: Equivalents for series resistors, series voltage source at left; series resistors, then source transformation at top: Source transformation at left; series resistors at right: Parallel resistors, then source transformation at left: 59 Finally, apply KVL to loop  6 + i (9 + 19)  36  vo = 0 i = 5 / 2 vo = 42 + 28 (5 / 2) = 28 V (checked using LNAP 8/15/02) P5.34  4  2000 ia  4000 ia + 10  2000 ia  3 = 0 ia = 375 A (checked using LNAP 8/15/02) 510 P5.35 12  6 ia + 24  3 ia  3 = 0 ia = 1 A (checked using LNAP 8/15/02)
P5.36 A source transformation on the right side of the circuit, followed by replacing series resistors with an equivalent resistor: Source transformations on both the right side and the left side of the circuit: 511 Replacing parallel resistors with an equivalent resistor and also replacing parallel current sources with an equivalent current source: Finally, va = 50 (100 ) 100 ( 0.21) = ( 0.21) = 7 V 50 + 100 3 (checked using LNAP 8/15/02) 512 Section 54 Superposition P5.41 Consider 6 A source only (open 9 A source) Use current division:
v1 15 = 6 v1 = 40 V 20 15 + 30 Consider 9 A source only (open 6 A source) Use current division: v2 10 = 9 v2 = 40 V 20 10 + 35 v = v1 + v2 = 40 + 40 = 80 V (checked using LNAP 8/15/02)
P5.42 Consider 12 V source only (open both current sources) KVL:
20 i1 + 12 + 4 i1 + 12 i1 = 0 i1 = 1/ 3 mA Consider 3 mA source only (short 12 V and open 9 mA sources) Current Division: 4 16 i2 = 3 = 3 mA 16 + 20 513 Consider 9 mA source only (short 12 V and open 3 mA sources) Current Division: 12 i3 = 9 = 3 mA 24 + 12 i = i1 + i2 + i3 =  1/ 3 + 4 / 3  3 =  2 mA (checked using LNAP 8/15/02)
P5.43 Consider 30 mA source only (open 15 mA and short 15 V sources). Let i1 be the part of i due to the 30 mA current source. 2 ia = 30 = 6 mA 2+8 6 i1 = ia = 2 mA 6 + 12 Consider 15 mA source only (open 30 mA source and short 15 V source) Let i2 be the part of i due to the 15 mA current source. 4 ib = 15 = 6 mA 4+6 6 i2 = ib = 2 mA 6 + 12 514 Consider 15 V source only (open both current sources). Let i3 be the part of i due to the 15 V voltage source. 6  6 3 i3 =  2.5 ( 6  6 ) + 12 =  10 3 + 12 = 0.5 mA Finally,
i = i1 + i2 + i3 = 2 + 2  0.5 = 3.5 mA (checked using LNAP 8/15/02)
P5.44 Consider 10 V source only (open 30 mA source and short the 8 V source) Let v1 be the part of va due to the 10 V voltage source.
v1 = = 100 100 (10 ) (100 100 ) + 100 50 10 (10 ) = V 150 3 Consider 8 V source only (open 30 mA source and short the 10 V source) Let v2 be the part of va due to the 8 V voltage source.
v1 = = 100 100 (8) (100 100 ) + 100 50 8 (8) = V 150 3 515 Consider 30 mA source only (short both the 10 V source and the 8 V source) Let v2 be the part of va due to the 30 mA current source.
v3 = (100 100 100)(0.03) = 100 (0.03) = 1 V 3 Finally, va = v1 + v2 + v3 = 10 8 + +1 = 7 V 3 3 (checked using LNAP 8/15/02) P5.45 Consider 8 V source only (open the 2 A source) Let i1 be the part of ix due to the 8 V voltage source. Apply KVL to the supermesh: 6 ( i1 ) + 3 ( i 1 ) + 3 ( i 1 )  8 = 0 i1 = 8 2 = A 12 3 Consider 2 A source only (short the 8 V source) Let i2 be the part of ix due to the 2 A current source. Apply KVL to the supermesh: 6 ( i 2 ) + 3 ( i 2 + 2 ) + 3 i2 = 0 i2 = 6 1 = A 12 2 Finally, i x = i1 + i 2 = 2 1 1  = A 3 2 6 516 Section 55: Thvenin's Theorem P5.51 (checked using LNAP 8/15/02) 517 P5.52 The circuit from Figure P5.52a can be reduced to its Thevenin equivalent circuit in four steps: (a) (b) (c) (d) Comparing (d) to Figure P5.52b shows that the Thevenin resistance is Rt = 16 and the open circuit voltage, voc = 12 V. 518 P5.53 The circuit from Figure P5.53a can be reduced to its Thevenin equivalent circuit in five steps: (a) (b) (c) (d) (e) Comparing (e) to Figure P5.53b shows that the Thevenin resistance is Rt = 4 and the open circuit voltage, voc = 2 V. (checked using LNAP 8/15/02) 519 P5.54 Find Rt: Rt = Write mesh equations to find voc: 12 (10 + 2 ) =6 12 + (10 + 2 ) Mesh equations:
12 i1 + 10 i1  6 ( i2  i1 ) = 0 6 ( i2  i1 ) + 3 i 2  18 = 0
28 i1 = 6 i 2 9 i 2  6 i 1 = 18 36 i1 = 18 i1 = i2 = 7 1 voc = 3 i 2 + 10 i1 = 3 + 10 = 12 V 3 2 14 1 7 = A 3 2 3 1 A 2 Finally, (checked using LNAP 8/15/02) 520 P5.55 Find voc: Notice that voc is the node voltage at node a. Express the controlling voltage of the dependent source as a function of the node voltage: va = voc Apply KCL at node a: 6  voc voc 3  +  voc = 0 + 8 4 4 6 + voc + 2 voc  6 voc = 0 voc = 2 V Find Rt: We'll find isc and use it to calculate Rt. Notice that the short circuit forces va = 0 Apply KCL at node a: 60 0 3  + +  0 + i sc = 0 8 4 4 i sc =
Rt = 6 3 = A 8 4 voc 2 8 = = i sc 3 4 3 (checked using LNAP 8/15/02) 521 P5.56 Find voc: 2 va  va va = + 3 + 0 va = 18 V 3 6 The voltage across the righthand 3 resistor is zero so: va = voc = 18 V Apply KCL at the top, middle node: Find isc: Apply KCL at the top, middle node: 2 va  va va v = + 3 + a va = 18 V 3 6 3 va 18 i sc = = = 6 V Apply Ohm's law to the righthand 3 resistor : 3 3 v 18 Finally: R t = oc = = 3 i sc 6 (checked using LNAP 8/15/02) 522 P5.57 (a) vs + R1 ia + ( d + 1) R 2 ia = 0 ia = v oc = vs R1 + ( d + 1) R 2 ( d + 1) R 2vs R1 + ( d + 1) R 2
ia = vs R1 i sc = ( d + 1) ia = ( d + 1) vs
R1 ia  d ia + vT  iT = 0 R2 R1 ia = vT
iT = ( d + 1) vT vT R 2 ( d + 1) + R1 + = vT R1 R 2 R1 R 2 Rt = (b) Let R1 = R2 = 1 k. Then 625 = R t = and 5 = voc = R1 R 2 vT = iT R1 + ( d + 1) R 2 1000 1000 d=  2 = 0.4 A/A 625 d +2 vs = 0.4 + 2 5 = 13.33 V 0.4 + 1 (checked using LNAP 8/15/02) ( d + 1) vs
d +2 523 P5.58 From the given data:
6= 2000 voc R t + 2000 voc = 1.2 V 4000 R t = 1600 voc 2= R t + 4000 When R = 8000 ,
v= R voc Rt + R v= 8000 (1.2 ) = 1.5 V 1600 + 8000 P5.59 From the given data:
0.004 = voc R t + 2000 voc = 24 V voc R t = 4000 0.003 = R t + 4000 i= voc Rt + R (a) When i = 0.002 A: 24 0.002 = R = 8000 4000 + R (b) Maximum i occurs when R = 0: 24 = 0.006 = 6 mA i 6 mA 4000 P5.510 The current at the point on the plot where v = 0 is the short circuit current, so isc = 20 mA. The voltage at the point on the plot where i = 0 is the open circuit voltage, so voc = 3 V. The slope of the plot is equal to the negative reciprocal of the Thevenin resistance, so 1 0  0.002  = R t = 150 Rt 3  0 524 P5.511
12 + 6000 ia + 2000 ia + 1000 ia = 0 ia = 4 3000 A voc = 1000 ia = 4 V 3 ia = 0 due to the short circuit
12 + 6000 isc = 0 isc = 2 mA 4 voc Rt = = 3 = 667 isc .002 4 3 ib = 667 + R ib = 0.002 A requires 4 3  667 = 0 R = 0.002 (checked using LNAP 8/15/02) 525 P5.512 10 = i + 0 i = 10 A voc + 4 i  2 i = 0 voc = 2 i = 20 V i + i sc = 10 i = 10  i sc 4 i + 0  2 i = 0 i = 0 i sc = 10 A Rt = voc 20 = = 2 isc 10 2 = iL = 20 RL = 12 RL  2 (checked using LNAP 8/15/02) 526 Section 56: Norton's Theorem P5.61 When the terminals of the boxes are opencircuited, no current flows in Box A, but the resistor in Box B dissipates 1 watt. Box B is therefore warmer than Box A. If you short the terminals of each box, the resistor in Box A will draw 1 amp and dissipate 1 watt. The resistor in Box B will be shorted, draw no current, and dissipate no power. Then Box A will warm up and Box B will cool off.
P5.62 (checked using LNAP 8/16/02) 527 P5.63 P5.64 To determine the value of the short circuit current, isc, we connect a short circuit across the terminals of the circuit and then calculate the value of the current in that short circuit. Figure (a) shows the circuit from Figure 5.64a after adding the short circuit and labeling the short circuit current. Also, the meshes have been identified and labeled in anticipation of writing mesh equations. Let i1 and i2 denote the mesh currents in meshes 1 and 2, respectively. In Figure (a), mesh current i2 is equal to the current in the short circuit. Consequently, i2 = isc . The controlling current of the CCVS is expressed in terms of the mesh currents as i a = i1  i 2 = i1  isc Apply KVL to mesh 1 to get 3 i1  2 ( i1  i 2 ) + 6 ( i1  i 2 )  10 = 0 7 i1  4 i 2 = 10 Apply KVL to mesh 2 to get 5 i 2  6 ( i1  i 2 ) = 0  6 i1 + 11 i 2 = 0 i1 = Substituting into equation 1 gives 11 7 i 2  4 i 2 = 10 i 2 = 1.13 A i sc = 1.13 A 6 11 i2 6
(1) 528 Figure (a) Calculating the short circuit current, isc, using mesh equations. To determine the value of the Thevenin resistance, Rt, first replace the 10 V voltage source by a 0 V voltage source, i.e. a short circuit. Next, connect a current source across the terminals of the circuit and then label the voltage across that current source as shown in Figure (b). The Thevenin resistance will be calculated from the current and voltage of the current source as v Rt = T iT In Figure (b), the meshes have been identified and labeled in anticipation of writing mesh equations. Let i1 and i2 denote the mesh currents in meshes 1 and 2, respectively. In Figure (b), mesh current i2 is equal to the negative of the current source current. Consequently, i2 = i T . The controlling current of the CCVS is expressed in terms of the mesh currents as i a = i1  i 2 = i1 + i T Apply KVL to mesh 1 to get 3 i1  2 ( i1  i 2 ) + 6 ( i1  i 2 ) = 0 7 i1  4 i 2 = 0 i1 = Apply KVL to mesh 2 to get 5 i 2 + vT  6 ( i1  i 2 ) = 0  6 i1 + 11 i 2 = vT Substituting for i1 using equation 2 gives 4 6 i 2 + 11 i 2 = vT 7 Finally, Rt = 7.57 i 2 = vT 4 i2 7
(2) vT vT vT = = = 7.57 iT iT i2 529 Figure (b) Calculating the Thevenin resistance, R t = vT , using mesh equations. iT To determine the value of the open circuit voltage, voc, we connect an open circuit across the terminals of the circuit and then calculate the value of the voltage across that open circuit. Figure (c) shows the circuit from Figure 4.64a after adding the open circuit and labeling the open circuit voltage. Also, the meshes have been identified and labeled in anticipation of writing mesh equations. Let i1 and i2 denote the mesh currents in meshes 1 and 2, respectively. In Figure (c), mesh current i2 is equal to the current in the open circuit. Consequently, i2 = 0 A . The controlling current of the CCVS is expressed in terms of the mesh currents as i a = i1  i 2 = i1  0 = i1 Apply KVL to mesh 1 to get 3 i1  2 ( i1  i 2 ) + 6 ( i1  i 2 )  10 = 0 3 i1  2 ( i1  0 ) + 6 ( i1  0 )  10 = 0 i1 = Apply KVL to mesh 2 to get 5 i 2 + voc  6 ( i1  i 2 ) = 0 voc = 6 ( i1 ) = 6 (1.43) = 8.58 V 10 = 1.43 A 7 Figure (c) Calculating the open circuit voltage, voc, using mesh equations. As a check, notice that R t isc = ( 7.57 )(1.13) = 8.55 voc (checked using LNAP 8/16/02) 530 P5.65 To determine the value of the short circuit current, Isc, we connect a short circuit across the terminals of the circuit and then calculate the value of the current in that short circuit. Figure (a) shows the circuit from Figure 4.65a after adding the short circuit and labeling the short circuit current. Also, the nodes have been identified and labeled in anticipation of writing node equations. Let v1, v2 and v3 denote the node voltages at nodes 1, 2 and 3, respectively. In Figure (a), node voltage v1 is equal to the negative of the voltage source voltage. Consequently, v1 = 24 V . The voltage at node 3 is equal to the voltage across a short, v3 = 0 . The controlling voltage of the VCCS, va, is equal to the node voltage at node 2, i.e. va = v2 . The voltage at node 3 is equal to the voltage across a short, i.e. v3 = 0 . Apply KCL at node 2 to get v1  v 2 3 = v 2  v3 6 2 v1 + v 3 = 3 v 2  48 = 3 v a v a = 16 V Apply KCL at node 3 to get v2  v3 6 + 4 v 2 = isc 3 9 v a = isc 6 isc = 9 ( 16 ) = 24 A 6 Figure (a) Calculating the short circuit current, Isc, using mesh equations. To determine the value of the Thevenin resistance, Rth, first replace the 24 V voltage source by a 0 V voltage source, i.e. a short circuit. Next, connect a current source circuit across the terminals of the circuit and then label the voltage across that current source as shown in Figure (b). The Thevenin resistance will be calculated from the current and voltage of the current source as v R th = T iT Also, the nodes have been identified and labeled in anticipation of writing node equations. Let v1, v2 and v3 denote the node voltages at nodes 1, 2 and 3, respectively. 531 In Figure (b), node voltage v1 is equal to the across a short circuit, i.e. v1 = 0 . The controlling voltage of the VCCS, va, is equal to the node voltage at node 2, i.e. va = v2 . The voltage at node 3 is equal to the voltage across the current source, i.e. v3 = vT . Apply KCL at node 2 to get v1  v 2 3 Apply KCL at node 3 to get
v2  v3 6 + 4 v 2 + iT = 0 9 v 2  v3 + 6 iT = 0 3 9 v a  vT + 6 iT = 0 3 v T  vT + 6 iT = 0 2 vT = 6 iT Finally, Rt = vT = 3 iT = v 2  v3 6 2 v1 + v 3 = 3 v 2 vT = 3 v a Figure (b) Calculating the Thevenin resistance, R th = vT , using mesh equations. iT To determine the value of the open circuit voltage, voc, we connect an open circuit across the terminals of the circuit and then calculate the value of the voltage across that open circuit. Figure (c) shows the circuit from Figure P 4.65a after adding the open circuit and labeling the open circuit voltage. Also, the nodes have been identified and labeled in anticipation of writing node equations. Let v1, v2 and v3 denote the node voltages at nodes 1, 2 and 3, respectively. In Figure (c), node voltage v1 is equal to the negative of the voltage source voltage. Consequently, v1 = 24 V . The controlling voltage of the VCCS, va, is equal to the node voltage at node 2, i.e. va = v2 . The voltage at node 3 is equal to the open circuit voltage, i.e. v3 = voc . Apply KCL at node 2 to get 532 v1  v 2 3 = v 2  v3 6 2 v1 + v 3 = 3 v 2  48 + v oc = 3 v a Apply KCL at node 3 to get v2  v3 6 + 4 v 2 = 0 9 v 2  v 3 = 0 9 v a = v oc 3 Combining these equations gives
3 ( 48 + voc ) = 9 v a = voc voc = 72 V Figure (c) Calculating the open circuit voltage, voc, using node equations. As a check, notice that R th I sc = ( 3)( 24 ) = 72 = Voc (checked using LNAP 8/16/02) Section 57: Maximum Power Transfer P5.71 a) For maximum power transfer, set RL equal to the Thevenin resistance: R L = R t = 100 + 1 = 101 b) To calculate the maximum power, first replace the circuit connected to RL be its Thevenin equivalent circuit: 533 The voltage across RL is Then vL =
pmax 101 (100 ) = 50 V 101 + 101 2 v 502 = L = = 24.75 W R L 101 P5.72 Reduce the circuit using source transformations: Then (a) maximum power will be dissipated in resistor R when: R = Rt = 60 and (b) the value of that maximum power is P = i 2 ( R) = (0.03)2 (60) = 54 mW max R 534 P5.73 RL v L = vS RS + R L 2 2 vL vS RL pL = = R L ( RS + R L )2 By inspection, pL is max when you reduce RS to get the smallest denominator. set RS = 0
P5.74 Find Rt by finding isc and voc: The current in the 3 resistor is zero because of the short circuit. Consequently, isc = 10 ix. Apply KCL at the topleft node to get ix + 0.9 = 10 ix so Next isc = 10 ix = 1A ix = 0.9 = 0.1 A 9 Apply KCL at the topleft node to get 535 ix + 0.9 = 10 ix Apply Ohm's law to the 3 resistor to get ix = 0.9 = 0.1 A 9 voc = 3 (10 ix ) = 30 ( 0.1) = 3 V For maximum power transfer to RL: R L = Rt = voc 3 = =3 isc 1 The maximum power delivered to RL is given by
pmax = voc 32 3 = = W 4 R t 4 ( 3) 4
2 P5.75 The required value of R is R = Rt = 8 + ( 20 + 120 ) (10 + 50 ) = 50 ( 20 + 120 ) + (10 + 50 ) 30 170 voc = ( 20 ) 10  170 + 30 ( 20 ) 50 170 + 30 170(20)(10)  30(20)(50) 4000 = = = 20 V 200 200 The maximum power is given by 2 v 202 pmax = oc = =2W 4 R t 4 ( 50 ) 536 PSpice Problems
SP51 a = 0.3333 b = 0.3333 c =33.33 V/A (a) vo = 0.3333 v1 + 0.3333 v2 + 33.33 i 3 18 3 = 3 = 30 mA i3 = 100 100 3 7 (b) 7 = 0.3333 (10 ) + 0.3333 ( 8 ) + 33.33 i 3 537 SP52 Before the source transformation: VOLTAGE SOURCE CURRENTS NAME CURRENT V_V1 V_V2 After the source transformation: 3.000E02 4.000E02 VOLTAGE SOURCE CURRENTS NAME CURRENT V_V2 4.000E02 538 SP53 voc = 2 V VOLTAGE SOURCE CURRENTS NAME CURRENT V_V3 V_V4 7.500E01 7.500E01 isc = 0.75 A Rt = 2.66 539 SP54 voc = 8.571 V VOLTAGE SOURCE CURRENTS NAME CURRENT V_V5 2.075E+00 V_V6 1.132E+00 X_H1.VH_H1 9.434E01 isc = 1.132 A Rt = 7.571 540 Verification Problems
VP51 Use the data in the first two lines of the table to determine voc and Rt:
voc Rt + 0 voc = 39.9 V voc R t = 410 0.0438 = R t + 500 0.0972 = Now check the third line of the table. When R= 5000 : v 39.9 i = oc = = 7.37 mA R t + R 410 + 5000 which disagree with the data in the table.
The data is not consistent. VP52 Use the data in the table to determine voc and isc: voc = 12 V (line 1 of the table)
isc = 3 mA so Rt = voc = 4 k isc (line 3 of the table) Next, check line 2 of the table. When R = 10 k: v 12 i = oc = = 0.857 mA 3 R t + R 10 (10 ) + 5 (103 ) To cause i = 1 mA requires which agrees with the data in the table. v 12 0.001 = i = oc = R = 8000 R t + R 10 (103 ) + R I agree with my lab partner's claim that R = 8000 causes i = 1 mA. 541 VP53 60 60 voc 11 i= = = 11 = 54.55 mA R t + R 6 110 + 40 60 + 40 ( ) 11 The measurement supports the prelab calculation. Design Problems
DP51 The equation of representing the straight line in Figure DP 51b is v =  R t i + voc . That is, the slope of the line is equal to 1 times the Thevenin resistance and the "v  intercept" is equal to the 05 open circuit voltage. Therefore: R t =  = 625 and voc = 5 V. 0.008  0 Try R1 = R 2 = 1 k . (R1  R2 must be smaller than Rt = 625 .) Then 5= and R1 R2 = R3 + 500 R3 = 125 R1 + R2 Now vs, R1, R2 and R3 have all been specified so the design is complete. 625 = R 3 + 1 vs = vs 2 R1 + R 2 R2 vs = 10 V DP52 The equation of representing the straight line in Figure DP 52b is v =  R t i + voc . That is, the slope of the line is equal to 1 times the Thevenin resistance and the "v  intercept" is equal to the 0  ( 3 ) = 500 and voc = 3 V. open circuit voltage. Therefore: R t =  0.006  0 From the circuit we calculate R 3 ( R1 + R 2 ) R1 R 3 and voc =  is Rt = R1 + R 2 + R 3 R1 + R 2 + R 3 so R 3 ( R1 + R 2 ) R1 R 3 500 = is and 3 V =  R1 + R 2 + R 3 R1 + R 2 + R 3 542 Try R 3 = 1k and R1 + R 2 = 1k . Then R t = 500 and i s 6 = R1 i s 2000 2 This equation can be satisfied by taking R1 = 600 and is = 10 mA. Finally, R2 = 1 k  400 = 400 . Now is, R1, R2 and R3 have all been specified so the design is complete. 3 =  1000 R1 is =  R1 DP53 The slope of the graph is positive so the Thevenin resistance is negative. This would require R1 R 2 R3 + < 0 , which is not possible since R1, R2 and R3 will all be nonnegative. R1 + R 2 Is it not possible to specify values of vs, R1, R2 and R3 that cause the current i and the voltage v in Figure DP 53a to satisfy the relationship described by the graph in Figure DP 53b. DP54 The equation of representing the straight line in Figure DP 54b is v =  R t i + voc . That is, the slope of the line is equal to the Thevenin impedance and the "v  intercept" is equal to the open 5  0 circuit voltage. Therefore: R t =  = 625 and voc = 5 V. 0  0.008 The open circuit voltage, voc, the short circuit current, isc, and the Thevenin resistance, Rt, of this circuit are given by R 2 ( d + 1) voc = vs R1 + ( d + 1) R 2 , ( d + 1) v isc = s R1 and R1 R 2 Rt = R1 + ( d + 1) R 2 Let R1 = R2 = 1 k. Then 625 = R t = and 5 = 1000 1000 d=  2 = 3.6 A/A d +2 625 vs = 3.6 + 2 (  5 ) = 3.077 V 3.6 + 1 ( d + 1) vs
d +2 Now vs, R1, R2 and d have all been specified so the design is complete. 543 Chapter 6: The Operational Amplifier
Exercises
Ex. 6.41 vs vs  vo + +0 = 0 R1 R2 vo R = 1+ 2 vs R1 Ex. 6.42 a)
va = R2 vs R1 + R2 va va  v0 + +0 =0 R3 R4 vo R = 1+ 4 va R3
b)
When R2 >> R1 then vo R2 R4 = 1 + vs R1 + R2 R3 R2 R vo R  2 = 1 and  1+ 4 R1 + R2 R2 vs R3 61 Ex. 6.51 vo vo  vs + +0= 0 R2 R1 vo R2 = vs R1 + R2 Ex. 6.61 R vin  vout vin + + 0 = 0 vout = 1 + f vin Rf R1 R1 when R f = 100 k and R1 = 25 k then 100 103 vout = 1 + = 5 vin 25 103 62 Ex. 6.71 R2 R1 10 103 10 103 v3 =  v v2 + 1 + 1 + 3 3 3 3 1 10 10 R 2 + 10 10 10 10 10 10 R2 R1 =  v + 2 1 + v 3 2 3 1 10 10 R 2 + 10 10 1 We require v3 = ( 4 ) v1  v2 , so 5 R1 3 4 = 2 1 + R1 = 10 10 = 10 k 10 103 and
R2 1 = 5 R 2 + 10 103 R 2 + 10 103 = 5 R 2 R 2 = 2.5 k 63 Ex. 6.72 As in Ex 6.71 R2 R1 v3 =  v + 2 1 + v 3 2 3 1 R 2 + 10 10 10 10 4 We require v3 = ( 6 ) v1  v2 , so 5 R1 3 6 = 2 1 + R1 = 20 10 = 20 k 10 103 and
R2 4 = 5 R 2 + 10 103 4 R 2 + 40 103 = 5 R 2 R 2 = 40 k Ex. 6.81 Analysis of the circuit in Section 6.7 showed that output offset voltage = 6 vos + (50 103 ) ib1 For a A741 op amp, vos 1 mV and ib1 80 nA so output offset voltage = 6 vos + (50 103 )ib1 6 (103 )+(50.103 )(80109 ) = 10 mV Ex. 6.82 vo =  R R2 vin + 1 + 2 vos + R2ib1 R1 R1 ib1 500 nA then
9 3 When R2 = 10 k, R1 = 2 k, vos 5 mV and output offset voltage 6 5 103 + 10 103 ( ) ( ) ( 500.10 ) 3510 = 35 mV 64 Ex. 6.83 Analysis of this circuit in Section 6.7 showed that output offset voltage = 6 vos + ( 50 103 ) ib1 For a typical OPA1O1AM, vos = 0.1 mV and ib = 0.012 nA so output offset voltage 6 0.1103 + ( 50 103 ) 0.012 109 3 6 3 0.6 10 + 0.6 10  0.6 10 = 0.6 mV
Ex. 6.84 Writing node equations
v  vs v  vo v + + =0 Ra Rb Ri + Rs R i v vo   A  R +R i s + vo  v = 0 R0 Rb After some algebra
Av = R0 ( Ri + Rs ) + ARi R f vo = vs ( R f + R0 ) ( Ri + Rs ) + Ra ( R f + R0 + Ri + Rs )  ARi Ra For the given values, Av = 2.00006 V/V. 65 Problems
Section 64: The Ideal Operational Amplifier P6.41 (checked using LNAP 8/16/02)
P6.42 Apply KVL to loop 1:  12 + 3000 i1 + 0 + 2000 i1 = 0 12 = 2.4 mA 5000 The currents into the inputs of an ideal op amp are zero so io = i1 = 2.4 mA i1 =
va = i2 (1000 ) + 0 = 2.4 V Apply Ohm's law to the 4 k resistor vo = va  io ( 4000 ) i2 =  i1 =  2.4 mA = 2.4  ( 2.4 103 ) ( 4000 ) = 12 V (checked using LNAP 8/16/02) 66 P6.43 The voltages at the input nodes of an ideal op amp are equal so va = 2 V . Apply KCL at node a: vo  ( 2 ) 12  ( 2 ) + = 0 vo = 30 V 8000 4000 Apply Ohm's law to the 8 k resistor
io = 2  vo = 3.5 mA 8000 (checked using LNAP 8/16/02)
P6.44 The voltages at the input nodes of an ideal op amp are equal so v = 5 V . Apply KCL at the inverting input node of the op amp: v 5 3  a  0.1 10  0 = 0 va = 4 V 10000 Apply Ohm's law to the 20 k resistor va 1 i = = mA 20000 5 (checked using LNAP 8/16/02)
P6.45 The voltages at the input nodes of an ideal op amp are equal so va = 0 V . Apply KCL at node a: v  0 12  0 3  o   2 10 = 0 3000 4000 vo =  15 V Apply KCL at the output node of the op amp: v v io + o + o = 0 io = 7.5 mA 6000 3000 (checked using LNAP 8/16/02) 67 P6.46 The currents into the inputs of an ideal op amp are zero and the voltages at the input nodes of an ideal op amp are equal so va = 2.5 V . Apply Ohm's law to the 4 k resistor: v 2.5 ia = a = = 0.625 mA 4000 4000 Apply KCL at node a: ib = ia = 0.625 mA Apply KVL: vo = 8000 ib + 4000 ia = (12 103 )( 0.625 103 ) = 7.5 V (checked using LNAP 8/16/02)
P6.47 R2 v  0 va  0 vs  s + 0 = 0 va =   R1 R1 R 2 io = R 2 + R3 R 2 + R3 0  va 0  va + = va = v R1 R 3 s R2 R3 R 2 R3 v  0 va  0 R4 R2 R4  o va = vs  + 0 = 0 vo =  R 4 R3 R3 R1 R 3 68 P6.48 The node voltages have been labeled using: 1. The currents into the inputs of an ideal op amp are zero and the voltages at the input nodes of an ideal op amp are equal. 2. KCL 3. Ohm's law Then v0 = 11.8  1.8 = 10 V and
io = 10 = 2.5 mA 4000 (checked using LNAP 8/16/02)
P6.49 KCL at node a: va  ( 18 ) v + a + 0 = 0 va = 12 V 4000 8000 The node voltages at the input nodes of ideal op amps are equal so vb = va . Voltage division:
vo = 8000 vb = 8 V 4000 + 8000 (check using LNAP 8/16/02) 69 Section 65: Nodal Analysis of Circuits Containing Ideal Operational Amplifiers P6.51 KCL at node b: vb  2 vb v +5 1 + + b = 0 vb =  V 20000 40000 40000 4 1 V. 4 The node voltages at the input nodes of an ideal op amp are equal so ve = vb =  KCL at node e:
ve v v 10 + e d = 0 vd = 10 ve =  V 1000 9000 4 (checked using LNAP 8/16/02)
P6.52 Apply KCL at node a:
0= va  12 v v 0 + a + a va = 4 V 6000 6000 6000 Apply KCL at the inverting input of the op amp:
v 0 0  vo  a +0+ = 0 6000 6000 vo = va = 4 V Apply KCL at the output of the op amp: vo 0  vo = 0 io  + 6000 6000 v io =  o = 1.33 mA 3000 (checked using LNAP 8/16/02) 610 P6.53 Apply KCL at the inverting input of the op amp: v  0 vs  0  a  = 0 R2 R1 R va =  2 vs R1 Apply KCL at node a: 1 1 1 va v0 va va  0 R R +R R +R R + + = 0 v0 = R4 + + va = 2 3 2 4 3 4 va R4 R3 R2 R2 R3 R4 R3 R2 =
Plug in values yields vo 30 + 900 + 30 = = 200 V/V 4.8 vs R2 R3 + R2 R4 + R3 R4 vs R1 R3 P6.54 Ohm's law:
i= v1  v2 R2 KVL:
v0 = ( R1 + R2 + R3 ) i = R1 + R2 + R3 ( v1  v2 ) R2 611 P6.55 R v1 va v1 v2 R + + 0 = 0 va = 1+ 1 v1  1 v2 R1 R7 R7 R7 R v2  vb v v R  1 2 + 0 = 0 vb = 1+ 2 v2  2 v1 R2 R7 R7 R7 v v v 0 R6  b c + c + 0 = 0 vc = vb R4 + R6 R4 R6 v v v v R R  a c + c 0 + 0 = 0 v0 =  5 va + (1+ 5 )vc R3 R3 R3 R5 R R R (R +R ) R R (R +R ) R R R v0 = 5 1 + 6 3 5 (1+ 2 ) v2  5 (1+ 1 ) + 6 3 5 2 v1 R7 R7 R3 ( R4 + R6 ) R7 R3 R7 R3 ( R4 + R6 ) R3 v v i0 = c 0 = R5 612 P6.56 KCL at node b: KCL at node a: So va vc 5 + = 0 vc =  va 3 3 20 10 25 10 4 5 va   va va  ( 12 ) va va + 0 4 = 0 v =  12 V + + + a 3 3 3 40 10 10 10 20 10 10 103 13 5 15 vc =  va =  . 4 13 613 P6.57 Apply KCL at the inverting input node of the op amp ( va + 6 )  0 v 0  a = 0 +0 10000 30000 va = 1.5 V Apply KCL to the super node corresponding the voltage source:
va 0 va + 6 0 + 10000 30000 ( v + 6 )vb = 0 v v + a b + a 30000 10000 3va + va + 6 + va  vb + 3 ( va + 6 ) vb = 0 vb = 2va + 6 = 3 V Apply KCL at node b: vb v  v v  v ( v + 6 )  vb + b 0  a b  a = 0 10000 30000 30000 10000 3vb +( vb  v0 )( va  vb )3( va + 6 )  vb = 0 v0 = 8vb  4va 18 = 12 V Apply KCL at the output node of the op amp:
i0 + v0 v v + 0 b = 0 i0 =  0.7 mA 30000 30000 614 P6.58 Apply KVL to the bottom mesh: i0 (10000)  i0 (20000) + 5 = 0 i0 = 1 mA 6 The node voltages at the input nodes of an ideal op amp are equal. Consequently
va = 10000 i0 = 10 V 6 Apply KCL at node a:
va v v + a 0 = 0 10000 20000 v0 = 3va = 5 V P6.59 KCL at node b: vb + 12 vb + = 0 vb = 4 V 40000 20000 The node voltages at the input nodes of an ideal op amp are equal, so vc = vb = 4 V . The node voltages at the input nodes of an ideal op amp are equal, so vd = vc + 0 10 4 = 4 V . KCL at node g:
vg v f  vg 2  + = 0 vg = v f 3 3 3 20 10 40 10 615 The node voltages at the input nodes of an ideal op amp are equal, so ve = vg = 2 vd  v f vd  3 v f vd  ve KCL at node d: 0 = + = + 20 103 20 103 20 103 20 103 vd  v f Finally, ve = vg =
P6.510
2 16 vf =  V. 3 5 2 vf . 3 6 24 V v f = vd =  5 5 By voltage division (or by applying KCL at node a)
va = R0 vs R1 + R0 Applying KCL at node b:
vb  vs vb v0 + = 0 R1 R0 +R R0 +R ( vb vs )+ vb = v0 R1 The node voltages at the input nodes of an ideal op amp are equal so vb = va . R +R R0 R +R R0 R R v0 = 0 +1  0 vs = vs vs =  R1 R1 + R0 R1 + R0 R0 R1 + R0 R1 616 Section 66: Design Using Operational Amplifier P6.61 Use the currenttovoltage converter, entry (g) in Figure 6.61. P6.62 Use the voltage controlled current source, entry (i) in Figure 6.61. P6.63 Use the noninverting summing amplifier, entry (e) in Figure 6.61. 617 P6.64 Use the difference amplifier, entry (f) in Figure 6.61. P6.65 Use the inverting amplifier and the summing amplifier, entries (a) and (d) in Figure 6.61. P6.66 Use the negative resistance converter, entry (h) in Figure 6.61. 618 P6.67 Use the noninverting amplifier, entry (b) in Figure 6.61. Notice that the ideal op amp forces the current iin to be zero. P6.68 Summing Amplifier: va =  ( 6 v1 + 2 v2 ) vo = 6 v1 + 2 v2 Inverting Amplifier: vo = va P6.69 619 Using superposition, vo = v1 + v2 + v3 = 9  16 + 32 = 7 V
P6.610 R1 R2 vo/vs R1 R2 vo/vs 6 121224 0.8 1212 624 0.8 12 61224 0.286 1224 612 0.5 24 61212 0.125 61212 24 8 612 1224 2 61224 12 3.5 624 1212 1.25 121224 6 1.25 620 Section 67: Operational Amplifier Circuits and Linear Algebraic Equations P6.71 621 P6.72 622 Section 68: Characteristics of the Practical Operational Amplifier P6.81 The node equation at node a is: Solving for vout: vout  vos vos = + ib1 3 10010 10103 100103 3 3 vout = 1+ vos + (100 10 ) ib1 = 11vos + (100 10 ) ib1 10103 = 11 ( 0.03103 )+(100103 ) 1.2109 = 0.45 mV ( ) P6.82 The node equation at node a is: Solving for vo: vos v v + ib1 = 0 os 10000 90000 90103 vo = 1+ v + ( 90 103 ) ib1 = 10 vos + ( 90 103 ) i b1 3 os 1010 = 10(5 103 )+ ( 90 103 ) (.05 109 ) = 50.0045 103  50 mV 623 P6.83 v1 vin v1 v1 v0 + + = 0 R1 Rin R2 v0 Rin ( R0  AR2 ) = v0 + Av1 v0  v1 vin ( R1 + Rin )( R0 + R2 ) + R1 Rin (1+ A) + =0 R0 R2 P6.84 a) v0 R 49103 =  2 =  = 9.6078 vin R1 5.1103 b) ( 2106 ) 75( 200,000)( 50103 ) v0 = = 9.9957 vin (5103 + 2106 )(75+50103 ) + (5103 )(2106 )(1+ 200,000)
v0 2106 (75 (200,000)(49103 )) = = 9.6037 vin (5.1103 +2106 )(75+49103 )+(5.1103 )(2106 )(1+200,000) ( ) c) 624 P6.85 Apply KCL at node b: R3 vb = (vcm  v p ) R2 + R3 Apply KCL at node a: va v0 va (vcm + vn ) + = 0 R4 R1 The voltages at the input nodes of an ideal op amp are equal so va = vb . R R +R v0 =  4 (vcm + vn ) + 4 1 va R1 R1 R v0 =  4 (vcm + vn ) + R1
( R4 + R1 ) R3 (vcm  v p ) R1 ( R2 + R3 )
when so v0 =  R4 R R (vcm + vn ) + 4 (vcm  v p ) =  4 (vn + v p ) R1 R1 R1 R4 R1 R4 +1 ( R4 + R1 ) R3 R3 R R R1 then = = 3 = 4 R3 R2 R1 ( R2 + R3 ) R1 +1 R2 R2 625 PSpice Problems
SP61: (a) v z = a vw + b v x + c v y The following three PSpice simulations show 1 V = vz = a when vw= 1 V, vx = 0 V and vy = 0 V 4 V = vz = b when vw= 0 V, vx = 1 V and vy = 0 V 5 V = vz = c when vw= 0 V, vx = 0 V and vy = 1 V Therefore (b) When vw= 2 V:
v z = vw + 4 v x  5 v y vz = 4 vx  5 v y + 2 1 V = vz = a when vw= 1 V, vx = 0 V and vy = 0 V: 626 4 V = vz = b when vw= 0 V, vx = 1 V and vy = 0 V: 5 V = vz = c when vw= 0 V, vx = 0 V and vy = 1 V: 627 SP62 a) Using superposition and recognizing the inverting and noninverting amplifiers: vo =  80 80 vs + 1 + ( 2 ) = 3.2 vs  8.4 25 25 b) Using the DC Sweep feature of PSpice produces the plot show below. Two points have been labeled in anticipation of c). c) Notice that the equation predicts ( 3.2 ) ( 5 )  8.4 = 7.6
and ( 3.2 ) ( 0 )  8.4 = 8.4 Both agree with labeled points on the plot. 628 SP63 VOLTAGE SOURCE CURRENTS NAME CURRENT V_V1 V_V2 3.000E04 7.000E04 v34 = 1.5  12 106 1.5 V v23 = 4.5  ( 1.5 ) = 6 V v50 = 12  0 = 12 V io = 7 104 = 0.7 mA 629 SP64 V4 is a short circuit used to measure io. The input of the VCCS is the voltage of the lefthand voltage source. (The nominal value of the input is 20 mV.) The output of the VCCS is io. A plot of the output of the VCCS versus the input is shown below. The gain of the VCVS is gain = 1 A = 103 V 100 10  ( 100 10 ) 2
3 3 50 106  ( 50 106 ) (The op amp saturates for the inputs larger than 0.1 V, limiting the operating range of this VCCS.) 630 Verification Problems
VP61 Apply KCL at the output node of the op amp io = v  ( 5 ) vo + o =0 10000 4000 Try the given values: io =1 mA and vo = 7 V 1103 3.7 103 = 7  ( 5 ) 7 + 10000 4000 KCL is not satisfied. These cannot be the correct values of io and vo. VP62 va = ( 4 103 )( 2 103 ) = 8 V vo =  12 103 va = 1.2 ( 8 ) = 9.6 V 10 103 So vo = 9.6 V instead of 9.6 V. 631 VP63 First, redraw the circuit as: Then using superposition, and recognizing of the inverting and noninverting amplifiers: 6 4 4 vo =   ( 3) + 1 + ( 2 ) = 18 + 6 = 12 V 2 2 2 The given answer is correct. VP64 First notice that ve = v f = vc is required by the ideal op amp. (There is zero current into the input lead of an ideal op amp so there is zero current in the 10 k connected between nodes e and f, hence zero volts across this resistor. Also, the node voltages at the input nodes of an ideal op amp are equal.) The given voltages satisfy all the node equations at nodes b, c and d: node b:
0 (5) 0 0 2 + + =0 10000 40000 4000 0 2 2 5 = +0 4000 6000 2 5 5 511 = + 6000 5000 4000 node c: node d: Therefore, the analysis is correct. 632 VP65 The given voltages satisfy the node equations at nodes b and e: node b: .25 2 .25 .25( 5 ) + + =0 20000 40000 40000 2.5( 0.25 ) 0.25 +0 9000 1000 node e: Therefore, the analysis is not correct. Notice that 2.5( +0.25 ) +0.25 = +0 9000 1000 So it appears that ve = +0.25 V instead of ve = 0.25 V. Also, the circuit is an noninverting summer with Ra = 10 k and Rb = 1 k, K1 =1/ 2, K2 = 1/ 4 and K4 = 9. The given node voltages satisfy the equation 2.5 = vd = K 4 ( K v + K v ) = 10 1 ( 2 )+ 1 ( 5) 4 2 1 a 2 c Nonetheless, the analysis is not correct. 633 Design Problems
DP61 From Figure 6.61g, this circuit is described by vo = R f i in . Since i out =
Notice that i oa = i in + i in < (1250 ) i in
5000 Rf vo 1 i out , we require = = , or Rf = 1250 5000 4 i in 5000 = 5 5 i in . To avoid current saturation requires i in < i sat or 4 4 4 i sat . For example, if isat = 2 mA, then iin < 1.6 mA is required to avoid current saturation. 5 DP62 3 3 3 3 12 3 12 vo =  vi + 3 =  vi + 1 + 5  vi + 1 + 5 4 4 4 4 35 4 12 + 23 634 DP63 1 1 1 1 (a) 12 v i + 6 = 24 v i + ( 5 ) K 4 = 24, K 1 = , and K 2 = . Take Ra = 18 k and 20 2 20 2 Rb = 1 k to get (b) (c) (d) 635 DP64 636 DP65 We require a gain of 4 = 200 . Using an inverting amplifier: 20 103 Here we have 200 =  R2 10 103 + R1 . For example, let R1 = 0 and R2 = 1 M. Next, using the noninverting amplifier: Here we have 200 = 1 + R2 R1 . For example, let R1 = 1 k and R2 = 199 k. The gain of the inverting amplifier circuit does not depend on the resistance of the microphone. Consequently, the gain does not change when the microphone resistance changes. 637 Chapter 7 Energy Storage Elements
Exercises
Ex. 7.31
2 2<t <4 d and i C ( t ) = 1 v s ( t ) = 1 4 < t < 8 dt 0 otherwise 2 t  2 2 < t < 4 so i (t ) = i C ( t ) + i R ( t ) = 7  t 4<t <8 0 otherwise 2 t  4 2 < t < 4 i R (t ) = 1 v s (t ) = 8  t 4<t <8 0 otherwise Ex. 7.32 1 t 1 t v(t ) = i s ( ) d + v(t 0 ) = i s ( ) d  12 1 0 C t0 3
v(t ) = 3 4 d  12 = 12 t  12 for 0 < t < 4
0 t t In particular, v(4) = 36 V. In particular, v(10) = 0 V. v(t ) = 3 ( 2 ) d + 36 = 60  6 t for 4 < t < 10
4 v(t ) = 3 0 d + 0 = 0 for 10 < t
10 t Ex. 7.41 W = Cv 2 1 2 = ( 210 4 ) (100 ) = 1 J 2 2 +  vc ( 0 ) = vc ( 0 ) = 100 V 71 Ex. 7.42 a) W ( t ) = W ( 0 ) + 0 vi dt
t First, W ( 0 ) = 0 since v ( 0 ) = 0 Next, v( t ) = v( 0 ) + W (t ) =
t 0 W (1s ) = 2 104 J = 20 kJ
b)
W (100s ) = 2 104 (100 )
2 ( 210 ) t ( 2 )dt
4 1 t 4 t 4 0 i dt = 10 0 2 dt = 210 t C = 2 104 t 2 = 2 108 J = 200 MJ Ex. 7.43
We have v (0+ ) = v (0 ) = 3 V vc ( t ) =
t 1 t 5t 5t 5t 0 i(t ) dt + vc (0) = 5 0 3 e dt + 3 = 3 ( e 1)+3 = 3 e V, 0<t <1 C a) b) v(t ) = vR ( t ) + vc ( t ) = 5 i ( t ) + vc ( t ) = 15 e5t + 3 e5t = 18 e5t V, 0 < t < 1 W (t ) t =0.2 s = 6.65 J 2 W ( t ) = 1 Cvc2 ( t ) = 1 0.2 ( 3e5t ) = 0.9e10t J 2 2 W ( t ) t =0.8 s = 2.68 kJ Ex. 7.51 72 Ex. 7.52 v1 = v2 dv1 dv2 i i C = 1 = 2 i1 = 1 i2 dt dt C1 C2 C2 C KCL: i = i1 + i2 = 1 + 1 i2 C2 i2 = C2 i C1 +C2 Ex. 7.53 (a) to (b) : 1 1 = mF , 1 1 1 9 + + 1 1 1 3 3 3 (b) to (c) : 1+ 1 10 = mF , 9 9 (c) to (d) : 1 1 1 1 = + + 2 2 10 Ceq 9 Ceq = 10 mF 19 73 Ex. 7.61 2 2<t <4 d and v L ( t ) = 1 i s ( t ) = 1 4 < t < 8 dt 0 otherwise 2 t  2 2 < t < 4 so v(t ) = v L ( t ) + v R ( t ) = 7  t 4<t <8 0 otherwise 2 t  4 2 < t < 4 4<t <8 v R (t ) = 1 is (t ) = 8  t 0 otherwise Ex. 7.62 i (t ) = 1 t 1 t t 0 v s ( ) d + i(t 0 ) = 1 0 v s ( ) d  12 L 3
t i (t ) = 3 4 d  12 = 12 t  12 for 0 < t < 4
0 In particular, i(4) = 36 A. i (t ) = 3 ( 2 ) d + 36 = 60  6 t for 4 < t < 10
4 t In particular, i(10) = 0 A. i (t ) = 3 0 d + 0 = 0 for 10 < t
10 t Ex. 7.71 v = L P = vi = (1t ) e t ( 4 t e t ) = 4 t (1t ) e 2t W 2 1 11 W = Li 2 = ( 4 t e t ) = 2 t 2 e  2t J 2 24 di 1 d = ( 4 t et ) = (1t ) et V dt 4 dt 74 v (t ) = L di 1 di = dt 2 dt 0 2t and i ( t ) = 2( t  2 ) 0 Ex. 7.72 t <0 0 0<t <1 1 v( t ) = 1<t < 2 1 0 t >2 t <0 0<t <1 1<t < 2 t >2 p (t ) = v (t ) i (t ) t <0 0 2t 0<t <1 = 2( t  2 ) 1<t < 2 0 t >2 W ( t ) = W ( t0 ) + tt p( t ) dt
0 i (t ) = 0 for t < 0 p ( t ) = 0 for t < 0 W ( t0 ) = 0 2 t dt = t 1<t < 2 : W ( t ) = W (1)+ 2 ( t  2 ) dt = t
2 0 t 0 < t < 1: W ( t ) = t 2 t >2 : W (t ) = W ( 2) = 0 1  4t + 4 Ex. 7.81 75 Ex. 7.82 Ex. 7.83
i1 = 1 t v dt + i1 ( t0 ) , L1 t 0 i2 = 1 t v dt + i 2 ( t0 ) L 2 t0 but i1 ( t0 ) = 0 and i 2 ( t0 ) = 0 1 1 t 1 t 1 t t t v dt + t v dt = + v dt t v dt = L1 0 LP t 0 0 L1 L2 0 1 t 1 t v dt i L2 L 0 L1 1 = 1 = = 1 t 1 1 i L1 + L2 + t v dt LP 0 L1 L2 i = i1 + i2 = 76 Problems
Section 73: Capacitors P7.31 v (t ) = v (0) + 1 t i ( ) d C 0 and q = Cv In our case, the current is constant so Cv ( t ) = Cv ( 0 ) + i t i ( ) d .
0 t 6 6 q Cv( 0 ) 15010 (1510 )( 5 ) t= = = 3 ms i 25103 P7.32
i (t ) = C d 1d 1 v (t ) = 12 cos ( 2t + 30 ) = (12 )( 2 ) sin ( 2t + 30 ) = 3cos ( 2t + 120 ) A dt 8 dt 8 P7.33
d ( 310 ) cos ( 500t + 45 ) = C dt
3 12 cos ( 500t  45 ) = C (12 )( 500 ) sin ( 500t  45 ) = C ( 6000 ) cos ( 500t + 45 ) so 3103 1 1 = 106 = F C= 3 610 2 2 77 P7.34 v (t ) = 1 t 1 0 i ( ) d + v ( 0 ) = 2 1012 C i ( ) d  10
0 t 3 0 < t < 2 109 2 109 < t < 3 109 is ( t ) = 0 v ( t ) =
is ( t ) = 4 106 A 1 2 1012 0 d  10
0 t 3 = 103 t 1 4 106 ) d  103 = 5 103 + ( 2 106 ) t 12 2ns ( 2 10 In particular, v ( 3 109 ) = 5 103 + ( 2 106 ) ( 3 109 ) = 103 v (t ) = 3 109 < t < 5 109 is ( t ) = 2 106 A
t 1 2 106 ) d + 103 = 4 103  (106 ) t 12 3ns ( 2 10 In particular, v ( 5 109 ) = 4 103  (106 ) ( 5 109 ) = 103 V v (t ) = 5 109 < t is ( t ) = 0 v ( t ) = 1 2 1012 t 5ns 0 d  103 = 103 V P7.35 (b) (a) 0 0 < t <1 d 4 1< t < 2 i (t ) = C v(t ) = dt 4 2 < t < 3 0 3<t t 1 t v ( t ) = i ( ) d + v ( 0 ) = i ( ) d 0 C 0 For 0 < t < 1, i(t) = 0 A so
t v ( t ) = 0 d + 0 = 0 V
0 t For 1 < t < 2, i(t) = (4t  4) A so v ( t ) = ( 4  4 ) d + 0 = 2 2  4
1 ( v(2) = 2 22  4 ( 2 ) + 2 = 2 V . For 2 < t < 3, i(t) = (4t + 12) A so v ( t ) = ( 4 + 12 ) d + 2 = 2 2 + 12
2 t ( ) ) 1=2 t t 2  4t + 2 V ( v(3) = 2 32 + 12 ( 3)  14 = 4 V For 3 < t, i(t) = 0 A so v ( t ) = 0 d + 4 = 4 V
0 t ( ) ) 1 +2= ( 2 t t 2 + 12 t  14 V ) 78 P7.36 (a) (b) 0 0<t <2 d i (t ) = C v(t ) = 0.1 2 < t < 6 dt 0 6<t t 1 t v ( t ) = i ( ) d + v ( 0 ) = 2 i ( ) d 0 C 0 For 0 < t < 2, i(t) = 0 A so v ( t ) = 2 0 d + 0 = 0 V
0 t For 2 < t < 6, i(t) = 0.2 t  0.4 V so v ( t ) = 2 ( 0.2  0.4 ) d + 0 = 0.2 2  0.8
1 t ( v(6) = 0.2 62  0.8 ( 6 ) + 0.8 = 3.2 V . For 6 < t, i(t) = 0.8 A so v ( t ) = 2 0.8 d + 3.2 = 1.6 t  6.4 V
6 t ( ) ) 2 =0.2 t t 2  0.8 t + 0.8 V P7.37 v (t ) = v ( 0) + 1 t 4 t 3 6 0 i( ) d = 25 + 2.5 10 0 ( 610 ) e d C = 25 + 150 0 e 6 d 1 = 2 5 + 150  e 6 = 50  25e6t V 6 0
t t P7.38 iR = v 1 = (1 2e2t ) 103 = 25 (1 2e 2t ) A 3 20010 40 dv iC = C = 10106 ( 2 ) ( 10 e2t ) = 200 e2 t A dt i = iR + i C = 200 e2t + 25  50 e 2t ( ) = 25 + 150e 2t A 79 Section 74: Energy Storage in a Capacitor P7.41 Given
0 t<2 i ( t ) = 0.2 ( t  2 ) 2 < t < 6 0.8 t >6 The capacitor voltage is given by v (t ) = For t < 2
t 1 t i ( ) d + v ( 0 ) = 2 i ( ) d + v ( 0 ) 0 0.5 0 v ( t ) = 2 0 d + 0 = 0
0 t In particular, v ( 2 ) = 0. For 2 < t < 6
v ( t ) = 2 2 (  2 ) d + 0 = ( 0.2 2  0.8 ) = ( 0.2 t 2  0.8 t + 0.8 ) V = 0.2 ( t 2  4 t + 4 ) V
t t 2 2 In particular, v ( 6 ) = 3.2 V. For 6 < t v ( t ) = 2 0.8 d + 3.2 = 1.6 2 + 3.2 = (1.6 t  6.4 ) V = 1.6 ( t  4 ) V
t 6 t Now the power and energy are calculated as
0 2 p ( t ) = v ( t ) i ( t ) = 0.04 ( t  2 ) 1.28 ( t  4 ) t<2 2<t <6 6<t and
W (t ) = t 0 0 t<2 4 2<t<6 p ( ) d = 0.01( t  2 ) 2 6<t 0.8 ( t  4 )  0.64 710 711 These plots were produced using three MATLAB scripts: capvol.m function v = CapVol(t) if t<2 v = 0; elseif t<6 v = 0.2*t*t  .8*t +.8; else v = 1.6*t  6.4; end function i = CapCur(t) if t<2 i=0; elseif t<6 i=.2*t  .4; else i =.8; end t=0:1:8; for k=1:1:length(t) i(k)=CapCur(k1); v(k)=CapVol(k1); p(k)=i(k)*v(k); w(k)=0.5*v(k)*v(k); end plot(t,i,t,v,t,p) text(5,3.6,'v(t), V') text(6,1.2,'i(t), A') text(6.9,3.4,'p(t), W') title('Capacitor Current, Voltage and Power') xlabel('time, s') % plot(t,w) % title('Energy Stored in the Capacitor, J') % xlabel('time, s') capcur.m c7s4p1.m 712 P7.42 ic ( 0 ) = 0.2 A dv = (10106 ) ( 5 )( 4000 ) e 4000t = 0.2e4000t A 19 dt ic (10ms ) = 8.510 A 1 W ( t ) = Cv 2 ( t ) and v ( 0 ) = 5  5e0 = 0 W ( 0 ) = 0 2 3 v (1010 ) = 5  5 e 40 = 5  21.2 1018 5 W (10 ) = 1.25104 J ic = C P7.43 i (t ) = C dvc so read off slope of vc (t ) to get i (t ) dt p (t ) = vc (t ) i (t ) so multiply vc (t ) & i(t ) curves to get p (t ) P7.44 vc ( t ) = vc ( 0 ) + 1 t 1 t 0 i d = vc ( 0 ) + 2 0 50 cos10t + 6 d = C 5 Now since vc ( t )ave = 0 vc ( 0 )  sin = 0 vc ( t ) 2 6 Wmax ( 210 ) ( 2.5) = 6.25 J 1 = C v2 = c max 2 2
6 2 5 5 vc ( 0 )  2 sin 6 + 2 s in 10t + 6 5 = sin 10t + V 2 6 First nonnegative t for max energy occurs when: 10t + 6 = 2 t = 30 = 0.1047 s 713 P7.45 Max. charge on capacitor = C v = (10106 ) ( 6 ) = 60 C q 60106 = = 6 sec to charge i 10106 1 1 2 stored energy = W = C v 2 = (10106 ) ( 6 ) =180 J 2 2 t = Section 75: Series and Parallel capacitors P7.51 2 F 4 F = 6 F 6 F in series with 3 F = i (t ) = 2 F 6 F3 F = 2 F 6 F+3 F d (6 cos100t ) = (2106 ) (6) (100) ( sin100t ) A = 1.2 sin100t mA dt
4 F4 F = 2 F 4 F+4 F P7.52
4 F in series with 4 F = 2 F 2 F = 4 F 4 F in series with 4 F = 2 F i (t ) =(2106 ) d (5+ 3 e 250t ) = (2106 ) (0+ 3(250) e 250t ) A = 1.5 e 250t mA dt P7.53 C in series with C = C C C 5 = C 2 2 C C C = C +C 2 C 5 C 5 5 2 C in series with C = = C 5C 2 7 C+ 2 5 d 5 (25103 ) cos 250t = C (14sin 250t ) = C (14)(250) cos 250t 7 dt 7 so 25103 = 2500 C C = 10106 = 10 F 714 Section 76: Inductors P7.61
di = 2 0 0 [1 0 0 ( 4 0 0 ) c o s 4 0 0 t ] V dt 8 1 0 6 V = 4 1 0 6 V v m ax = 8 1 0 6 V th u s h a ve a fie ld o f m m 2 6 w h ic h e x ce e d s d ie le c tric stre n g th in a ir o f 3 1 0 V /m W e g e t a d isc h a rg e a s th e a ir is io n iz e d . F in d m a x . v o ltag e a c ro ss c o il: v (t ) = L P7.62 v=L
P7.63 di + R i = (.1) (4e t  4te t ) + 10(4te t ) = 0.4 e  t + 39.6t e  t V dt (a) 0 0 < t <1 4 1< t < 2 d v(t ) = L i (t ) = dt 4 2 < t < 3 3<t 0 i (t ) = For 0 < t < 1, v(t) = 0 V so
t 1 t v ( ) d + i ( 0 ) = v ( ) d 0 L 0 (b) i ( t ) = 0 d + 0 = 0 A
0 t i (2) = 4 ( 22 )  4 ( 2 ) + 2 = 2 A For 1 < t < 2, v(t) = (4t  4) V so t t i ( t ) = ( 4  4 ) d + 0 = ( 2 2  4 ) =2 t 2  4 t + 2 A 0 1 For 2 < t < 3, v(t) = 4t + 12 V so
t t i ( t ) = ( 4 + 12 ) d + 2 = ( 2 2 + 12 ) +2= ( 2 t 2 + 12 t  14 ) A 2 2 i (3) = 2 ( 32 ) + 12 ( 3)  14 = 4 A
t 3 For 3 < t, v(t) = 0 V so i ( t ) = 0 d + 4 = 4 A 715 P7.64
v (t ) = (250 10 3 ) d (120 10 3 ) sin(500t  30 ) = (0.25)(0.12)(500) cos(500 t  30 ) dt = 15 cos(500t  30 ) P7.65
iL (t ) = for 1 5 103 1 5103 v ( ) d
0 s t t  2 106 0< t < 1 s vs (t ) = 4 mV 4103 6 6 4 103 d  2106 = t  210 = 0.8 210 A 0 5103 iL (t ) = 4103 6 iL (1s) = 1106 )  2106 =  106 A =1.2 A 3 ( 5 510 for 1 s <t < 3 s vs (t ) = 1 mV
t 1 6 1103 6 1103 ) d  106 = (t 1106 )  106 =( 0.2 t 106 ) A 3 1 s ( 3 510 5 510 5 1103 iL ( 3 s ) =  + 3106  1106 = 1.6 A 3 510 iL (t ) = for 3 s < t vs (t ) = 0 so iL (t ) remains  1.6 A 716 P7.66
v(t ) = ( 2 10 ) i
3 s (t ) + d ( 4 10 ) dt
3 is (t ) (in general) for 0<t <1 s v(t ) = (2103 )(1103 ) t + 4103 (1103 ) = ( 2106 t + 4 ) V for 1 s <t < 3 s is (t ) = 1 mA d is (t ) = 0 dt v(t ) = (2103 )(1103 ) + ( 4103 )0 = 2 V d 1103 =103 is (t ) =  6 dt 110 1103 d is (t ) = (1) t = 103 t is (t ) = 1103 6 dt 110 1103 t for 3 s< t < 5 s is (t ) = 4103  6 110 v(t ) = ( 2103 )( 4103 103 t )+ 4103 ( 103 ) = 4  ( 2106 ) t is (t ) = 1103 and d is (t ) = 0 dt when 5 s <t< 7 s v(t ) = ( 2103 )(103 ) =  2 V 1103 d when 7 s< t < 8 s is (t ) = t  8103 is (t ) = 1103 6 dt 110 d is (t ) = 0 dt v(t ) = ( 2 103 )(103 t  8 103 ) + ( 4 103 )(103 ) = 12 + ( 2 106 ) t when 8 s < t , then is (t ) = 0 v(t )= 0 P7.68 (a) (b) 0 0<t <2 d v(t ) = L i (t ) = 0.1 2 < t < 6 dt 0 6<t t 1 t i ( t ) = v ( ) d + i ( 0 ) = 2 v ( ) d 0 L 0 For 0 < t < 2, v(t) = 0 V so i ( t ) = 2 0 d + 0 = 0 A
0 t For 2 < t < 6, v(t) = 0.2 t  0.4 V so
t t i ( t ) = 2 ( 0.2  0.4 ) d + 0 = ( 0.2 2  0.8 ) =0.2 t 2  0.8 t + 0.8 A 2 2 i (6) = 0.2 62  0.8 ( 6 ) + 0.8 = 3.2 A . ( ) For 6 < t, v(t) = 0.8 V so
717 i ( t ) = 2 0.8 d + 3.2 = (1.6 t  6.4 ) A
6 t Section 77: Energy Storage in an Inductor P7.71 t<0 0 d v( t ) =10010 i ( t ) = 0.4 0 t 1 dt 0 t>1 t <0 0 p( t ) =v( t ) i( t ) = 1.6t 0t 1 0 t >1 3 W (t ) = t 0 0 p ( ) d = 0.8t 2 0.8 t <0 0<t <1 t >1 718 P7.72 d p (t ) = v (t ) i (t ) = 5 (4sin 2t ) (4sin 2t ) dt = 5 (8cos 2t ) (4sin 2t ) = 80 [2 cos 2t sin 2t ] = 80 [sin(2t + 2t ) + sin(2t  2t )] = 80 sin 4t W t t 80 W(t ) = p( ) d = 80 sin4 d =  [cos 4 t0 ] = 20 (1  cos 4t ) 0 0 4 P7.73
t 1 6 cos 100 d + 0 25103 0 6 t [sin 100  0 ] = 2.4sin100 t = 3 (2510 )(100) p(t ) = v(t ) i(t ) = (6 cos100 t )(2.4 sin100t ) i(t ) = = 7.2 [ 2(cos100 t )(sin100 t ) ] = 7.2 [sin 200 t + sin 0] = 7.2 sin 200 t W (t ) = 0 p ( ) d = 7.2 0 sin 200 d
7.2 cos 200 t0 200 = 0.036[1  cos 200t ] J = 36 [1  cos 200t ] mJ = t t Section 78: Series and Parallel Inductors P7.81 63 = 2 H and 2 H + 2 H = 4 H 6+3 1 t 6 sin100  t0 = 0.015sin100 t A = 15sin100 t mA i (t ) = 0 6 cos100 d = 4 4100 6H 3H = P7.82
4 mH + 4 mH = 8 mH , 8mH 8mH = (810 )(810 )
3 3 8103 +8103 = 4 mH and 4 mH + 4 mH = 8 mH d v(t ) = (8103 ) (5+ 3e 250t ) = (8103 ) (0+ 3(250) e 250t ) =6 e 250t V dt 719 P7.83 L L L L 5 L = and L + L + = L+ L 2 2 2 5 d 25cos 250 t = L (14103 ) sin 250 t = 5 L (14103 )(250) cos 250 t 2 dt 2 25 so L = = 2.86 H 5 3 (1410 ) (250) 2 L L = ( ) Section 79: Initial Conditions of Switched Circuits P7.91 Then Next i L ( 0+ ) = i L ( 0 ) = 0 and v C ( 0+ ) = v C ( 0 ) = 12 V 720 P7.92 Then Next i L ( 0+ ) = i L ( 0 ) = 1 mA and v C ( 0+ ) = v C ( 0 ) = 6 V P7.93 Then Next i L ( 0+ ) = i L ( 0 ) = 0 and v C ( 0+ ) = v C ( 0 ) = 0 V 721 P7.94 at t = 0 KVL:  vc (0 ) + 32  15 = 0 vc (0 ) = vc (0+ ) =17 V at t = 0+ Apply KCL to supernode shown above: 15  9 15 ic ( 0+ ) +  + 0.003 = 0 ic ( 0+ ) = 6 mA 4000 5000 Then ic ( 0+ ) 6 103 dvc V = = = 3000 6 2 10 s dt t =0+ C 722 Section 710: Operational amplifier Circuits and Linear Differential Equations P7.101 P7.102 723 P7.103 P7.104 724 Verification Problems
VP71 We need to check the values of the inductor current at the ends of the intervals. 1 ? + 0.065 = 0.025 ( Yes!) at t = 1 0.025 =  25
at t = 3  3 ? 3  0.115 + 0.065 = 25 50 0.055 = 0.055 at t = 9 9 ?  0.115 = 0.065 50 ( Yes!) 0.065 = 0.065 ( Yes!) The given equations for the inductor current describe a current that is continuous, as must be the case since the given inductor voltage is bounded. VP72 We need to check the values of the inductor current at the ends of the intervals. 1 1 ? + 0.025 =  + 0.03 ( Yes!) at t = 1  200 100
4 ? 4  0.03 ( No!) + 0.03 = 100 100 The equation for the inductor current indicates that this current changes instantaneously at t = 4s. This equation cannot be correct. at t = 4  Design Problems
DP71 i (t ) d = 0.5 F . v ( t ) = 6 e 3t is proportional to i(t) so the element is a capacitor. C = d dt v (t ) dt v (t ) d = 0.5 H . b) i ( t ) = 6 e 3t is proportional to v(t) so the element is an inductor. L = d dt i (t ) dt v (t ) c) v(t) is proportional to i(t) so the element is a resistor. R = = 2 . i (t ) a) 725 DP72
1.131cos ( 2t + 45 ) = 1.131 cos ( 45 ) cos ( 2t )  sin ( 45 ) sin ( 2t ) = 0.8 cos 2 t  0.8 sin 2 t The first term is proportional to the voltage. Associate it with the resistor. The noticing that t  v ( ) d = 4 cos 2 t d = 2 sin 2t
 t d d v ( t ) = 4 cos 2 t = 8 sin 2 t dt dt associate the second term with a capacitor to get the minus sign. Then 4 cos 2 t 4 cos 2 t R= = = 5 and i1 (t ) 0.8 cos 2 t 0.8 sin 2 t i2 (t ) = = 0.1 F C= d 8 sin 2 t 4 cos 2 t dt 1.131cos ( 2t  45 ) = 1.131 cos ( 45 ) cos ( 2t )  sin ( 45 ) sin ( 2t ) = 0.8 cos 2 t + 0.8 sin 2 t The first term is proportional to the voltage. Associate it with the resistor. Then noticing that v ( ) d =  t t  4 cos 2 t d = 2 sin 2t d d v ( t ) = 4 cos 2 t = 8 sin 2 t dt dt associate the second term with an inductor to get the plus sign. Then
R=
L= 4 cos 2 t 4 cos 2 t = = 5 and i1 (t ) 0.8 cos 2 t
t  4 cos 2 t d i2 (t ) = 2 sin 2 t = 2.5 H 0.8 sin 2 t 726 DP73 a) 11.31cos ( 2t + 45 ) = 11.31 cos ( 45 ) cos ( 2t )  sin ( 45 ) sin ( 2t ) = 8 cos 2 t  8 sin 2 t The first term is proportional to the voltage. Associate it with the resistor. The noticing that i ( ) d =  t t  4 cos 2 t d = 2 sin 2t d d i ( t ) = 4 cos 2 t = 8 sin 2 t dt dt associate the second term with an inductor to get the minus sign. Then v (t ) 8 cos 2 t v2 (t ) 8 sin 2 t R= 1 = = 2 and L = = =1H d 4 cos 2 t 4 cos 2 t 4 cos 2 t 8 sin 2 t dt b) 11.31cos ( 2t + 45 ) = 11.31 cos ( 45 ) cos ( 2t )  sin ( 45 ) sin ( 2t ) = 8 cos 2 t + 8 sin 2 t The first term is proportional to the voltage. Associate it with the resistor. The noticing that t  i ( ) d = 4 cos 2 t d = 2 sin 2t
 t d d i ( t ) = 4 cos 2 t = 8 sin 2 t dt dt associate the second term with a capacitor to get the minus sign. Then
v (t ) 8 cos 2 t R= 1 = = 2 and C = 4 cos 2 t 4 cos 2 t t  4 cos 2 t d v2 (t ) = 2 sin 2 t = 0.25 F 8 sin 2 t 727 DP74 at t=0 iL ( 0 ) = 0 By voltage division: vC ( 0 ) = We require vC ( 0 ) = 3 V so VB = 12 V at t=0+ VB 4 Now we will check First: and dvC dt t = 0+ iL ( 0+ ) = iL ( 0 ) = 0 vC ( 0+ ) = vC ( 0 ) = 3 V Apply KCL at node a: VB  vC ( 0+ ) + + iL ( 0 ) + iC ( 0 ) = 3
0 + iC ( 0+ ) = 12  3 iC ( 0+ ) = 3 A 3
+ iC ( 0 dvC = dt t =0+ C as required. Finally )= 3 V = 24 0.125 s DP75
1 1 2 L i L2 = C v C where iL and vC are the steady state inductor current and capacitor 2 2 v voltage. At steady state, i L = C . Then R We require v L C = C vC2 R 2 C= L R2 R = L = C 102 = 106 104 = 10 2 so R = 100 . 728 Chapter 8 The Complete Response of RL and RC Circuit
Exercises
Ex. 8.31 Before the switch closes: After the switch closes: Therefore R t = 2 = 8 so = 8 ( 0.05 ) = 0.4 s . 0.25 Finally, v (t ) = voc + (v (0)  voc ) e t = 2 + e2.5 t V for t > 0 Ex. 8.32 Before the switch closes: After the switch closes:
81 2 6 = 8 so = = 0.75 s . 0.25 8 1 1 1.33 t Finally, i (t ) = isc + (i (0)  isc ) et = + e A for t > 0 4 12 Therefore R t =
Ex. 8.33 At steadystate, immediately before t = 0: 12 10 i ( 0) = = 0.1 A 10 + 40 16+ 4010 After t = 0, the Norton equivalent of the circuit connected to the inductor is found to be so I sc = 0.3 A, Rt = 40 , = Finally: L 20 1 s = = 40 2 Rt i (t ) = (0.1  0.3)e 2t + 0.3 = 0.3  0.2e 2t A 82 Ex. 8.34 At steadystate, immediately before t = 0 After t = 0, we have:
so Voc = 12 V, Rt = 200 , = Rt C = (200)(20 10 6 ) = 4 ms Finally: v(t ) = (12  12) e t 4 + 12 = 12 V Ex. 8.35 Immediately before t = 0, i (0) = 0. After t = 0, replace the circuit connected to the inductor by its Norton equivalent to calculate the inductor current:
I sc = 0.2 A, Rt = 45 , = L 25 5 = = Rth 45 9 So i (t ) = 0.2 (1  e1.8t ) A Now that we have the inductor current, we can calculate v(t):
v(t ) = 40 i (t ) + 25 d i (t ) dt = 8(1  e 1.8t ) + 5(1.8)e 1.8t = 8 + e 1.8t V for t > 0 83 Ex. 8.36 At steadystate, immediately before t = 0 so i(0) = 0.5 A. After t > 0: Replace the circuit connected to the inductor by its Norton equivalent to get
I sc = 93.75 mA, Rt = 640 , = L .1 1 s = = Rt 640 6400 i (t ) = 406.25 e 6400t + 93.75 mA Finally: v (t ) = 400 i (t ) + 0.1 d i (t ) = 400 (.40625e 6400t + .09375) + 0.1 (6400) (0.40625e 6400t ) dt = 37.5  97.5e 6400t V Ex. 8.41 = ( 2103 )(1106 ) = 2 103 s
vc (t ) = 5 + (1.55 ) e 500 t V
vc (0.001) = 5  3.5e  0.5 = 2.88 V So vc (t ) will be equal to vT at t = 1 ms if v = 2.88 V. T 84 Ex. 8.42 iL (0) = 1 mA, I sc = 10 mA iL ( t ) = 10  9 e L Rt =500 , = 500 vR (t ) = 300 iL ( t ) = 3  2.7 e
 500 t L 500 t L mA V We require that vR ( t ) = 1.5 V at t = 10 ms = 0.01 s . That is 1.5 = 3  2.7e
Ex. 8.61 0 < t < t1  500 (0.01) L L= 5 = 8.5 H 0.588 v(t ) = v()+Ae t / RC where v() = (1 A)(1 ) = 1 V v(t ) = 1 + A e t /(1)(.1) = 1 + A e10 t Now v(0 ) = v(0+ ) = 0 = 1 + A A = 1 v(t ) =1e10t V t > t1
 t .5 (1)(.1) t1 = 0.5 s, v(t ) = v(t1 ) e = v(0.5) e10(t .5) Now v(0.5) 1  e 10(0.5) = 0.993 V v(t ) = 0.993 e10(t 0.5) V 85 Ex. 8 62 t < 0 no sources v(0 ) = v(0+ ) = 0
0 < t <t1
 t v (t ) = v ( ) + A e  t / RC = v ( ) + A e 2 1 0 5 (1 0  7 ) where for t = (steadystate) capacitor becomes an open v() = 10 V
v(t ) = 10 + Ae 50t Now v(0) = 0 = 10 + A A = 10 v(t ) = 10(1 e 50t ) V t > t1 , t1 = .1 s v(t ) = v(.1) e50(t .1) where v(.1) = 10(1 e 50(.1) ) = 9.93 V v(t ) = 9.93e50( t .1) V Ex. 8.63 For t < 0 i = 0. For 0 < t < 0.2 s KCL: 5 + v / 2 + i = 0 di + 10i = 50 di also: v = 0.2 dt dt 10 t i (t ) = 5+ Ae i (0) = 0 = 5+ A A = 5 so we have i (t ) = 5 (1e10t ) A For t > 0.2 s i (0.2) = 4.32 A i(t ) = 4.32e10(t .2) A 86 Ex. 8.71
vs ( t ) = 10sin 20t V d v( t ) KVL: 10sin 20t +10 .01 + v( t ) = 0 dt d v( t ) +10 v( t ) = 100sin 20t dt Natural response: vn (t ) = Aet where = Rt C vn (t ) = Ae10t Forced response: try v f (t ) = B1 cos 20t + B2 sin 20 t Plugging v f (t ) into the differential equation and equating like terms yields: B1 =  4 & B2 = 2 Complete response: v(t ) = vn (t ) + v f (t ) v(t ) = Ae 10t  4 cos 20t + 2 sin 20t Now v(0 ) = v(0+ ) = 0 = A  4 A = 4 v(t ) = 4 e 10t  4 cos 20t + 2sin 20 t V
Ex. 8.72
is ( t ) = 10 e 5t Now v ( t ) = 0.1
Natural response: in (t ) = Ae t for t > 0 di ( t ) di ( t ) +100 i ( t ) = 1000 e 5t dt dt KCL at top node: 10e 5t + i ( t ) + v( t ) /10 = 0 where = L R t in (t ) = Ae 100t B = 10.53
5t Forced response: try i f (t ) = Be 5t & plug into the differential equation 5 Be 5t + 100 Be 5t = 1000e 5t Complete response: i (t ) = Ae
 + 100 t + 10.53e Now i (0 ) = i (0 ) = 0 = A + 10.53 A = 10.53 i (t ) = 10.53 (e 5t  e 100t ) A Ex. 8.73 When the switch is closed, the inductor current is iL = vs / R = vs . When the switch opens, the inductor current is forced to change instantaneously. The energy stored in the inductor instantaneously dissipates in the spark. To prevent the spark, add a resistor (say 1 k) across the switch terminals. 87 Problems
Section 8.3: The Response of a First Order Circuit to a Constant Input P8.31 Here is the circuit before t = 0, when the switch is open and the circuit is at steady state. The open switch is modeled as an open circuit. A capacitor in a steadystate dc circuit acts like an open circuit, so an open circuit replaces the capacitor. The voltage across that open circuit is the initial capacitor voltage, v (0). By voltage division v (0) = 6 (12 ) = 4 V 6+6+6 Next, consider the circuit after the switch closes. The closed switch is modeled as a short circuit. We need to find the Thevenin equivalent of the part of the circuit connected to the capacitor. Here's the circuit used to calculate the open circuit voltage, Voc. Voc = 6 (12 ) = 6 V 6+6 Here is the circuit that is used to determine Rt. A short circuit has replaced the closed switch. Independent sources are set to zero when calculating Rt, so the voltage source has been replaced by a short circuit. ( 6 )( 6 ) = 3 Rt = 6+6 Then = R t C = 3 ( 0.25 ) = 0.75 s Finally,
v ( t ) = Voc + ( v ( 0 )  Voc ) et / = 6  2 e1.33 t V for t > 0 88 P8.32 Here is the circuit before t = 0, when the switch is closed and the circuit is at steady state. The closed switch is modeled as a short circuit. An inductor in a steadystate dc circuit acts like an short circuit, so a short circuit replaces the inductor. The current in that short circuit is the initial inductor current, i(0). i ( 0) = 12 =2 A 6 Next, consider the circuit after the switch opens. The open switch is modeled as an open circuit. We need to find the Norton equivalent of the part of the circuit connected to the inductor. Here's the circuit used to calculate the short circuit current, Isc. I sc = 12 =1 A 6+6 Here is the circuit that is used to determine Rt. An open circuit has replaced the open switch. Independent sources are set to zero when calculating Rt, so the voltage source has been replaced by an short circuit. ( 6 + 6 )( 6 ) = 4 Rt = ( 6 + 6) + 6 Then L 8 = = =2 s Rt 4
Finally, i ( t ) = I sc + ( i ( 0 )  I sc ) e t / = 1 + e 0.5 t A for t > 0 89 P8.33 Before the switch closes: After the switch closes: Therefore R t = 6 = 3 so = 3 ( 0.05 ) = 0.15 s . 2 Finally, v (t ) = voc + (v (0)  voc ) e t = 6 + 18 e6.67 t V for t > 0 P8.34 Before the switch closes: After the switch closes: 810 Therefore R t = 6 6 = 3 so = = 2 s . 2 3 t  10 Finally, i (t ) = isc + (i (0)  isc ) e = 2 + e0.5 t A for t > 0 3
P8.35 Before the switch opens, v o ( t ) = 5 V v o ( 0 ) = 5 V . After the switch opens the part of the circuit connected to the capacitor can be replaced by it's Thevenin equivalent circuit to get: Therefore = ( 20 103 )( 4 106 ) = 0.08 s . Next, v C (t ) = voc + (v (0)  voc ) e
 t = 10  5 e12.5 t V for t > 0 Finally, v 0 (t ) = vC (t ) = 10  5 e 12.5 t V for t > 0 811 P8.36 Before the switch opens, v o ( t ) = 5 V v o ( 0 ) = 5 V . After the switch opens the part of the circuit connected to the capacitor can be replaced by it's Norton equivalent circuit to get: Therefore = 5 = 0.25 ms . 20 103
 Next, i L (t ) = isc + (i L (0)  isc ) e Finally, vo ( t ) = 5 t = 0.5  0.25 e4000 t mA for t > 0 for t > 0 d i L ( t ) = 5 e 4000 t V dt P8.37 At t = 0 (steadystate) Since the input to this circuit is constant, the inductor will act like a short circuit when the circuit is at steadystate: for t > 0 iL ( t ) = iL ( 0 ) e  ( R L ) t = 6 e20t A 812 P8.38 Before the switch opens, the circuit will be at steady state. Because the only input to this circuit is the constant voltage of the voltage source, all of the element currents and voltages, including the capacitor voltage, will have constant values. Opening the switch disturbs the circuit. Eventually the disturbance dies out and the circuit is again at steady state. All the element currents and voltages will again have constant values, but probably different constant values than they had before the switch opened. Here is the circuit before t = 0, when the switch is closed and the circuit is at steady state. The closed switch is modeled as a short circuit. The combination of resistor and a short circuit connected is equivalent to a short circuit. Consequently, a short circuit replaces the switch and the resistor R. A capacitor in a steadystate dc circuit acts like an open circuit, so an open circuit replaces the capacitor. The voltage across that open circuit is the capacitor voltage, vo(t). Because the circuit is at steady state, the value of the capacitor voltage will be constant. This constant is the value of the capacitor voltage just before the switch opens. In the absence of unbounded currents, the voltage of a capacitor must be continuous. The value of the capacitor voltage immediately after the switch opens is equal to the value immediately before the switch opens. This value is called the initial condition of the capacitor and has been labeled as vo(0). There is no current in the horizontal resistor due to the open circuit. Consequently, vo(0) is equal to the voltage across the vertical resistor, which is equal to the voltage source voltage. Therefore
vo ( 0 ) = Vs The value of vo(0) can also be obtained by setting t = 0 in the equation for vo(t). Doing so gives
vo ( 0 ) = 2 + 8 e0 = 10 V Consequently, Vs = 10 V 813 Next, consider the circuit after the switch opens. Eventually (certainly as t ) the circuit will again be at steady state. Here is the circuit at t = , when the switch is open and the circuit is at steady state. The open switch is modeled as an open circuit. A capacitor in a steadystate dc circuit acts like an open circuit, so an open circuit replaces the capacitor. The voltage across that open circuit is the steadystate capacitor voltage, vo(). There is no current in the horizontal resistor and vo() is equal to the voltage across the vertical resistor. Using voltage division, 10 vo ( ) = (10 ) R + 10 The value of vo() can also be obtained by setting t = in the equation for vo(t). Doing so gives
vo ( ) = 2 + 8 e  = 2 V Consequently, 10 (10 ) 2 R + 20 = 100 R = 40 R + 10 t Finally, the exponential part of vo(t) is known to be of the form e where = R t C and 2= Rt is the Thevenin resistance of the part of the circuit connected to the capacitor.
Here is the circuit that is used to determine Rt. An open circuit has replaced the open switch. Independent sources are set to zero when calculating Rt, so the voltage source has been replaced by a short circuit. R t = 10 +
so ( 40 )(10 ) = 18
40 + 10 = R t C = 18 C From the equation for vo(t) t 0.5 t =  =2s Consequently, 2 = 18 C C = 0.111 = 111 mF 814 P8.39: Before the switch closes, the circuit will be at steady state. Because the only input to this circuit is the constant voltage of the voltage source, all of the element currents and voltages, including the inductor current, will have constant values. Closing the switch disturbs the circuit by shorting out the resistor R1. Eventually the disturbance dies out and the circuit is again at steady state. All the element currents and voltages will again have constant values, but probably different constant values than they had before the switch closed. The inductor current is equal to the current in the 3 resistor. Consequently,
 0.35 t vo (t ) 6  3 e  0.35 t = = 2 e A when t > 0 i (t ) = 3 3 In the absence of unbounded voltages, the current in any inductor is continuous. Consequently, the value of the inductor current immediately before t = 0 is equal to the value immediately after t = 0. Here is the circuit before t = 0, when the switch is open and the circuit is at steady state. The open switch is modeled as an open circuit. An inductor in a steadystate dc circuit acts like a short circuit, so a short circuit replaces the inductor. The current in that short circuit is the steady state inductor current, i(0). Apply KVL to the loop to get
R1 i ( 0 ) + R 2 i ( 0 ) + 3 i ( 0 )  24 = 0 i (0) = 24 R1 + R 2 + 3 The value of i(0) can also be obtained by setting t = 0 in the equation for i(t). Do so gives
i ( 0 ) = 2  e0 = 1 A Consequently,
1= 24 R1 + R 2 = 21 R1 + R 2 + 3 Next, consider the circuit after the switch closes. Here is the circuit at t = , when the switch is closed and the circuit is at steady state. The closed switch is modeled as a short circuit. The combination of resistor and a short circuit connected is equivalent to a short circuit. Consequently, a short circuit replaces the switch and the resistor R1. 815 An inductor in a steadystate dc circuit acts like a short circuit, so a short circuit replaces the inductor. The current in that short circuit is the steady state inductor current, i(). Apply KVL to the loop to get 24 R 2 i ( ) + 3 i ( )  24 = 0 i ( ) = R2 + 3 The value of i() can also be obtained by setting t = in the equation for i(t). Doing so gives
i ( ) = 2  e  = 2 A Consequently
2= 24 R2 = 9 R2 + 3 Then R1 = 12 Finally, the exponential part of i(t) is known to be of the form e t where =
L and Rt Rt is the Thevenin resistance of the part of the circuit that is connected to the inductor. Here is shows the circuit that is used to determine Rt. A short circuit has replaced combination of resistor R1 and the closed switch. Independent sources are set to zero when calculating Rt, so the voltage source has been replaced by an short circuit. R t = R 2 + 3 = 9 + 3 = 12 so =
From the equation for i(t) 0.35 t =  Consequently, 2.857 = L L = 34.28 H 12 t L L = R t 12 = 2.857 s 816 P8.310 First, use source transformations to obtain the equivalent circuit for t < 0: for t > 0: So iL ( 0 ) = 2 A, I sc and iL ( t ) = 2e24t 1 L 1 s = 0, Rt = 3 + 9 = 12 , = = 2 = 24 Rt 12 t >0 t >0 Finally v ( t ) = 9 iL ( t ) = 18 e24t 817 Section 84: Sequential Switching P8.41 Replace the part of the circuit connected to the capacitor by its Thevenin equivalent circuit to get: Before the switch closes at t = 0 the circuit is at steady state so v(0) = 10 V. For 0 < t < 1.5s, voc = 5 V and Rt = 4 so = 4 0.05 = 0.2 s . Therefore v (t ) = voc + (v (0)  voc ) et = 5 + 5e5 t V for 0 < t < 1.5 s At t =1.5 s, v (1.5) = 5 + 5e ( = 8 0.05 = 0.4 s . Therefore Finally
5 t for 0 < t < 1.5 s 5+5 e V v (t ) = 2.5 ( t 1.5) for 1.5 s < t V 10  5 e 0.05 1.5) = 5 V . For 1.5 s < t, voc = 10 V and Rt = 8 so
( t 1.5) v (t ) = voc + (v (1.5)  voc ) e = 10  5 e 2.5 ( t 1.5 ) V for 1.5 s < t P8.42 Replace the part of the circuit connected to the inductor by its Norton equivalent circuit to get: Before the switch closes at t = 0 the circuit is at steady state so i(0) = 3 A. For 0 < t < 1.5s, isc = 2 12 A and Rt = 6 so = = 2 s . Therefore 6 i (t ) = isc + (i (0)  isc ) et = 2 + e0.5 t A for 0 < t < 1.5 s 818 At t =1.5 s, i (1.5) = 2 + e Therefore 0.5 (1.5) = 2.47 A . For 1.5 s < t, isc = 3 A and Rt = 8 so =
( t 1.5 ) 12 = 1.5 s . 8 i (t ) = isc + (i (1.5)  isc ) e = 3  0.53 e 0.667 ( t 1.5 ) V for 1.5 s < t Finally 2 + e 0.5 t A for 0 < t < 1.5 s i (t ) = 0.667 ( t 1.5 ) for 1.5 s < t A 3  0.53 e P8.43 At t = 0:
KVL :  52 + 18 i + (12 8) i = 0 i (0 ) =104 39 A 6 + iL = i = 2 A = iL (0 ) 6+ 2 For 0 < t < 0.051 s iL (t ) = iL (0) e t where = L R t R t = 6 12 + 2 = 6 iL (t ) = 2 e 6t A 6 +12 6 t i (t ) = iL (t ) =6e A 6 For t > 0.051 s i L ( t ) = i L (0.051) e  ( R L ) ( t  0.051) i L (0.051) = 2 e  6 (.051) = 1.473 A i L ( t ) = 1.473 e  14 ( t  0.051) A i ( t ) = i L ( t ) = 1.473 e  14 ( t  0.051) A 819 P8.44 At t = 0: Assume that the circuit has reached steady state so that the voltage across the 100 F capacitor is 3 V. The charge stored by the capacitor is q ( 0 ) = (100 106 ) ( 3) = 300 106 C 0 < t < 10ms: With R negligibly small, the circuit reaches steady state almost immediately (i.e. at t = 0+). The voltage across the parallel capacitors is determined by considering charge conservation:
q ( 0+ ) = (100 F) v ( 0+ ) + (400 F) v ( 0+ ) v (0
+ v 0+ = 0.6 V ( ) ) = 100 10 q ( 0+ )
6 + 400 106 = q ( 0 ) 500 106 = 300 106 500 106 10 ms < t < l s: Combine 100 F & 400 F in parallel to obtain
v(t ) = v ( 0+ ) e  (t .01) RC = 0.6e  (t .01) (10 ) (5 x10 v(t ) = 0.6 e2(t .01) V
3 4 ) P8.45 For t < 0: Find the Thevenin equivalent of the circuit connected to the inductor (after t >0). First, the open circuit voltage:
i1 = 40 =1 A 20 + 20 voc = 20 i1  5 i1 = 15 V 820 Next, the short circuit current: 20 i 1 = 5 i 1 i 1 = 0 i sc + 0 = Then
voc 15 = = 7.5 i sc 2 Replace the circuit connected to the inductor by its Norton equivalent circuit. First L 15 103 1 = = = Rt 7.5 500 Next i ( t ) = 2  2 e  500 t A t >0 Rt = 40 i sc = 2 A 20 After t = 0, the steady state inductor current is 2 A. 99% of 2 is 1.98. 1.98 = 2  2 e  500 t t = 9.2 ms P8.46 v ( 0 ) = 5 V , v ( ) = 0 and = 105 106 = 0.1 s v ( t ) = 5 e 10 t V for t > 0 2.5 = 5 e 10 t1 i (t1 ) = v (t1 ) 100 10
3 t 1 = 0.0693 s 2.5 = 25 A 100 103 = 821 Section 85: Stability of First Order Circuits P8.51 This circuit will be stable if the Thvenin equivalent resistance of the circuit connected to the inductor is positive. The Thvenin equivalent resistance of the circuit connected to the inductor is calculated as i (t ) = 100 v T (400 R) 100 iT = 100+ 400 Rt = iT 100+ 400 vT = 400 i (t )  R i (t ) The circuit is stable when R < 400 . P8.52 The Thvenin equivalent resistance of the circuit connected to the inductor is calculated as Ohm's law: v ( t ) = 1000 iT ( t ) KVL: A v ( t ) + vT ( t )  v ( t )  4000 iT ( t ) = 0 vT ( t ) = (1  A ) 1000 iT ( t ) + 4000 iT ( t ) vT ( t ) = ( 5  A ) 1000 iT ( t ) The circuit is stable when A < 5 V/V. Rt =
P8.53 The Thvenin equivalent resistance of the circuit connected to the inductor is calculated as v (t ) Ohm's law: i ( t ) =  T 6000 v (t ) KCL: i ( t ) + B i ( t ) + i T ( t ) = T 3000 v ( t ) vT ( t ) i T ( t ) =  ( B + 1)  T + 6000 3000 ( B + 3) vT ( t ) = 6000 vT ( t ) 6000 Rt = = iT ( t ) B + 3 The circuit is stable when B > 3 A/A. 822 P8.54 The Thvenin equivalent resistance of the circuit connected to the inductor is calculated as (1000 )( 4000 ) i (t ) = 800 i (t ) v(t ) = T T 1000 + 4000 vT (t ) = v(t )  Av(t ) = (1  A ) v(t ) vT (t ) = 800 (1  A) iT (t ) The circuit is stable when A < 1 V/V. Rt = 823 Section 86: The Unit Step Response P8.61 The value of the input is one constant, 8 V, before time t = 0 and a different constant, 7 V, after time t = 0. The response of the first order circuit to the change in the value of the input will be
vo ( t ) = A + B e  a t for t > 0 where the values of the three constants A, B and a are to be determined. The values of A and B are determined from the steady state responses of this circuit before and after the input changes value. Capacitors act like open circuits when the input is constant and the circuit is at steady state. Consequently, the capacitor is replaced by an open circuit. The value of the capacitor voltage at time t = 0, will be equal to the steady state capacitor voltage before the input changes. At time t = 0 the output voltage is a 0 vo ( 0 ) = A + B e ( ) = A + B The steadystate circuit for t < 0. Consequently, the capacitor voltage is labeled as A + B. Analysis of the circuit gives
A+ B = 8 V Capacitors act like open circuits when the input is constant and the circuit is at steady state. Consequently, the capacitor is replaced by an open circuit. The value of the capacitor voltage at time t = , will be equal to the steady state capacitor voltage after the input changes. At time t = the output voltage is vo ( ) = A + B e
 a () =A The steadystate circuit for t > 0. Consequently, the capacitor voltage is labeled as A. Analysis of the circuit gives A = 7 V Therefore B = 15 V 824 The value of the constant a is determined from the time constant, , which is in turn calculated from the values of the capacitance C and of the Thevenin resistance, Rt, of the circuit connected to the capacitor. 1 = = Rt C a Here is the circuit used to calculate Rt. Therefore a= Rt = 6 1 1 = 2.5 3 s ( 6 ) ( 66.7 10 ) (The time constant is = ( 6 ) ( 66.7 103 ) = 0.4 s .) Putting it all together: 8 V for t 0 vo ( t ) =  2.5 t V for t 0 7 + 15 e P8.62 The value of the input is one constant, 3 V, before time t = 0 and a different constant, 6 V, after time t = 0. The response of the first order circuit to the change in the value of the input will be
vo ( t ) = A + B e  a t for t > 0 where the values of the three constants A, B and a are to be determined. The values of A and B are determined from the steady state responses of this circuit before and after the input changes value. Capacitors act like open circuits when the input is constant and the circuit is at steady state. Consequently, the capacitor is replaced by an open circuit. The value of the capacitor voltage at time t = 0, will be equal to the steady state capacitor voltage before the input changes. At time t = 0 the output voltage is a 0 vo ( 0 ) = A + B e ( ) = A + B Consequently, the capacitor voltage is labeled as A + B. Analysis of the circuit gives The steadystate circuit for t < 0. 825 A+ B = 6 ( 3) = 2 V 3+ 6 Capacitors act like open circuits when the input is constant and the circuit is at steady state. Consequently, the capacitor is replaced by an open circuit. The value of the capacitor voltage at time t = , will be equal to the steady state capacitor voltage after the input changes. At time t = the output voltage is The steadystate circuit for t > 0. vo ( ) = A + B e
 a () =A Consequently, the capacitor voltage is labeled as A. Analysis of the circuit gives A= Therefore B = 2 V The value of the constant a is determined from the time constant, , which is in turn calculated from the values of the capacitance C and of the Thevenin resistance, Rt, of the circuit connected to the capacitor. 1 = = Rt C a Here is the circuit used to calculate Rt. Rt = Therefore
a= 6 (6) = 4 V 3+ 6 ( 3)( 6 ) = 2
3+ 6
1 1 s ( 2 )(.5 ) =1 (The time constant is = ( 2 )( 0.5 ) = 1 s .) Putting it all together: 2 V for t 0 vo ( t ) =  t 4  2 e V for t 0 826 P8.63 The value of the input is one constant, 7 V, before time t = 0 and a different constant, 6 V, after time t = 0. The response of the first order circuit to the change in the value of the input will be
vo ( t ) = A + B e  a t for t > 0 where the values of the three constants A, B and a are to be determined. The values of A and B are determined from the steady state responses of this circuit before and after the input changes value. Inductors act like short circuits when the input is constant and the circuit is at steady state. Consequently, the inductor is replaced by a short circuit. The value of the inductor current at time t = 0, will be equal to the steady state inductor current before the input changes. At time t = 0 the output current is The steadystate circuit for t < 0. io ( 0 ) = A + B e
 a ( 0) = A+ B Consequently, the inductor current is labeled as A + B. Analysis of the circuit gives A+ B = 7 = 1.4 A 5 Inductors act like short circuits when the input is constant and the circuit is at steady state. Consequently, the inductor is replaced by a short circuit. The value of the inductor current at time t = , will be equal to the steady state inductor current after the input changes. At time t = the output current is The steadystate circuit for t > 0. io ( ) = A + B e
 a () =A Consequently, the inductor current is labeled as A. Analysis of the circuit gives A= Therefore B = 2.6 V 6 = 1.2 A 5 827 The value of the constant a is determined from the time constant, , which is in turn calculated from the values of the inductance L and of the Thevenin resistance, Rt, of the circuit connected to the inductor. 1 L = = a Rt Here is the circuit used to calculate Rt. Rt = Therefore a= 2.22 1 = 1.85 1.2 s 1.2 = 0.54 s .) 2.22 ( 5 ) ( 4 ) = 2.22
5+ 4 (The time constant is = Putting it all together: 1.4 A for t 0 io ( t ) =  1.85 t A for t 0 1.2  2.6 e
P8.64 v (t ) = 4u (t )  u (t  1)  u (t  2) + u (t  4)  u (t  6) P8.65 Assume that the circuit is at steady state at t = 1. Then 0 vs ( t ) = 4 0 t <1 1<t < 2 t >2
v ( t ) = 4  4 e  (t 1) V for 1 t 2 = R C = ( 5 105 )( 2 106 ) = 1 s so v ( 2 ) = 4  4 e  (21) = 2.53 V and
v ( t ) = 2.53 e  (t  2) V for t 2 0 v(t ) = 4 4e  ( t 1) 2.53e  (t  2) t 1 1t 2 t 2 828 P8.66 The capacitor voltage is v(0) = 10 V immediately before the switch opens at t = 0. For 0 < t < 0.5 s the switch is open: v ( 0 ) = 10 V, v ( ) = 0 V, = 3 so v ( t ) = 10 e  2 t V In particular, v ( 0.5 ) = 10 e For t > 0.5 s the switch is closed:
 2 ( 0.5) 1 1 = s 6 2 = 3.679 V v ( 0 ) = 3.679 V, v ( ) = 10 V, Rt = 6  3 = 2 , = 2 =
so 1 6 1 s 3
 3 ( t  0.5) v ( t ) = 10 + ( 3.679  10 ) e = 10  6.321 e
 3 ( t  0.5 ) V V P8.67 Assume that the circuit is at steady state before t = 0. Then the initial inductor current is i(0) = 0 A. For 0 < t < 1 ms: The steady state inductor current will be 30 i ( ) = lim i ( t ) = ( 40 ) = 24 A t 30 + 20 The time constant will be 50 103 1 = = 103 = s 30 + 20 1000 The inductor current is i ( t ) = 24 (1  e 1000 t ) A In particular, i ( 0.001) = 24 (1  e 1 ) = 15.2 A For t > 1 ms Now the initial current is i(0.001) = 15.2 A and the steady state current is 0 A. As before, the time constant is 1 ms. The inductor current is i ( t ) = 15.2 e
1000 ( t  0.001) A 829 The output voltage is
480 (1  e 1000 t ) V t < 1 ms v ( t ) = 20 i ( t ) = 1000 ( t  0.001) V t > 1 ms 303 e P8.68 For t < 0, the circuit is: After t = 0, replace the part of the circuit connected to the capacitor by its Thevenin equivalent circuit to get: vc ( t ) = 15 + ( 6  ( 15 ) ) e = 15 + 9 e  5 t V
 t / ( 40000.00005 ) 830 Section 87 The Response of an RL or RC Circuit to a Nonconstant Source P8.71 Assume that the circuit is at steady state before t = 0: KVL : 12ix + 3(3 ix ) + 38.5 = 0 ix = 1.83 A Then vc (0 ) = 12 ix = 22 V = vc (0+ ) After t = 0: KVL : 12i (t )  8e 5t + v ( t ) = 0 x c dv ( t ) 1 dvc ( t ) KCL : ix ( t )2ix ( t ) + (1 36) c = 0 ix ( t ) = dt 108 dt 1 dvc ( t ) 5t 12 + v (t ) = 0  8e c 108 dt dv (t ) c + 9v (t ) = 72e5t v (t ) = Ae 9t c cn dt Try v (t ) = Be 5t & substitute into the differential equation B = 18 cf v (t ) = Ae 9t + 18 e5t c v (0) = 22 = A + 18 A = 4 c v (t ) = 4e9t + 18e5t V c 831 P8.72 Assume that the circuit is at steady state before t = 0:
12 = 3A 4 iL (0+ ) = iL (0 ) = After t = 0: v( t ) 12 v( t ) + iL ( t ) + = 6 e 2t 4 2 di ( t ) also : v ( t ) = (2 / 5) L dt di ( t ) 3 iL ( t ) + (2 / 5) L = 3 + 6 e 2t 4 dt KCL : diL ( t ) 10 + iL ( t ) = 10 + 20 e 2t 3 dt
 (10 / 3)t in (t ) = Ae , try i f (t ) = B + Ce2t , substitute into the differential equation, and then equating like terms B =3, C =15 i f (t ) =3+15 e2t iL (t ) =in (t ) + i f (t ) = Ae (10 / 3)t + 3+15e2t , iL (0) = 3 = A + 3 + 15 A = 15 iL (t ) = 15e  (10 / 3) t + 3 + 15e2t Finally, v(t ) =( 2 / 5 ) diL = 20 e  (10 / 3) t 12 e 2t V dt P8.73 Assume that the circuit is at steady state before t = 0: 6 Current division: iL (0 ) = 5 = 1 mA 6 + 24 832 After t = 0: KVL:  25sin 4000 t + 24iL ( t ) + .008 di L ( t ) 25 +3000i L ( t ) = sin4000t dt .008 diL ( t ) =0 dt in (t ) = Ae 3000t , try i f (t ) = B cos 4000t + C sin 4000t , substitute into the differential equation and equate like terms B = 1/ 2, C = 3 / 8 i f (t ) = 0.5cos 4000 t + 0.375 sin 4000 t iL (t ) = in (t ) + i f (t ) = Ae 3000t  0.5cos 4000 t + 0.375 sin 4000 t iL (0+ ) = iL (0 ) =103 = A 0.5 A 0.5 iL (t ) = 0.5 e 3000t  0.5cos 4000 t + 0.375 sin 4000 t mA but v(t ) = 24iL (t ) = 12 e 3000t  12 cos 4000t + 9sin 4000t V P8.74 Assume that the circuit is at steady state before t = 0: Replace the circuit connected to the capacitor by its Thevenin equivalent (after t=0) to get: dvc ( t ) KVL:  10 cos 2t + 15 1 +v t =0 30 dt c ( ) dvc ( t ) + 2vc ( t ) = 20 cos 2t dt vn (t ) = Ae2t , Try v f (t ) = B cos 2t + C sin 2t & substitute into the differential equation to get B = C = 5 v f (t ) = 5cos 2t + 5sin 2t. vc (t ) = vn (t ) + v f (t ) = Ae2t + 5cos 2t + 5sin 2t Now vc (0) = 0 = A + 5 A = 5 vc (t ) = 5e2t + 5cos 2t + 5sin 2t V 833 P8.75 Assume that the circuit is at steady state before t = 0. There are no sources in the circuit so i(0) = 0 A. After t = 0, we have: di ( t ) KVL :  10sin100t + i ( t ) + 5 + v (t ) = 0 dt v( t ) Ohm's law : i ( t ) = 8 dv( t ) +18 v( t ) = 160sin100t dt vn (t ) = Ae18t , try v f (t ) = B cos100t + C sin100t , substitute into the differential equation and equate like terms B = 1.55 & C = 0.279 v f (t ) = 1.55cos100t + 0.279sin100t v(t ) = vn (t ) + v f (t ) = Ae18t 1.55 cos100 t + 0.279 sin100 t v(0) = 8 i (0) = 0 v (0) = 0 = A1.55 A = 1.55 so v(t ) = 1.55e18t 1.55cos100t + 0.279 sin100t V P8.76 Assume that the circuit is at steady state before t = 0. vo ( t ) = vc ( t ) vC (0+ ) = vC (0 ) = 10 V
After t = 0, we have v (t ) 8 e5 t i (t ) = s = = 0.533 e5 t mA 15000 15000 The circuit is represented by the differential dv ( t ) vC ( t ) equation: i ( t ) = C C + . Then dt R ( 0.533 10 ) e
3 5 t = ( 0.25 106 ) dvc ( t ) + (103 ) vc ( t ) dt dvc ( t ) + 4000 vc ( t ) = 4000 e5t dt Then vn ( t ) = Ae4000t . Try v f ( t ) = Be5t . Substitute into the differential equation to get
d B e5t dt ( ) + 4000 ( B e ) = 4000 e
5t 5t B= 4000 = 1.00125 1 3995 834 vC (t ) = v f ( t ) + vn ( t ) = e 5t + Ae 4000t vC (0) = 10 = 1 + A A = 11 vC (t ) = 1 e2t  11 e4000t V Finally vo (t ) =  vC (t ) = 11e4000t 1e 5t V , t 0 P8.77
From the graph iL (t ) = 1 t mA . Use KVL to get 4 (1) iL (t ) + 0.4
Then diL (t ) = v1 (t ) dt diL (t ) + 2.5 iL (t ) = 2.5 v1 (t ) dt
v1 = 0.1+ 0.25t V di 1 t + 2.5 1 t = 2.5 v1 (t ) 4 dt 4 P8.78 Assume that the circuit is at steady state before t = 0. v (0+ ) = v (0 ) = 2 30 = 10 V 4+ 2 After t = 0 we have
KVL : 1 d v( t ) 5 d v( t ) + v (t ) + 4 i = 30 2 dt 2 dt 1 d v( t ) 3t 2 i ( t ) + 4 i ( t )  + 30 = e 2 dt The circuit is represented by the differential equation d v( t ) 6 6 2 (10 + e 3t ) v (t ) = + 19 19 3 dt Take vn ( t ) = Ae
( 6 /19 ) t . Try , v f ( t ) = B + Ce 3t , substitute into the differential equation to get 835 3Ce 3t + Equate coefficients to get B = 10 , C =  Then 6 60 4 3t ( B + Ce 3t ) = + e 19 19 19 4 4 v f ( t ) = e 3t + Ae (6 /19) t 51 51 4 3t e + Ae (6 /19) t 51 4 +A 51 A= 4 51 v ( t ) = vn ( t ) + v f ( t ) = 10  Finally vc (0+ ) = 10 V, 10 = 10  vc (t ) = 10 + 4  (6 /19) t 3t (e e ) V 51 P8.79 We are given v(0) = 0. From part b of the figure: 5t 0 t 2 s vs ( t ) = t > 2s 10 Find the Thevenin equivalent of the part of the circuit that is connected to the capacitor: The open circuit voltage: The short circuit current: (ix=0 because of the short across the right 2 resistor) Replace the part of the circuit connected to the capacitor by its Thevenin equivalent: KVL: 2 dv( t ) + v ( t )  vs ( t ) = 0 dt dv( t ) v ( t ) vs ( t ) + = dt 2 2 vn ( t ) = Ae0.5 t 836 For 0 < t < 2 s, vs ( t ) = 5 t . Try v f ( t ) = B + C t . Substituting into the differential equation and equating coefficients gives B = 10 and C =5. Therefore v ( t ) = 5t  10 + A e  t / 2 . Using v(0) = 0, we determine that A =10. Consequently, v ( t ) = 5t + 10(et / 2  1) . At t = 2 s, v( 2 ) = 10e1 = 3.68 . Next, for t > 2 s, vs ( t ) = 10 V . Try v f ( t ) = B . Substituting into the differential equation and equating coefficients gives B = 10. Therefore v ( t ) = 10 + Ae determine that A = 6.32. Consequently, v ( t ) = 10  6.32 e
 (t 2) / 2 . Using v ( 2 ) = 3.68 , we  (t  2) / 2 . P8.710 d v (t ) KVL:  kt + Rs C C + vC ( t ) = 0 dt d vC ( t ) k 1 vC ( t ) = t + Rs C Rs C dt vc ( t ) = vn ( t ) + v f ( t ) , where vc ( t ) = Ae t / Rs C . Try v f ( t ) = B0 + B1 t & plug into D.E. B1 + 1 k t thus B0 =  kRs C , B1 = k . [ B0 + B1t ] = Rs C Rs C Now we have vc (t ) = Ae  t / Rs C + k (t  Rs C ). Use vc (0) = 0 to get 0 = A  kRs C A = kRs C. vc (t ) = k[t  Rs C (1 e t / Rs C )]. Plugging in k =1000 , Rs = 625 k & C = 2000 pF get vc (t ) = 1000[t  1.25 103 (1  e 800 t )] v(t) and vC(t) track well on a millisecond time scale. 837 Spice Problems
SP 81 838 SP 82 839 SP 83 v(t ) = A + B e t / 7.2 = v(0) = A + B e 0 for t > 0 7.2 = A + B B = 0.8 V  A = 8.0 V 8.0 = v() = A + B e 0.05 8  7.7728 7.7728 = v(0.05) = 8  0.8 e 0.05 /  = ln = 1.25878 0.8 0.05 = = 39.72 ms 1.25878 Therefore
v(t ) = 8  0.8 e t / 0.03972 V for t > 0 840 SP 84 i (t ) = A + B e t / 0 = i (0) = A + B e
0 for t > 0 3 B = 4 10 A A 3 0 = A+ B A = 4 103
3 4 103 = i () = A + B e 
3 6 2.4514 10 = v(5 10 ) = ( 4 10  5 106 )  ( 4 10 ) e  5106 / ( ) ( 4  2.4514 ) 103 = ln = 0.94894 4 103 Therefore 5 106 = = 5.269 s 0.94894 i (t ) = 4  4 e t / 5.26910
6 mA for t > 0 841 Verification Problems
VP 81 First look at the circuit. The initial capacitor voltage is vc(0) = 8 V. The steadystate capacitor voltage is vc = 4 V. We expect an exponential transition from 8 volts to 4 volts. That's consistent with the plot. Next, let's check the shape of the exponential transition. The Thevenin resistance of the part of ( 2000 )( 4000 ) = 4 k so the time constant is the circuit connected to the capacitor is R t = 2000 + 4000 3 4 2 = R t C = 103 ( 0.5 106 ) = ms . Thus the capacitor voltage is 3 3 vc (t ) = 4 e t 0.67 +4 V where t has units of ms. To check the point labeled on the plot, let t1 = 1.33 ms. Then 1.33  4 e .67 vc (t1 ) = So the plot is correct. + 4 = 4.541 ~ 4.5398 V VP 82 The initial and steadystate inductor currents shown on the plot agree with the values obtained from the circuit. Next, let's check the shape of the exponential transition. The Thevenin resistance of the part of ( 2000 )( 4000 ) = 4 k so the time constant is the circuit connected to the inductor is R t = 2000 + 4000 3 L 5 15 ms . Thus inductor current is = = = R t 4 103 4 3 iL (t )  2 e t 3.75 + 5 mA where t has units of ms. To check the point labeled on the plot, let t1 = 3.75 ms. Then iL (t1 ) = 3.75  2 e 3.75 + 5 = 4.264 mA 4.7294 mA so the plot does not correspond to this circuit.
842 VP 83 Notice that the steadystate inductor current does not depend on the inductance, L. The initial and steadystate inductor currents shown on the plot agree with the values obtained from the circuit. After t = 0 So I sc = 5 mA and = L 1333 The inductor current is given by iL (t ) = 2e 1333t has units of Henries. Let t 1 = 3.75 ms, then L + 5 mA , where t has units of seconds and L 4.836 = iL (t1 ) = 2 e (1333)(0.00375) L + 5 = 2e5 L + 5 so 4.8365 = e 5 L 2
L= is the required inductance.
VP 84 First consider the circuit. When t < 0 and the circuit is at steadystate: and 5 =2 H 4.8365 ln 2 For t > 0 So Voc = R2 R1 R2 RRC ( A + B) , Rt = and = 1 2 R1 + R2 R1 + R2 R1 + R2 843 Next, consider the plot. The initial capacitor voltage is (vc (0)=) 2 and the steadystate capacitor voltage is (Voc =) 4 V, so vC (t ) =  6e t + 4 At t 1 = 1.333 ms 3.1874 = vC (t1 ) =  6 e 0.001333 + 4 so = 0.001333 = 0.67 ms 4+ 3.1874 ln 6 Combining the information obtained from the circuit with the information obtained from the plot gives R2 R2 R1 R2C A = 2, ( A + B ) = 4, = 0.67 ms R1 + R2 R1 + R2 R1 + R2 There are many ways that A, B, R , R , and C can be chosen to satisfy these equations. Here is one convenient way. Pick R = 3000 and R = 6000. Then
1 2 1 2 2A = 2 A = 3 3 2( A+ B) = 4 B 3 = 6 B = 9 3 2 1 F = C 2000 C = ms 3 3 Design Problems
DP 81 R3 6= 12 R1 + R 2 = R 3 . Steadystate response when the switch is open: R1 + R 2 + R 3 Steadystate response when the switch is open: 10 = 10 ms = 5 = ( R 1  R 3 ) C =
R3 6 C R3 R1 + R 3 12 R1 = R3 5 . Let C = 1 F. Then R 3 = 60 k, R 1 = 30 k and R 2 = 30 k. 844 DP 82 12 steady state response when the switch is open : 0.001 = R + R 1 2 steady state response when the switch is open: 0.004 = Therefore, R 2 = 9 k. L L 10 ms = 5 = 5 L = 240 H = R1 + R 2 2400 12 R1 R + R = 12 k .
1 2 R1 = 3 k . DP 83 Rt = 50 k when the switch is open and Rt = 49 k 50 k when the switch is closed so use Rt = 50 k. 106 (a) t = 5 Rt C C = = 4 pF 5 50103 (b) t = 5 ( 50103 )( 2106 ( ) ) = 0.5 s DP 84 Rt = 50 k when the switch is open and Rt = 49 k 50 k when the switch is closed so use Rt = 50 k. t t When the switch is open: 5 e = (1  k ) 5 ln (1 k ) =  t =  ln (1 k ) When the switch is open: 5  5 e (a) C = t = k 5 t =  ln (1 k ) (b) t =  ln(1  .95) ( 50103 )( 2106 ) = 0.3 s 106 = 6.67 pF  ln (1.95 ) ( 50103 ) DP 85 i (0) = R1 20 40 R1 R1 + 40 40 + 40 + R1 845 For t > 0: i (t ) = i (0) e t where = L 102 = R t 40+ R 2 At t < 200 s we need i ( t ) > 60 mA and i ( t ) <180 mA First let's find a value of R 2 to cause i (0) < 180 mA. Try R 2 = 40 . Then i (0) = 1 t A = 166.7 mA so i (t ) = 0.1667 e . 6 Next, we find a value of R 2 to cause i (0.0002) > 60 mA. 102 1 s. = 0.2 ms = 50 5000 i (0.0002) = 166.7103 e 50000.0002 = 166.7103 e 1 = 61.3 mA Try R 2 = 10, then = DP 86 The current waveform will look like this: We only need to consider the rise time:
t Vs A t iL (t ) = (1  e ) = (1  e ) R+2 R+2 where L 0.2 1 s = = = 3 15 Rt A iL (t ) = (1  e 15t ) 3 2 Now find A so that iL R fuse 10 W during 0.25 t 0.75 s 2 we want [iL (0.25)]R fuse = 10 W A2 (1e 15(.25) ) 2 (1) =10 A = 9.715 V 9 846 Chapter 9  Complete Response of Circuits with Two Energy Storage Elements
Exercises
Ex. 9.31 Apply KVL to right mesh: di ( t ) + v ( t ) + 1( i ( t ) is ( t ) ) = 0 dt di ( t ) v ( t ) = 2  ( i ( t )is ( t ) ) dt 2 The capacitor current and voltage are related by
i (t ) = 1 dis ( t ) 1 di ( t ) d 2i ( t ) 1 dv ( t ) 1 d di ( t ) = 2 i ( t )+ is ( t ) =   dt dt 2 2 dt 2 dt 2 dt 2 dt d 2i ( t ) 1 di ( t ) 1 dis ( t ) + + i( t ) = 2 dt 2 dt 2 dt The inductor voltage is related to the inductor current by di ( t ) v (t ) = 1 dt Apply KCL at the top node: is ( t ) = v (t ) 1 dv ( t ) + i (t ) + 1 2 dt Ex. 9.32 Using the operator s = v (t ) 1 + sv ( t ) is ( t ) = v ( t ) + 1 s 2 is ( t ) = v ( t ) + i ( t ) + sv ( t ) 2 Therefore d we have dt v (t ) = s i (t ) 2s is ( t ) = 2 s v ( t ) + 2 v ( t ) + s 2 v ( t ) d 2v ( t ) dv ( t ) d i (t ) +2 + 2 v (t ) = 2 s 2 dt dt dt 91 Ex. 9.33 Using the operator s = d , apply KVL to the dt left mesh: i1 ( t ) + s ( i1 ( t ) i 2 ( t ) ) = vs ( t ) Apply KVL to the right mesh: 1 2 i 2 ( t ) + 2 i 2 ( t ) + s ( i 2 ( t ) i1 ( t ) ) = 0 s 1 2 i1 ( t ) = 2 i 2 ( t ) + 2 i 2 ( t ) + i 2 ( t ) s s
Combining these equations gives: 3s i2 ( t ) + 4si2 ( t ) + 2i2 ( t ) = s vs ( t )
2 2 or d 2i2 ( t ) di2 ( t ) d 2 vs ( t ) 3 +4 + 2i2 ( t ) = dt 2 dt dt 2 Ex. 9.41 Using the operator s = top node: i s (t ) = d , apply KCL at the dt v (t ) 1 + i (t ) + s v (t ) 4 4 Apply KVL to the rightmost mesh:
v (t )  ( s i (t ) + 6 i (t )) = 0 Combining these equations gives:
s 2 i ( t ) + 7 s i ( t ) + 10 i ( t ) = 4 i s ( t ) The characteristic equation is: s 2 + 7 s + 10 = 0 . The natural frequencies are: s = 2 and s = 5 . Assume zero initial conditions . Write mesh d equations using the operator s = : dt 1 s i1 ( t )  i 2 ( t ) + 7 + 10 i1 ( t )  10 = 0 2 and 1 v ( t )  7  s i1 ( t )  i 2 ( t ) = 0 2 Ex. 9.42 92 Now 0.005 s v ( t ) = i 2 ( t ) v ( t ) = 200
i2 (t ) s i2 (t ) s so the second mesh equation becomes: 200 1  7  s i1 ( t )  i 2 ( t ) = 0 2 Writing the mesh equation in matrix form:
s 10 + 2 1 s 2 1 s i1 ( t ) 3 2 = 1 200 i 2 ( t ) 7 s+ 2 s  Obtain the characteristic equation by calculating a determinant: 10 +
 s 2 1 s 2 1 s 2 = s 2 + 20s + 400 = 0 s1,2 = 10 j 17.3 1 200 s+ 2 s
 Ex. 9.51 After t = 0 , we have a parallel RLC circuit with 1 1 7 1 1 2 = = = =6 = and o = 2 RC 2(6)(1/ 42) 2 LC (7)(1/ 42) 7  6 = 1,  6 2 dv ( t ) vn (t ) = A1e t + A2 e6t . We need vn (0) and n dt 7 s 1 , s 2 =   =  2
2 2 o 2 to evaluate A1 & A2 . t =0 At t = 0+ we have:
iC ( 0+ ) = 10 A Then vn (0+ ) = 0 = A1 + A2 dv ( t ) 10 = = 420 V s 1 dt t =0+ 42 A1 = 84 , A2 = 84 dvn =420=  A1  6 A2 dt t =0+ 93 Finally vn (t ) = 84e t + 84e 6t V Ex. 9.52 1 1 = 0 s 2 + 40s + 100 = 0 s+ RC LC Therefore s 1 , s 2 = 2.68 , 37.3 s2 + vn ( t ) = A1 e 2.68t + A2 e37.3t , v(0) = 0 = A1 + A2 v(0+ ) 1 dv(0+ ) + KCL at t = 0 yields + i (0 ) + = 0 so 1 40 dt dv(0+ ) =  40 v(0+ )  40 i (0+ ) =  40(0)  40(1) =  2.7 A1  37.3 A2 dt Therefore: A1 = 1.16 , A2 = 1.16 v(t ) = vn (t ) = 1.16e 2.68t + 1.16e37.3t
+ Ex. 9.61 For parallel RLC circuits: = 1 1 1 1 2 = = 50, o = = = 2500 3 LC (0.4)(103 ) 2 RC 2(10)(10 )
(50) 2  2500 = 50, 50 The roots of the characteristic equations are: s1,2 = 50 The natural response is vn (t ) = A1 e50t + A2 t e50t . At t = 0+ we have: v(0+ ) ic (0 ) = =  .8V 10 dv( t ) i (0+ ) = c = 800 V / s dt c + t =0
+ 94 So vn (0+ ) = 8 = A1 vn (t ) = 8e50t + A2 t e50t dv(0+ ) = 800 =  400 + A2 A2 =  400 dt vn (t ) = 8 e 50t  400 t e50t V Ex. 9.71 = 1 1 = = 8000 2 RC 2(62.5)(106 ) 1 1 o2 = = = 1 08 6 LC (.01)(10 ) 2 s =  2  o =  8000 (8000) 2 108 =  8000 j 6000 vn (t ) = e 8000t [ A1 cos 6000 t + A2 sin 6000 t ] at t = 0+ 0.08 + 10 + ic (0+ ) = 0 62.5 ic (0+ ) = .24 A dv(0+ ) ic (0+ ) = = 2.4 10+5 V/s dt C dvn (0+ ) vn (0 ) = 10 = A1 and = 2.4 105 = 6000 A2  8000 A1 A2 = 26.7 dt
+ vn (t ) = e8000t [10 cos 6000 t  26.7 sin 6000 t ] V Ex. 9.81 The differential equation is d 2v ( t ) dv ( t ) +5 + 6 v ( t ) = vs ( t ) so the characteristic equation is 2 dt dt s 2 + 5 s + 6 = 0 . The roots are s 1 , s 2 = 2,  3 . d 2v ( t ) dv ( t ) (a) +5 + 6 v ( t ) = 8 . Try v f ( t ) = B . Substituting into the differential equation gives 2 dt dt 6 B = 8 v f (t ) = 8 / 6 V . 95 (b) d 2v ( t ) dt
2 +5 dv ( t ) dt + 6 v ( t ) = 3 e  4 t . Try v f ( t ) = B e 4 t . Substituting into the differential 3 3 equation gives (4) 2 B + 5(4) B + 6 B = 3 B = . v f ( t ) = e4t . 2 2 2 d v (t ) dv ( t ) (c) +5 + 6 v ( t ) = 2 e  2 t . Try v f ( t ) = B t e 2 t because 2 is a natural frequency. 2 dt dt Substituting into the differential equation gives
(4t  4) B + 5 B (1  2t ) + 6 Bt = 2 B = 2. v f ( t ) = 2 t e 2t . Ex. 9.82
+ 20 i ( t ) = 36 + 12 t . Try i f ( t ) = A + B t . Substituting into the differential dt 2 dt equation gives 0 + 9 B + 20( A + Bt ) = 36 + 12t B = 0.6 and A = 1.53. +9 i f ( t ) = 1.53 + 0.6 t A d 2i ( t ) di ( t ) Ex. 9.91 When the circuit reaches steady state after t = 0, the capacitor acts like an open circuit and the inductor acts like a short circuit. Under these conditions vC ( ) = R2 R1 + R 2 1 Next, represent the circuit by a 2nd order differential equation: KCL at the top node of R2 gives: KVL around the outside loop gives: Use the substitution method to get vC ( t ) R2 vs ( t ) = L +C d vC ( t ) = iL ( t ) dt d iL ( t ) + R1 iL ( t ) + vC ( t ) dt 96 vs ( t ) = L v (t ) d vC ( t ) d d + C vC ( t ) + R1 C + C vC ( t ) + vC ( t ) R2 dt R 2 dt dt L d R1 d2 + R1 C vC ( t ) + 1 + vC ( t ) + v t R2 dt R2 C ( ) dt 2 = LC (a) C = 1 F, L = 0.25 H, R1 = R2 = 1.309 Use the steady state response as the forced response: R2 1 1= V v f = vC ( ) = 2 R1 + R 2 The characteristic equation is R1 1+ 1 R1 R2 2 2 s + + s+ = s + 6 s + 8 = ( s + 2 )( s + 4 ) = 0 R 2 C L LC so the natural response is vn = A1 e 2 t + A2 e 4 t V The complete response is vc ( t ) = iL ( t ) = At t = 0
+ 1 + A1 e 2 t + A2 e4 t V 2 vC ( t ) 1.309 + d vC ( t ) = 1.236 A1 e 2 t  3.236 A2 e4 t + 0.3819 dt 0 = vc 0+ = A1 + A2 + 0.5
1 2 0 = iL 0 ( ) = 1.236 A  3.236 A
+ ( ) + 0.3819 Solving these equations gives A1 = 1 and A2 = 0.5, so vc ( t ) = 1 2 t 1 4 t e + e V 2 2 (b) C = 1 F, L = 1 H, R1 = 3 , R2 = 1 Use the steady state response as the forced response: R2 1 v f = vC ( ) = 1= V R1 + R 2 4 The characteristic equation is 97 R1 1+ 1 R1 R2 2 2 2 s + + s+ = s + 4s + 4 = ( s + 2 ) = 0 R 2 C L LC so the natural response is vn = ( A1 + A2 t ) e 2 t V The complete response is vc ( t ) = iL ( t ) = vC ( t ) + At t = 0+ 1 + ( A1 + A2 t ) e 2 t V 4 d 1 vC ( t ) = + dt 4 (( A 2  A1 )  A2 t e 2 t ) 0 = vc 0+ = A1 + 0 = iL 0+ = ( ) 1 4 ( ) 1 + A2  A1 4 Solving these equations gives A1 = 0.25 and A2 = 0.5, so vc ( t ) = 1 1 1 2 t  + t e V 4 4 2 (c) C = 0.125 F, L = 0.5 H, R1 = 1 , R2 = 4 Use the steady state response as the forced response: R2 4 v f = vC ( ) = 1= V R1 + R 2 5 The characteristic equation is R1 1+ 1 R1 R2 2 2 s + + s+ = s + 4s + 20 = ( s + 2  j 4 )( s + 2 + j 4 ) = 0 R 2 C L LC so the natural response is vn = e 2 t ( A1 cos 4 t + A2 sin 4 t ) V The complete response is vc ( t ) = 0.8 + e 2 t ( A1 cos 4 t + A2 sin 4 t ) V vC ( t ) 4 + A 2 2 t A1 1d vC ( t ) = 0.2 + e cos 4 t  e2 t sin 4 t 8 dt 2 2 iL ( t ) = 98 At t = 0+ 0 = vc 0+ = 0.8 + A1 0 = iL 0+ = 0.2 + ( ) ( ) A2 2 Solving these equations gives A1 = 0.8 and A2 = 0.4, so
vc ( t ) = 0.8  e 2 t ( 0.8cos 4 t + 0.4sin 4 t ) V Ex 9.92 When the circuit reaches steady state after t = 0, the capacitor acts like an open circuit and the inductor acts like a short circuit. Under these conditions vC ( ) = R2 R1 + R 2 1, iL ( ) = 1 R1 + R 2 and vo ( ) = R2 R1 + R 2 1 Next, represent the circuit by a 2nd order differential equation: KVL around the righthand mesh gives: KCL at the top node of the capacitor gives: Use the substitution method to get
vs ( t ) = R1 C d d d L iL ( t ) + R 2 iL ( t ) + L iL ( t ) + R 2 iL ( t ) + R1 iL ( t ) dt dt dt d iL ( t ) + R 2 iL ( t ) dt vs ( t )  vC ( t ) d  C vC ( t ) = iL ( t ) R1 dt vC ( t ) = L Using iL ( t ) = vo ( t ) gives R2 d2 d = R1 LC 2 iL ( t ) + ( L + R1 R 2 C ) iL ( t ) + ( R1 + R 2 ) iL ( t ) dt dt L d R1 + R 2 d2 vs ( t ) = LC 2 vo ( t ) + + R1 C vo ( t ) + v t R2 dt R2 o ( ) R2 dt R1 99 (a) C = 1 F, L = 0.25 H, R1 = R2 = 1.309 Use the steady state response as the forced response: R2 1 1= V v f = vo ( ) = 2 R1 + R 2 The characteristic equation is R2 1+ 1 R2 R1 2 2 s + + s+ = s + 6 s + 8 = ( s + 2 )( s + 4 ) = 0 R1 C L LC so the natural response is vn = A1 e 2 t + A2 e 4 t V The complete response is 1 + A1 e 2 t + A2 e 4 t V 2 A1 2 t A2 4 t v (t ) 1 iL ( t ) = o e + e V = + 1.309 2.618 1.309 1.309 vo ( t ) = vC ( t ) = 1.309 iL ( t ) + At t = 0+ 1 d 1 iL ( t ) = + 0.6180 A1 e 2 t + 0.2361 A2 e 4 t 4 dt 2 0 = iL 0+ = 0 = vC 0+ = ( ) A1 A2 1 + + 2.618 1.309 1.309 ( ) 1 + 0.6180 A1 + 0.2361 A2 2 Solving these equations gives A1 = 1 and A2 = 0.5, so vo ( t ) = 1 2 t 1 4 t e + e V 2 2 (b) C = 1 F, L = 1 H, R1 = 1 , R2 = 3 Use the steadystate response as the forced response: R2 3 v f = vo ( ) = 1= V R1 + R 2 4 The characteristic equation is R2 1+ 1 R2 R1 2 2 s2 + + s+ = s + 4s + 4 = ( s + 2 ) = 0 R1 C L LC 910 so the natural response is The complete response is vn = ( A1 + A2 t ) e 2 t V vo ( t ) =
iL ( t ) = 3 + ( A1 + A2 t ) e 2 t V 4
= 1 A1 A2 2 t t e V + + 4 3 3 vo ( t ) 3 vC ( t ) = 3 iL ( t ) + At t = 0+ 3 A1 A2 A2 2 t d iL ( t ) = + + t e + 4 3 3 3 dt 0 = iL 0+ = ( ) A1 0 = vC 0+ ( ) 3 3 A1 A2 = + + 4 3 3 + 1 4 Solving these equations gives A1 = 0.75 and A2 = 1.5, so vo ( t ) = 3 3 3 2 t  + t e V 4 4 2 (c) C = 0.125 F, L = 0.5 H, R1 = 4 , R2 = 1 Use the steady state response as the forced response: R2 1 v f = vo ( ) = 1= V R1 + R 2 5 The characteristic equation is R2 1+ 1 R2 R1 2 2 s + + s+ = s + 4s + 20 = ( s + 2  j 4 )( s + 2 + j 4 ) = 0 R1 C L LC so the natural response is vn = e 2 t ( A1 cos 4 t + A2 sin 4 t ) V The complete response is vo ( t ) = 0.2 + e 2 t ( A1 cos 4 t + A2 sin 4 t ) V iL ( t ) = vo ( t ) 1 = 0.2 + e 2 t ( A1 cos 4 t + A2 sin 4 t ) V 911 vC ( t ) = iL ( t ) + At t = 0+ 1 d iL ( t ) = 0.2 + 2 A2 e2 t cos 4 t  2 A1 e2 t sin 4 t 2 dt 0 = iL 0+ = 0.2 + A1 0 = vC
+ ( ) ( 0 ) = 0.2 + 2 A 2 Solving these equations gives A1 = 0.8 and A2 = 0.4, so
vc ( t ) = 0.2  e 2 t ( 0.2 cos 4 t + 0.1sin 4 t ) V Ex. 9.101 At t = 0+ no initial stored energy v1 (0+ ) = v2 (0+ ) = i (0+ ) = 0 KVL :  0 + 3 di (0+ ) di (0+ ) +0=0 =0 10 dt dt 0 dv1 (0+ ) + = 0 KCL at A : + i1 (0 ) + 0 = 0 1 dt 5 dv2 (0+ ) = 10 KCL at B :  0 + i2 (0+ )  10 = 0 i2 (0+ ) = 6 dt KCL at A : dv2 (0+ ) = 12 V s dt For t > 0: v1 1 d v1 + +i = 0 1 12 dt 5 d v2 = 10 KCL at B :  i + 6 dt 3 di  v1 + + v2 = 0 KVL: 10 dt Eliminating i yields 1 d v1 5 d v2 v1 + +  10 = 0 12 dt 6 dt 3 5 d 2 v2 v1 + + v2 = 0 10 6 dt 2 Next
912 v1 = v2 + Now, eliminating v1
v2 + 1 d 2 v2 4 dt 2 d v1 d 2 v2 1 d 3 v2 = + dt dt 2 4 dt 3 1 d 2 v2 1 d v2 1 d 3 v2 5 d v2 + + = 10 + 4 dt 2 12 dt 4 dt 3 6 dt Finally, the circuit is represented by the differential equation: d 3 v2 d2 v dv + 12 2 2 + 44 2 + 48v2 = 480 3 dt dt dt The characteristic equation is s 3 + 12s 2 + 44s + 48 = 0 . It's roots are s1,2,3 = 2, 4, 6 . The natural response is vn = A1e 2t + A2 e 4t + A3e 6t Try v f = B as the forced response. Substitute into the differential equation and equate coefficients to get B = 10. Then v2 (t ) = vn (t ) + v f (t ) = A1e 2t + A2 e 4t + A3e6t + 10 We have seen that v2 (0+ ) = 0 and Then
v2 (0+ ) = 0 = A1 + A2 + A3 + 10 dv2 (0+ ) = 12 = 2 A1  4 A2  6 A3 dt d 2 v2 (0+ ) = 0 = 4 A1 + 16 A2 + 36 A3 dt 2 dv2 (0+ ) d 2 v2 (0+ ) = 12 V/s . Also = 4[v1 (0+ )  v2 (0+ )] = 0 . dt dt 2 Solving these equations yields A1 = 15, A2 = 6, A3 = 1 so v2 (t ) = ( 15 e 2t + 6 e 4t  e 6t + 10 ) V Ex. 9.111 1 1 s2 + s+ =0 RC LC In our case L = 0.1, C = 0.1 so we have s 2 + 10 s + 100 = 0 R 913 a)
R = 0.4 s 2 + 25s + 100 = 0 s1,2 = 5,  20 b) R = 1 s 2 + 10 s + 100 = 0 s1,2 =  5 j 5 3 914 Problems
Section 93: Differential Equations for Circuits with Two Energy Storage Elements P9.31 KCL: iL ( t ) = v (t ) dv ( t ) +C R2 dt KVL: vs ( t ) = R1iL ( t ) + L diL ( t ) + v (t ) dt dv ( t ) L dv ( t ) d 2v ( t ) v (t ) vs ( t ) = R1 +C + LC + v (t ) + dt R2 dt dt 2 R2 d 2v ( t ) R L dv ( t ) = 1 + 1 v ( t ) + R1C + + [ LC ] vs ( t ) R2 dt dt 2 R2 In this circuit R1 = 2 , R 2 = 100 , L = 1 mH, C = 10 F so
2 dv ( t ) 8 d v ( t ) vs ( t ) = 1.02v ( t ) + .00003 + 10 dt dt 2 dv ( t ) d 2 v ( t ) 8 8 10 vs ( t ) = 1.02 10 v ( t ) + 3000 + dt dt 2 P9.32 Using the operator s =
KCL: is ( t ) = d we have dt KVL: v ( t ) = R2iL ( t ) + LsiL ( t ) v (t ) + iL ( t ) + Csv ( t ) R1 Solving by usingCramer's rule for iL ( t ) : iL ( t ) = is ( t ) R2 Ls + + R2Cs + LCs 2 + 1 R1 R1 R2 L 2 1 + iL ( t ) + + R2C siL ( t ) + [ LC ] s iL ( t ) = is ( t ) R1 R1 915 In this circuit R1 = 100 , R 2 = 10 , L = 1 mH, C = 10 F so
1.1iL ( t ) + .00011siL ( t ) + 108 s 2iL ( t ) = is ( t ) diL ( t ) d 2iL ( t ) + = 108 is ( t ) 1.1 10 iL ( t ) + 11000 2 dt dt
8 P9.33 After the switch closes, a source transformation gives: KCL: iL ( t ) + C KVL: dvc ( t ) vs ( t ) + vc ( t ) + =0 dt R2 diL ( t )  vc ( t )  vs ( t ) = 0 dt di ( t ) vc ( t ) = R1is ( t ) + R1iL ( t ) + L L  vs ( t ) dt Differentiating R1is ( t ) + R1iL ( t ) + L d vc ( t ) d is ( t ) d iL ( t ) d 2iL ( t ) d vs ( t ) = R1 + R1 +L  dt dt dt dt 2 dt Then Solving for i L ( t ) : d is ( t ) d iL ( t ) d 2iL ( t ) d vs ( t ) vs ( t ) + R1 +L  iL ( t ) + C R1 + dt dt dt 2 dt R2 di ( t ) 1 + R1is ( t ) + R1iL ( t ) + L L  vs ( t ) = 0 R2 dt d 2i L ( t ) R1  R1 R1 di s ( t ) 1 dv s ( t ) 1 di L ( t ) R1 1 + + + + i s (t )  + i L (t ) = 2 dt LCR 2 L dt L dt L R 2C dt LR 2C LC 916 Section 94: Solution of the Second Order Differential Equation  The Natural Response P9.41 From Problem P 9.32 the characteristic equation is: 1.1108 +11000 s + s 2 = 0 s1 , s2 =
P9.42 11000 (11000) 2  4(1.1108 ) = 5500 j8930 2 diL ( t ) + vc ( t ) dt KVL: 40 ( is ( t )  iL ( t ) ) = (100 103 ) The current in the inductor is equal to the current in the capacitor so 1 dv ( t ) iL ( t ) = 103 c 3 dt
2 40 dv ( t ) 100 d vC ( t ) vC ( t ) = 40 is ( t )  103 C  106 2 3 dt 3 dt d 2 vC ( t ) dv ( t ) + 400 C + 30000 vC ( t ) = 40 is ( t ) 2 dt dt 2 s + 400s + 30000 = 0 ( s + 100)( s + 300) = 0 s1 = 100, s2 = 300 P9.43 v ( t )  vs ( t ) dv ( t ) + iL ( t ) + (10 106 ) =0 1 dt di ( t ) KVL: v ( t ) = 2iL ( t ) + (1 103 ) L dt KCL: 0 = 2 iL ( t ) + (1 103 ) vs ( t ) = 3iL ( t ) + 0.00102 diL ( t ) dt diL ( t ) dt  vs ( t ) + iL ( t ) + (10 106 ) ( 2 ) d 2iL ( t ) dt
2 diL ( t ) dt + (10 106 )(103 ) diL ( t ) dt d 2iL ( t ) dt + 108 d 2iL ( t ) dt + 102000 + 3 108 iL ( t ) = 108 vs ( t ) s 2 + 102000s + 3 108 = 0 s1 = 3031, s2 = 98969 917 Section 9.5: Natural Response of the Unforced Parallel RLC Circuit P9.51 The initial conditions are v ( 0 ) = 6 V, dv( 0 ) d = 3000 V/s . Using the operator s = , the node dt dt  vs ( t ) v( t ) v( t ) L + = 0 or LCs 2 + s + 1 v ( t ) = vs ( t ) equation is Csv ( t ) + R sL R 1 1 s+ = 0 s 2 + 500 s + 40, 000 = 0 The characteristic equation is: s 2 + RC LC The natural frequencies are: s1,2 = 250 2502  40, 000 = 100, 400 The natural response is of the form v ( t ) = Ae100t + Be400t . We will use the initial conditions to evaluate the constants A and B. dv ( 0 ) = 3000 = 100 A  400 B dt Therefore, the natural response is v ( t ) = 2e100t + 8e400t t >0 v ( 0) = 6 = A + B A = 2 and B = 8 P9.52 The initial conditions are v ( 0 ) = 2 V, i ( 0 ) = 0 . 1 1 s+ = 0 s 2 + 4s + 3 = 0 RC LC The natural frequencies are: s1 , s2 = 1,  3 The natural response is of the form v ( t ) = Ae  t + Be 3t . We will use the initial conditions to evaluate the constants A and B. dv ( t ) =  Ae  t  3Be 3t . At t = 0 this becomes Differentiating the natural response gives dt dv ( t ) v ( t ) dv ( t ) v (t ) i (t ) dv ( 0 ) + + i ( t ) = 0 or =   . =  A  3B . Applying KCL gives C dt R dt RC C dt dv ( 0 ) v ( 0) i ( 0) =  At t = 0 this becomes  . Consequently dt RC C The characteristic equation is: s 2 + 1A  3B =  v ( 0) i ( 0) 2  = 0 =  8 RC C 14 918 Also, v ( 0 ) = 2 = A + B . Therefore A = 1 and B = 3. The natural response is
v ( t ) = e  t + 3e 3t V P9.53
di1 ( t ) di ( t ) 3 2 =0 dt dt di ( t ) di ( t ) KVL :  3 1 +3 2 + 2i2 ( t ) = 0 dt dt
KVL : i1 + 5 (1) ( 2) d , the KVL equations are dt (1+5s )i1 + ( 3s )i2 = 0 3s 2 i1 = 0 (1 + 5s )( 3s + 2 )  ( 3s ) i1 = 0 (1 + 5s ) i1  ( 3s ) 3s + 2 ( 3s ) i1 + ( 3s + 2 ) i2 = 0 1 The characteristic equation is (1+5s )( 3s + 2 )  9 s 2 = 6 s 2 + 13s + 2 = 0 s1,2 =  , 2 6 Using the operator s = The currents are i1 ( t ) = Ae 6 + Be2t and i2 ( t ) = Ce 6 + De 2t , where the constants A, B, C and D must be evaluated using the initial conditions. Using the given initial values of the currents gives i1 ( 0 ) = 11 = A + B and i 2 ( 0 ) = 11 = C + D Let t = 0 in the KCL equations (1) and (2) to get di1 ( 0 ) dt = di2 ( 0 ) A C 33 143 =   2 B and = = D 2 6 6 6 dt
t t So A = 3, B = 8, C = 1 and D = 12. Finally, i1 (t ) = 3e t / 6 + 8e2t A and i 2 (t ) = e t / 6 + 12e 2t A 919 Section 9.6: Natural Response of the Critically Damped Unforced Parallel RLC Circuit P9.61 After t = 0 Using KVL: 100 ic ( t ) + 0.025 dic ( t ) + vc ( t ) = 0 dt The capacitor current and voltage are related by: ic ( t ) = 105
d 2 vc ( t ) dt
2 dvc ( t ) dt + 4000 dvc ( t ) dt + 4 106 vc ( t ) = 0 The characteristic equation is: s 2 + 4000 s + 4 106 = 0 The natural frequencies are: s1,2 =  2000,  2000 The natural response is of the form: vc ( t ) = A1e2000t + A2 t e2000t Before t = 0 the circuit is at steady state (The capacitor current is continuous at t = 0 in this circuit because it is equal to the inductor current.)
vc ( 0+ ) = 3 = A1 = 0 = 2000 A1 + A2 A2 = 6000 dt vc ( t ) = ( 3 + 6000t ) e2000t V for t 0 dvc ( 0+ ) P9.62 After t = 0 Using KCL: t  vc ( ) d + vc ( t ) + 1 dvc ( t ) =0 4 dt d 2 vc ( t ) dv ( t ) +4 c + 4vc ( t ) = 0 dt dt The characteristic equation is: s 2 + 4 s + 4 = 0 920 The natural frequencies are: s1,2 = 2, 2 The natural response is of the form: vc ( t ) = A1e2t + A2 t e2 t Before t = 0 the circuit is at steady state
i L ( 0+ ) = i L ( 0  ) and vC ( 0+ ) = vC ( 0 ) i C ( 0 + ) = i L ( 0 + ) =  2 A dv ( 0+ ) dt = i C ( 0+ ) 14 = 8 V vc ( 0 + )=0= A1 and dvc ( 0+ ) dt = 8 = A2 vc ( t ) = 8 t e2 t V P9.63 Assume that the circuit is at steady state before t = 0. The initial conditions are vc ( 0 ) = 104 V & iL ( 0 ) = 0 A After t = 0 KVL: KCL:  vc ( t ) + .01 diL ( t ) + 106 iL ( t ) = 0 dt (1) d 2iL ( t ) dvC ( t ) di ( t ) = C .01 + 106 L iL ( t ) = C 2 dt dt dt d 2iL ( t ) di ( t ) + 106 C L + iL ( t ) = 0 2 dt dt ( 2) 0.01 C The characteristic equation is: ( 0.01 C ) s 2 + (106 C ) s + 1 = 0 106 C The natural frequencies are: s1,2 = 2 ( 0.01C ) (10 C )
6 2  4 ( 0.01C ) For criticallydamped response: 1012 C 2  .04C = 0 C = 0.04 pF so s1,2 = 5 107 , 5 107 . 921 The natural response is of the form: iL ( t ) = A1e 510 t + A2 t e 510
7 7 t diL + ( 0 ) = 100 dt di ( 0 ) = 106 So iL ( 0 ) = 0 = A1 and L dt Now from (1) 7 vc ( 0+ )  106 iL ( 0+ ) = 106 A s = A2 iL ( t ) = 106 t e510 t A
7 Now v ( t ) = 106 iL ( t ) = 1012 t e510 t V P9.64 The characteristic equation can be shown to be: s 2 + The natural frequencies are: s1,2 = 250,  250 v ( 0 ) = 6 = A and v ( t ) = 6e250t 1 1 = s 2 + 500 s + 62.5 103 = 0 s+ RC LC The natural response is of the form: v ( t ) = Ae 250t + B t e250t dv ( 0 ) = 3000 = 250 A + B B = 1500 dt  1500 t e250t V P9.65 After t=0, using KVL yields: di ( t ) t + Ri ( t ) + 2 + 4 0 i ( ) d = 6 (1) dt v( t ) Take the derivative with respect to t: d 2i ( t ) di ( t ) +R + 4i ( t ) = 0 dt 2 dt
The characteristic equation is s 2 + Rs + 4 = 0 Let R = 4 for critical damping ( s + 2) 2 =0 So the natural response is i ( t ) = A t e 2t + B e 2t i ( 0 ) = 0 B = 0 and i ( t ) = 4 t e 2t A di ( 0 ) = 4  R ( i( 0 ) ) = 4  R ( 0 ) = 4 = A dt 922 Section 97: Natural Response of an Underdamped Unforced Parallel RLC Circuit P9.71 After t = 0 KCL: vc ( t ) dv ( t ) + iL ( t ) + 5 106 c = 0 dt 250 KVL: vc ( t ) = 0.8 diL ( t ) dt (1) ( 2) d 2vc ( t ) dv ( t ) + 800 c + 2.5 105 v ( t ) = 0 s 2 + 800 s + 250, 000 = 0, s1,2 = 400 j 300 c dt dt 2 The natural response is of the form v c (t ) = e 400t A1 cos 300t + A 2sin 300t Before t = 0 the circuit is at steady state: iL ( 0+ ) = iL ( 0 ) = 6 A 500 vc ( 0+ ) = vc ( 0 ) = 250 6 ( 500 )+6 = 3 V From equation (1) : dvc ( 0+ ) dt =  2 105 iL ( 0+ )  800vc ( 0+ ) = 0 vc ( 0+ ) = 3 = A1 dvc ( 0+ ) dt = 0 = 400 A1 + 300 A2 A2 = 4 vc ( t ) = e 400t [3cos 300t + 4sin 300t ] V 923 P9.72 Before t = 0 v ( 0+ ) = v ( 0 ) = 0 V i ( 0+ ) = i ( 0 ) = 2 A After t = 0 KCL :
t v (t ) 1 d v (t ) + + 2 v ( ) d + i ( 0 ) = 0 0 1 4 dt Using the operator s = d we have dt 1 2 v (t ) + s v (t ) + v (t ) + i (0) = 0 4 s (s 2 + 4s + 8) v ( t ) = 0 s = 2 j 2 The characteristic equation and natural frequencies are: s 2 + 4s + 8 = 0 The natural response is of the form: v ( t ) = e v ( 0 ) = 0 = B1 and so
2 t dv ( 0 ) = 4 i ( 0 )  v ( 0 ) = 4 [ 2] = 8 = 2 B2 or B2 = 4 dt
v ( t ) = 4e 2t sin 2t V B1 cos 2t + B 2 sin 2t P9.73 After t = 0 1 dvc ( t ) vc ( t ) + + iL ( t ) = 0 4 dt 2 4 diL ( t ) KVL : vc ( t ) = + 8 iL ( t ) dt KCL :
d 2i L ( t ) dt 2 di L ( t ) dt (1) ( 2) Characteristic Equation: +4 + 5 i L ( t ) = 0 s 2 + 4 s + 5 = 0 s1,2 = 2 i Natural Response: i L ( t ) = e 2t A1 cos t + A2 sin t 924 Before t = 0 vc ( 0 ) 48 +  = 7 4 8 + 2 vc ( 0 ) = vc ( 0 ) = 8 V 2 8 iL ( 0+ ) = iL ( 0 ) =  = 4 A 2 diL ( 0+ ) dt = vc ( 0+ ) 4  2iL ( 0+ ) = 8 A  2 ( 4 ) = 10 4 s iL ( 0+ ) = 4 = A1 diL ( 0+ ) iL ( t ) = e 2t [ 4 cos t + 2sin t ] A dt = 10 =  2 A1 + A2 A2 = 2 P9.74 The plot shows an underdamped response, i.e. v ( t ) = e  t [ k1 cos t + k2 sin t ] + k3 . Examining the plot shows v ( ) = 0 k3 = 0, v ( 0 ) = 0 k1 = 0 . Therefore, v ( t ) = k2 e  t sin t . Again examining the plot we see that the maximum voltage is approximately 260 mV the time is approximately 5 ms and that the minimum voltage is approximately 200 mV the time is approximately 7.5 ms. The time between adjacent maximums is approximately 5 ms so 2 = 1257 rad/s . Then 5 103  ( 0.005 ) 0.26 = k2 e sin (1257 (.005 ) ) (1)
0.2 = k2 e
 ( 0.0075 ) sin (1257 (.0075 ) ) ( 2) To find we divide (1) by (2) to get  1.3 = e ( 0.0025 ) sin ( 6.29 rad ) sin ( 9.43 rad ) e0.0025 = 1.95 = 267 From (1) we get k2 = 544 . Then v ( t ) = 544e 267t sin1257t V 925 P9.75 After t = 0 The characteristic equation is: s2 + 1 1 s+ = 0 or s 2 + 2 s + 5 = 0 RC LC The natural frequencies are: s1,2 = 1 j 2 The natural response is of the form: v(t ) = e  t B1 cos 2t + B 2 sin 2t v(0 ) = 2 = B1 . From KCL, ic ( 0
+ 2 1 ) =  5  i ( 0 ) =  5  10 =  1 V 2 s dv ( 0 ) 3 1 = 10  =  B + 2 B B = 
+ +
+ v ( 0+ ) so dt 2 1 2 2 2 3 Finally, v ( t ) = 2e  t cos 2t  e t sin 2t V 2 t0 926 Section 98: Forced Response of an RLC Circuit P9.81 After t = 0 KCL : is ( t ) = v (t ) R + iL ( t ) + C dt dv ( t ) dt KVL : v ( t ) = L
is ( t ) = diL ( t ) d 2iL ( t ) L diL ( t ) + iL ( t ) + LC R dt dt 2 + 1 diL ( t ) 1 1 + iL ( t ) = is ( t ) RC dt LC LC diL ( t ) dt + (105 ) iL ( t ) = (105 ) is ( t ) d 2iL ( t ) dt
2 d 2iL ( t ) dt
2 + ( 650 ) (a) Try a forced response of the form i f ( t ) = A . Substituting into the differential equations gives
0+0+ A 1 1 = 3 (.01) (110 ) (.01) (1103 ) A = 1 . Therefore i f ( t ) = 1 A . (b) Try a forced response of the form i f ( t ) = A t + B . Substituting into the differential equations gives 0 + A 65 1 + ( A t + B) = 0.5 t . Therefore A = 0.5 and ( 0.01)( 0.001) (100 ) ( 0.001) B = 3.25 10 3 . Finally i f ( t ) = 5 t  3.25 103 A . (c) Try a forced response of the form i f ( t ) = A e250t . It doesn't work so try a forced response of the form i f ( t ) = B t e250t . Substituting into the differential equation gives ( 250 )2 B e250t  500 B e250t + 650 ( 250 ) B t e250t + B e250t + 105 B t e250t = 2 e250t . Equating coefficients gives ( 250 )
and 2 2 B + 650 ( 250 ) B + 105 B = 0 ( 250 ) + 650 ( 250 ) + 105 B = 0 [ 0] B = 0 500 B + 650 B = 2 B = 0.0133 Finally i f ( t ) = 0.0133 t e 250t A . 927 P9.82 After t = 0 d 2v ( t ) dt d 2v ( t ) dt + v (t ) R dv ( t ) 1 + v (t ) = s L dt LC LC dv ( t ) dt + 12000v ( t ) = 12000 vs ( t ) + 70 (a) Try a forced response of the form v f ( t ) = A . Substituting into the differential equations gives
0 + 0 + 12000 A = 24000 A = 2 . Therefore v f ( t ) = 2 V . (b) Try a forced response of the form v f ( t ) = A + B t . Substituting into the differential equations gives 70 A + 12000 A t + 12000 B = 2400 t . Therefore A = 0.2 and B = Finally v f ( t ) = ( 1.167 103 ) t + 0.2 V .
70 A = 1.167 10 3 . 12000 (c) Try a forced response of the form v f ( t ) = A e 30t . Substituting into the differential equations gives 900 Ae 30t  2100 Ae 30 t + 12000 Ae 30 t = 12000 e 30t . Therefore A =
12000 = 1.11 . Finally 10800 v f ( t ) = 1.11e250 t V . 928 Section 99: Complete Response of an RLC Circuit P9.91 First, find the steady state response for t < 0, when the switch is open. Both inputs are constant so the capacitor will act like an open circuit at steady state, and the inductor will act like a short circuit. After a source transformation at the left of the circuit: 11  4 = 2.33 mA 3000 i L ( 0) = and v C ( 0) = 4 V After the switch closes Apply KCL at node a: vC R +C d vC + iL = 0 dt Apply KVL to the right mesh: L d d i L + Vs  vC = 0 vC = L i L + Vs dt dt After some algebra: V 1 d 1 d2 i + iL + iL =  s 2 L dt R C dt LC R LC The characteristic equation is
s 2 + 500 s + 1.6 105 = 0 s1,2 = 250 j 312 rad/s d2 d i + ( 500 ) i L + (1.6 105 ) i L = 320 2 L dt dt 929 After the switch closes the steadystate inductor current is iL() = 2 mA so
i L ( t ) = 0.002 + e 250 t ( A1 cos 312 t + A2 sin 312 t ) v C ( t ) = 6.25 d i L (t ) + 4 dt = 6.25 e 250 t 250 ( A1 cos 312 t  A2 sin 312 t )  312 ( A1 sin 312 t  A2 cos 312 t ) + 4 = 6.25 e 250 t ( 312 A2  250 A1 ) cos 312 t + ( 250 A2 + 312 A1 ) sin 312 t + 4 Let t = 0 and use the initial conditions: iL ( 0+ ) = 0.00233 = 0.002 + A1 0.00433 = A1 vC ( 0+ ) = 4 = 6.25 ( 312 A2  250 A1 ) + 4 Then i L ( t ) = 0.002 + e 250 t ( 0.00433cos 312 t + 0.00345sin 312 t ) = 0.002 + 0.00555 e 250 t cos ( 312 t  36.68 ) A v C ( t ) = 4 + 13.9 e 250 t sin ( 312 t ) V i (t ) = vC (t ) 2000 = 2 + 6.95 e 250 t sin ( 312 t ) mA (checked using LNAP on 7/22/03)
P9.92 First, find the steady state response for t < 0. The input is constant so the capacitor will act like an open circuit at steady state, and the inductor will act like a short circuit. A2 = 250 250 A2 = ( 0.00433) = 0.00347 312 312 i ( 0) = and v (0) = 1 = 0.2 A 1+ 4 4 ( 1) = 0.8 V 1+ 4 930 For t > 0 Apply KCL at node a:
v  Vs d +C v+i = 0 R1 dt Apply KVL to the right mesh: R2 i + L d d i  v = 0 v = R2 i + L iL dt dt d2 d i +5 i +5i =1 2 dt dt After some algebra: L + R1 R 2C d R1 + R 2 d2 Vs i+ i+ i= 2 dt R1 L C dt R1 L C R1 L C The forced response will be a constant, if = B so 1 = d2 d B + 5 B + 5 B B = 0.2 A . 2 dt dt To find the natural response, consider the characteristic equation:
0 = s 2 + 5 s + 5 = ( s + 3.62 )( s + 1.38 ) The natural response is in = A1 e 3.62 t + A2 e1.38 t so i ( t ) = A1 e 3.62 t + A2 e1.38 t + 0.2 Then d v ( t ) = 4 i ( t ) + 4 i ( t ) = 10.48 A1 e3.62 t  1.52 A2 e1.38 t + 0.8 dt At t=0+
0.2 = i ( 0 + ) = A1 + A2 + 0.2 0.8 = v ( 0 + ) = 10.48 A1  1.52 A2 + 0.8 so A1 = 0.246 and A2 = 0.646. Finally i ( t ) = 0.2 + 0.246 e 3.62 t  0.646 e1.38 t A 931 P9.93 First, find the steady state response for t < 0. The input is constant so the capacitors will act like an open circuits at steady state. v1 ( 0 ) = and 1000 (10 ) = 5 V 1000 + 1000
v2 ( 0 ) = 0 V For t > 0, Node equations: v1  10 1 v v d + 106 v1 + 1 2 = 0 1000 6 1000 dt 1 d 2 v1 + 103 v1  10 = v2 6 dt v1  v2 1 d = 106 v2 1000 16 dt 1 d v1  v2 = 103 v2 16 dt After some algebra: d2 d v + ( 2.8 104 ) v1 + ( 9.6 107 ) v1 = 9.6 108 2 1 dt dt The forced response will be a constant, vf = B so d2 d B + ( 2.8 104 ) B + ( 9.6 107 ) B = 9.6 108 2 dt dt To find the natural response, consider the characteristic equation: s 2 + ( 2.8 104 ) s + ( 9.6 107 ) = 0 s1,2 = 4 103 , 2.4 104 The natural response is
vn = A1 e 410 t + A2 e2.410
3 4t B = 10 V . so
v1 ( t ) = A1 e410 t + A2 e2.410
3 4t + 10 At t = 0 932 5 = v1 ( 0 ) = A1 e Next 4103 ( 0 ) + A2 e 2.4104 ( 0 ) + 10 = A1 + A2 + 10 (1) 1 d 2 v1 + 103 v1  10 = v2 6 dt At t = 0 d v1 = 12000v1 + 6000 v2 + 6 104 dt d v1 ( 0 ) = 12000v1 ( 0 ) + 6000 v2 ( 0 ) + 6 104 = 12000 ( 5 ) + 6000 ( 0 ) + 6 104 = 0 dt so
3 4 d v1 ( t ) = A1 4 103 e 410 t + A2 2.4 104 e2.410 t dt ( ) ( ) At t = 0+
0= d 4103 ( 0 ) 2.4104 ( 0 ) v1 ( 0 ) = A1 4 103 e + A2 2.4 104 e = A1 4 103 + A2 2.4 104 dt ( ) ( ) ( ) ( ) so A1 = 6 and A2 = 1. Finally
v1 ( t ) = 10 + e 2.4 10
4t  6 e4 10 3t V for t > 0 P9.94 For t > 0 KCL at top node:
diL ( t ) 1 dv ( t )  5 cos t + iL ( t ) + =0 0.5 dt 12 dt (1) KVL for right mesh: 0.5 Taking the derivative of these equations gives:
d 2iL ( t ) diL ( t ) 1 d 2 v ( t ) of (1) 0.5 + + = 5 sin t dt 12 dt 2 dt 2 dt 2 2 d of ( 2 ) 0.5 d iL ( t ) = 1 d v ( t ) + dv ( t ) dt 12 dt 2 dt 2 dt d (3) diL ( t ) 1 dv ( t ) = + v (t ) 12 dt dt ( 2) ( 4) 933 d 2iL ( t ) di ( t ) Solving for in ( 4 ) and L in ( 2 ) & plugging into ( 3) gives 2 dt dt d 2v ( t ) dv ( t ) +7 + 12v ( t ) = 30sin t dt 2 dt The characteristic equation is: s 2 + 7s+12 = 0 . The natural frequencies are s1,2 = 3, 4 . The natural response is of the form vn (t ) = A1e 3t + A2 e 4t . Try a forced response of the form
v f ( t ) = B1 cos t + B 2 sin t . Substituting the forced response into the differential equation and equating like terms gives B1 = 21 33 and B 2 =  . 17 17 21 33 cos t  sin t 17 17 v ( t ) = vn (t ) + v f ( t ) = A1e3t + A2 e4t + We will use the initial conditions to evaluate A1 and A2. We are given iL ( 0 ) = 0 and v ( 0 ) = 1 V . Apply KVL to the outside loop to get 1 iC ( t ) + iL ( t ) + 1( iC ( t ) ) + v ( t )  5cos t = 0 At t = 0+ iC ( 0 ) = 5cos ( 0 ) + iL ( 0 )  v ( 0 ) 5 + 0  1 = =2 A 2 2 dv ( 0 ) iC ( 0 ) 2 = = = 24 V/s dt 1 12 1 12 21 17 A1 = 25 429 A2 =  17 v(0+ ) = 1 = A1 + A2 + + 33 dv(0 ) = 24 = 3 A1  4 A2  dt 17 Finally, v(t ) = 25e 3t  429e 4t  21cos t + 33sin t V 17 934 P9.95 Use superposition. Find the response to inputs 2u(t) and 2u(t2) and then add the two responses. First, consider the input 2u(t): For 0< t < 2 s Using the operator s = d we have dt (1) KVL: vc ( t ) + siL ( t ) + 4 iL ( t )  2 = 0 KCL: 1 3 s vc ( t ) vc ( t ) = iL ( t ) (2) s 3 Plugging (2) into (1) yields the characteristic equation: ( s 2 + 4 s + 3) = 0 . The natural frequencies are s1,2 = 1 , 3 . The inductor current can be expressed as iL ( t ) = iL (t ) = in (t ) + i f (t ) = ( A1 e t + A2 e3t ) + 0 = A1 e t + A2 e 3t . Assume that the circuit is at steady state before t = 0. Then vc (0+ ) = 0 and iL (0+ ) = 0 . Using KVL we see that (1) diL (0+ ) = 4 2  iL (0+ )  vC (0+ ) = 8 A/s . Then dt iL (0) = 0 = A1 + A2 A1 = 4 , A2 = 4 . diL (0) = 8 =  A1  3 A2 dt Therefore iL (t ) = 4e  t  4e3t A . The response to 2u(t) is 0 t<0 v1 (t ) = 8  4 iL (t ) = t 3t 8  16 e + 16 e V t > 0 . = 8  16 e  t + 16 e 3t u ( t ) V The response to 2u(t2) can be obtained from the response to 2u(t) by first replacing t by t2 everywhere is appears and the multiplying by 1. Therefore, the response to 2u(t2) is v2 (t ) = 8 + 16e  (t  2)  16 e3(t  2) u ( t  2 ) V . By superposition, v(t ) = v1 (t ) + v2 (t ) . Therefore v(t ) = 8  16e t + 16e3t u (t ) + 8 + 16e (t  2)  16 e 3(t  2) u (t  2) V 935 P9.96 First, find the steady state response for t < 0, when the switch is closed. The input is constant so the capacitor will act like an open circuit at steady state, and the inductor will act like a short circuit. 5 = 1.25 A 4 i ( 0) =  and v (0) = 5 V After the switch opens Apply KCL at node a: v d + 0.125 v = i 2 dt Apply KVL to the right mesh: 10 cos t + v + 4 d i+4i =0 dt After some algebra: d2 d v + 5 v + 6 v = 20 cos t 2 dt dt The characteristic equation is
s 2 + 5 s + 6 = 0 s1,2 = 2,  3 Try
vf = A cos t + B sin t d2 d A cos t + B sin t ) + 5 ( A cos t + B sin t ) + 6 ( A cos t + B sin t ) = 20 cos t 2 ( dt dt 936 (  A cos t  B sin t ) + 5 (  A sin t + B cos t ) + 6 ( A cos t + B sin t ) = 20 cos t (  A + 5 B + 6 A) cos t + (  B  5 A + 6 B ) sin t = 20 cos t
Equating the coefficients of the sine and cosine terms yields A =2 and B =2. Then
vf = 2 cos t + 2 sin t v ( t ) = 2 cos t + 2 sin t + A1 e 2 t + A2 e 3 t Next v (t ) d + 0.125 v ( t ) = i ( t ) 2 dt d v (t ) = 8 i (t )  4 v (t ) dt d V 5 v ( 0 ) = 8 i ( 0 )  4 v ( 0 ) = 8   4 ( 5 ) = 30 dt s 4 Let t = 0 and use the initial conditions:
5 = v ( 0 ) = 2 cos 0 + 2 sin 0 + A1 e 0 + A2 e 0 = 2 + A1 + A2 d v ( t ) = 2 sin t + 2 cos t  2 A1 e 2 t  3 A2 e3 t dt 30 = d v ( 0 ) = 2 sin 0 + 2 cos 0  2 A1 e 0  3 A2 e 0 = 2  2 A1  3 A2 dt So A1 = 23 and A2 = 26 and
v ( t ) = 2 cos t + 2 sin t  23 e 2 t + 26 e 3 t V for t > 0 937 P9.97 First, find the steadystate response for t < 0. The input is constant so the capacitor will act like an open circuit at steady state, and the inductor will act like a short circuit.
i ( 0) = 0 A and v (0) = 0 V After t = 0 Apply KCL at node a: C d v=i dt Apply KVL to the right mesh: d 8 i + v + 2 i + 4 (2 + i) = 0 dt d 12 i + v + 2 i = 8 dt 2 1 d d 4 After some algebra: v + ( 6) v + v =  2 dt dt C 2C The forced response will be a constant, vf = B so 1 d2 d 4 B + ( 6) B + B =  2 dt dt C 2C B = 8 V (a) When C = 1/18 F the differential equation is Then v ( t ) = ( A1 + A2 t ) e 3t  8 . Using the initial conditions: d2 d v + ( 6 ) v + ( 9 ) v = 72 . 2 dt dt 2 The characteristic equation is s + 6 s + 9 = 0 s1,2 = 3, 3 938 0 = v ( 0 ) = ( A1 + A2 ( 0 ) ) e0  8 0 = i ( 0) = C So A1 = 8 A2 = 3 A1 = 24 d v ( 0 ) = C 3 ( A1 + A2 ( 0 ) ) e0 + A2 e0 dt
v ( t ) = ( 8 + 24 t ) e 3t  8 V for t > 0 (b) When C = 1/10 F the differential equation is Then v ( t ) = A1 e  t + A2 e 5 t  8 . d2 d v + ( 6 ) v + ( 5 ) v = 40 2 dt dt 2 The characteristic equation is s + 6 s + 5 = 0 s1,2 = 1, 5 Using the initial conditions: 0 = v ( 0 ) = A1 e0 + A2 e0  8 A1 + A2 = 8 A1 = 10 and A2 = 2 d 0 0 0 = v ( 0 ) =  A1 e  5 A2 e  A1  5 A2 = 0 dt So v ( t ) = 10 e  t  2 e 5 t  8 V for t > 0 (c) d2 d v + ( 6 ) v + (10 ) v = 80 2 dt dt 2 The characteristic equation is s + 6 s + 10 = 0 s1,2 = 3 j When C = 1/20 F the differential equation is Using the initial conditions: 0 = v ( 0 ) = e0 ( A1 cos 0 + A2 sin 0 )  8 0= So Then v ( t ) = e 3 t ( A1 cos t + A2 sin t )  8 . A1 = 8 A2 = 3 A1 = 24 d v ( 0 ) = 3 e0 ( A1 cos 0 + A2 sin 0 ) + e0 (  A1 sin 0 + A2 cos 0 ) dt
v ( t ) = e 3 t ( 8cos t + 24 sin t )  8 V for t > 0 939 P9.98 The circuit will be at steady state for t<0: so iL(0+) = iL(0) = 0.5 A and vC(0+) = vC(0) = 2 V. For t>0: Apply KCL at node b to get: 1 1 d 1 1 d = i (t ) + v (t ) i (t ) =  v (t ) L C L 4 4 dt 4 4 dt C Apply KVL at the rightmost mesh to get: 4i Use the substitution method to get d 1 1 d 1 1 d 1 d 4  vC ( t ) + 2  vC ( t ) = 8 vc ( t ) + v ( t ) dt 4 4 dt 4 4 dt 4 dt c or d2 d v t + 6 v (t ) + 2 v (t ) 2 C ( ) C dt dt C d2 d The forced response will be a constant, vC = B so 2 = B + 6 B + 2B B = 1 V . dt dt 2 2= To find the natural response, consider the characteristic equation:
0 = s 2 + 6 s + 2 = ( s + 5.65 )( s + 0.35 ) L( t) + 2 d 1 d i (t ) = 8 vc ( t ) + v ( t ) L dt 4 dt c The natural response is
vn = A1 e
5.65 t 5.65 t + A2 e + A2 e 0.35 t 0.35 t so
vC ( t ) = A1 e +1 Then iL ( t ) = 1 1 d 1 5.65 t 0.35 t + + 0.0875 A2 e vC ( t ) = + 1.41A1 e 4 4 dt 4 940 At t=0+ 2 = vC ( 0 + ) = A1 + A + 1
2 1 1 = iL ( 0+ ) = + 1.41A1 + 0.0875 A 2 2 4 so A1 = 0.123 and A2 = 0.877. Finally
vC ( t ) = 0.123 e 5.65 t + 0.877 e 0.35 t +1 V P9.99 After t = 0 The inductor current and voltage are related be v (t ) = L di ( t ) dt (1) Apply KCL at the top node to get C dv( t ) v( t ) + i (t ) + =5 dt 2 (2) d , and substituting (1) into (2) yields ( s 2 + 4s + 29 ) i ( t ) = 5 . dt The characteristic equation is s 2 + 4 s + 29 = 0 . The characteristic roots are s1,2 =  2 j 5 . Using the operator s = The natural response is of the form in ( t ) = e 2t [ A cos 5t + B sin 5t ] . Try a forced response of the form i f ( t ) = A . Substituting into the differential equation gives A = 5 . Therefore i f ( t ) = 5 A .
The complete response is i(t ) = 5 + e2t [ A cos 5t + B sin 5t ] where the constants A and B are yet to be evaluated using the initial condition: i (0) = 0 = A + 5 A = 5 di (0) di (0) 2A 0 = v ( 0) = L = 0 = 2 A + 5 B B = = 2 dt dt 5 Finally, i (t ) = 5 + e 2t [ 5cos 5t  2sin 5t ] A . P9.910 941 Assume that the circuit is at steady before t = 0. i (0+ ) = i (0 ) = 2 9 = 6 A 2+1 1 v(0+ ) = v(0 ) = 9 1.5 = 4.5 V 2+1 After t = 0: Apply KCL at the top node of the current source to get i ( t ) + 0.5 dv( t ) v( t ) + = is ( t ) dt 1.5 (1) Apply KVL and KCL to get dv( t ) v( t ) 5di( t ) v ( t ) + 0.5 + + i (t ) 0.5 = dt dt 1.5 Solving for i(t) in (1) and plugging into (2) yields
d 2 v( t ) 49 dv( t ) 4 di ( t ) 2 + + v ( t ) = is ( t ) + 2 s 2 dt dt 30 dt 5 5 where is ( t ) = 9 + 3e 2t A (2) Using the operator s = d 49 4 , the characteristic equation is s 2 + s + = 0 and the characteristic 30 5 dt roots are s1,2 =.817 j.365 . The natural response has the form vn (t ) = e0.817t A1 cos (0.365 t ) + A2 sin (0.365 t ) Try a forced response of the form v f (t ) = B0 + B1e
2 t . Substituting into the differential equations gives B0 = 4.5 and B1 = 7.04 . The complete response has the form v(t ) = e.817 t A1 cos(0.365 t ) + A2 sin (0.365 t ) + 4.5  7.04 e 2t Next, consider the initial conditions:
v (0) = 4.5 = A1 + 4.5  7.04 A1 = 7.04 942 d v(0) 4 4 = 2 is (0)  2 i (0)  v(0) = 2(9 + 3)  2(6)  (4.5) = 6 dt 3 3 6= d v( 0 ) = 0.817 A1 + 0.365 A2 + 14.08 A2 = 6.38 dt So the voltage is given by v(t ) = e0.817 t 7.04 cos(0.365 t ) + A2 sin (0.365 t ) + 4.5  7.04 e2t Next the current given by
i (t ) = is (t )  v(t ) d v(t )  0.5 1.5 dt Finally i (t ) = e 0.817 t [ 2.37 cos(0.365t ) + 7.14sin(0.365t ) ] + 6 + 0.65e 2t A P9.911 First, find the steady state response for t < 0. The input is constant so the capacitor will act like an open circuit at steady state, and the inductor will act like a short circuit. va ( 0 ) = 4 i ( 0 )
i ( 0 ) = 2va ( 0 ) = 2 4 i ( 0 ) i ( 0 ) = 0 A
and ( ) v ( 0 ) = 10 V 943 For t > 0 Apply KCL at node 2:
va d + K va + C v=0 R dt KCL at node 1 and Ohm's Law: va =  R i so
d 1+ K R v= i dt C L d i + R i + v  Vs = 0 dt Apply KVL to the outside loop: After some algebra: d2 R d 1+ K R 1+ K R v+ v+ v= Vs 2 dt L dt LC LC The forced response will be a constant, vf = B so d2 d v + 40 v + 144 v = 2304 2 dt dt d2 d B + ( 40 ) B + (144 ) B = 2304 B = 16 V 2 dt dt The characteristic equation is s 2 + 40 s + 144 = 0 s1,2 = 4, 36 . Then Using the initial conditions:
10 = v ( 0+ ) = A1 e0 + A2 e0 + 16 0= d v ( 0+ ) = 4 A1 e0  36 A2 e0 dt  4 A1  36 A2 = 0 A1 + A2 = 6 v ( t ) = A1 e 4 t + A2 e36 t + 16 . A1 = 6.75 and A2 = 0.75 So
v ( t ) = 0.75 e 36 t  6.75 e4 t + 16 V for t > 0 (checked using LNAP on 7/22/03) 944 Section 910: State Variable Approach to Circuit Analysis P9.101 At t = 0 the circuit is source free iL (0) = 0 and v(0) = 0. After t = 0 Apply KCL at the top node to get iL ( t ) + 1 dv( t ) =4 5 dt (1) Apply KVL to the right mesh to get v( t ) (1)
Solving for i1 ( t ) in (1) and plugging into (2) diL ( t )  6 iL ( t ) = 0 dt (2) d 2 v( t ) dv( t ) + 6 + 5v ( t ) = 120 . 2 dt dt The characteristic equation is s 2 + 6 s + 5= 0 . The natural frequencies are s1,2 =1, 5 . The natural response has the form vn (t ) = A1 et + A2 e5t . Try v f ( t ) = B as the forced response. Substituting into the differential equation gives B = 24 so v f ( t ) = 24 V. The complete response has the form v (t ) = A1 et + A2 e5t + 24 . Now consider the initial conditions. From (1)
v(0) = 0 = A1 + A2 + 24 dv(0) = 20 =  A1 5 A2 dt dv(0) = 20  5 iL (0) = 20 V . Then s dt A1= 25, A2 = 1 Finally v (t ) =  25e t + e 5t + 24 V . 945 P9.102 Before t = 0 there are no sources in the circuit so iL (0) = 0 and v(0) = 0 . After t = 0 we have: Apply KCL at the top node to get iL ( t ) = 4  1 dv ( t ) 10 dt (1) Apply KVL to the left mesh to get v( t )  diL ( t )  6iL ( t ) = 0 dt (2) Substituting iL ( t ) from (1) into (2) gives
d 2 v( t ) dv( t ) +6 + 10v( t ) = 240 2 dt dt The characteristic equation is s 2 + 6 s + 10 = 0 . The natural frequencies are s1,2 = 3 j . The response. Substituting into the differential equation gives B = 24 so v f ( t ) = 24 V. The complete response has the form v(t ) = e 3t A1 cos t + A2 sin t + 24 . Now consider the initial conditions. From (1)
dv(0) = 40  10 iL (0) = 40 V . Then s dt natural response has the form vn (t ) = e 3t A1 cos t + A2 sin t . Try v f ( t ) = B as the forced v (0) = 0 = A1 + 24 A1 = 24 dv(0) = 40 = 3 A1 + A2 = 72 + A2 A2 = 32 dt Finally, v (t ) = e 3t [ 24 cos t 32sin t ] + 24 V 946 P9.103 Assume that the circuit is at steady state before t = 0 so iL (0) = 3 A and v(0) = 0 V . After t = 0 we have KCL: i ( t ) + C KVL: v( t ) = L dv( t ) v( t ) + + 6=0 dt R di ( t ) dt i (t ) + C
d 2i ( t ) 6 1 di ( t ) 1 + + i (t ) = 2 dt R C dt LC LC d di( t ) 1 di ( t ) L + L + 6=0 dt dt R dt d 2i ( t ) di ( t ) + 100 + 250i ( t ) = 1500 2 dt dt The characteristic equation is s 2 + 100 s + 250 = 0 . The natural frequencies are s1,2 = 2.57,  97.4 . The natural response has the form in (t ) = A1 e2.57 t + A2 e97.4t . Try ( t ) = B as the forced response. Substituting into the differential equation gives B = 6 so i f ( t ) = 6 A . The complete response has the form i(t ) = A1 e2.57 t + A2 e97.4t  6 .
i
f Now consider the initial conditions:
i (0) = A1 + A2  6 = 3 A1 = 3 .081 di (0) = 0 =  2.57 A1 97.4 A2 A2 =0.081 dt Finally: i (t ) = 3. 081 e v(t ) = .2
2.57 t .081e 97.4 t 6 A di ( t ) = 1.58e dt 2.57 t +1.58e97.4t V 947 P9.104 Apply KCL to the supernode corresponding to the dependent voltage source to get ix ( t )  2ix ( t )  0.01 dv ( t ) vx ( t ) + =0 2 dt Apply KCL at node 1 to get i ( t )  2ix ( t ) + (Encircled numbers are node numbers.) vx ( t ) =0 2 Apply KVL to the topright mesh to get vx ( t ) + v ( t )  0.1 di ( t ) =0 dt Apply KVL to the outside loop to get ix ( t ) = 2 vx ( t )  v ( t ) . Eliminate ix ( t ) to get dv ( t ) 5 =0 vx ( t ) + v ( t )  0.01 2 dt 9 i ( t ) + vx ( t ) + 2 v ( t ) = 0 2 d i (t ) vx ( t ) = v ( t ) + 0.01 dt dv ( t ) di ( t ) + 0.25 =0 dt dt di ( t ) 2.5 v ( t ) + i ( t ) + 0.45 =0 dt 1.5 v ( t )  0.01 Using the operator s =
d we have dt (1.5  .01s )v ( t ) + (.25s ) i ( t ) = 0
(2.5)v( t ) + (1+.45s ) i ( y ) = 0 Then eliminate vx ( t ) to get The characteristic equation is s 2 +13.33 s + 333.33 = 0 . The natural frequencies The forced response is v are s1 , s2 = 6.67 j 17 . The natural response has the form vn (t ) = [ A cos17 t + B sin17 t ] e6.67 t . v(t ) = [ A cos17 t ( t ) = 0 . The complete response has the form + B sin 17 t ] e6.67 t .
f 948 The given initial conditions are i (0) = 0 and v (0) = 10 V. Then
v(0) =10 = A and dv(0) =111=  6.67 A +17 B B =2.6 dt Finally i (t ) = [3.27 sin 17 t ] e6.67 t A . (Checked using LNAP on 7/22/03)
P9.105
v(0) 10 = A. 3 3 Assume that the circuit is at steady state before t = 0 so v(0) = 10 V and iL (0) = The switch is open when 0 < t < 0.5 s For this series RLC circuit we have: = R 1 = 3 and 02 = = 12 2L LC  2 02 = s1,2 = 3 j 3 The natural response has the form vn (t ) = e 3t ( A cos1.73 t + B sin1.72 t ) . There is no source so v f ( t ) =0 . The complete response has the form v (t ) = e 3t ( A cos1.73 t + B sin1.72 t ) .
Next v(0) = 10 = A A= 10 dv(0) i ( 0 ) 10 3 = = =  20 = 3 A +1.73 B B =5.77 dt C 16 so v(t ) = e3t (10 cos1.73 t + 5.77 sin1.73 t ) V i(t ) = e3t ( 3.33 cos1.73 t  5.77 sin1.73 t ) A In particular,
1.73 1.73 v (0.5) = e 1.5 10 cos + 5.77 sin = 0.2231 ( 6.4864 + 4.3915 ) = 2.43 V 2 2 and
1.73 1.73 i (0.5) = e 1.5 3.33cos 5.77 sin = 0.2231 ( 2.1600  4.3915 ) = 0.50 A 2 2 949 The switch is closed when t > 0.5 s Apply KCL at the top node:
v( t ) 30 1 dv( t ) + iL ( t ) + =0 6 6 dt dv( t ) 1 iL ( t ) = 5  v( t ) + 6 dt 2 d iL ( t ) 1 dv( t ) d v( t ) = + dt 6 dt dt 2 Apply KVL to the right mesh: 1 diL ( t ) v( t ) = 3 iL ( t ) + 2 dt The circuit is represented by the differential equation d 2v ( t ) dv ( t ) +7 + 18 v ( t ) = 180 2 dt dt The characteristic equation is 0 = s 2 + 7 s + 18 . The natural frequencies are s1,2 = 3.7 j 2.4 . The natural response has the form vn (t ) = e 3.5 t ( A cos 2.4 t + B sin 2.4 t ) . The forced response is v f ( t ) = 10 V . The complete response has the form v (t ) = e 3.5 t ( A cos 2.4 t + B sin 2.4 t ) + 10 .
v (0.5) = e 3.50.5 ( A cos1.2 + B sin1.2 ) = 0.063 A + 0.162 B Next dv ( 0.5 ) = e3.50.5 ( 3.5 A + 2.4 B ) cos1.2  ( 3.5B + 2.4 A ) sin1.2 dt = e3.50.5 ( 3.5cos1.2  2.4sin1.2 ) A + e3.50.5 ( 2.4 cos1.2  3.5sin1.2 ) B = 0.6091A  0.4158B Using the initial conditions yields 2.43=v(0.5) = 0.063 A+ 0.162 B A=20.65 dv(0.5) i ( 0.5 ) 1 2 B = 23.03 = = =3=0.6091A 0.4158B dt C 16 v(t ) = e 3.5 t ( 20.65 cos 2.4 t + 23.03 sin 2.4 t ) + 10 Finally In summary e 3t (10 cos1.73 t + 5.77 sin1.73 t ) V 0<t <0.5 v(t ) = 3.5 t e ( 20.65 cos 2.4 t + 23.03 sin 2.4 t )+10 V 0.5<t 950 Section 911: Roots in the Complex Plane P9.111 After t = 0 i1 + i 2 + 2 103 d i1 dt 2 103 d i1 dt 2000 6 =0 d i2 dt = 3000 i 2 + 2 103 Using the operator s = d yields dt 2000 + 2 103 s i1 6 2000 = 3 3 2 10 s 3000 + 2 10 s i 2 0 s 2 + 3.5 106 s + 1.5 1012 = 0 s1,2 = 5 105 , 3 106 P9.112 From P9.71
s2 + 1 1 1 1 = 0 s2 + =0 s+ s+ 6 RC LC ( 250 ) ( 5 10 ) ( 0.8) ( 5 106 ) s 2 + 800 s + 250000 = 0 s1,2 = 400 j 300 P9.113 dv( t ) v( t ) 1 KCL: i L ( t ) = 106 + 4 dt 4000 di ( t ) KVL: vs ( t ) = 4 L + v( t ) dt d 2v ( t ) dv ( t ) dv( t ) v( t ) d 1 v ( t ) = 4 106 + + v ( t ) = 106 + 103 + v (t ) 2 s dt 4 dt 4000 dt dt 951 Characteristic equation: s 2 + 103 s + 106 = 0 Characteristic roots: s1,2 = 500 j 866 P9.114 Before t = 0 the voltage source voltage is 0 V so vb (0+) = vb (0) = 0 V and i (0+) = i (0) = 0 A . Apply KCL at node a to get va (0+ ) 36 v (0+ )  vb (0+ )  i (0+) + a = 0 va (0+ ) + 2 va (0+ ) = 36 va (0) = 12 V 12 6 After t = 0 the node equations are:  va ( t )  vs ( t ) 1 t v ( t )  va ( t ) + ( vb ( )  va ( ) ) d + b =0 0 12 6 L C d vb ( t ) vb ( t )  va ( t ) 1 t + + ( vb ( )  va ( ) ) d = 0 6 dt L 0 Using the operator s = d we have dt
v (t ) 1 1 1 1 1 + + va ( t ) +   vb ( t ) = s 6 12 s 12 6 s 1 1 1 1 1   va ( t ) + s + + vb ( t ) = 0 6 s 18 6 s Using Cramer's rule 952 ( s 2 +5s + 6) vb ( t ) = ( s + 6) vs ( t ) =( s + 6) ( 36 ) The characteristic equation is s 2 + 5s + 6 = 0 . The natural frequencies are s1,2 = 2, 3 . The natural response has the form vn (t ) = A1 e 2 t + A2 e 3 t . Try v f ( t ) = B as the forced response. Substituting into the differential equation gives B = 36 so v f ( t ) = 36 V. The complete response has the form
vb (t ) = A1 e 2 t + A2 e 3t + 36 . Next vb (0+ ) = 36 + A1 + A2 dvb + (0 ) = 2 A1  3 A2 dt Apply KCL at node a to get 1 dvb ( t ) vb ( t )  va ( t ) + + i (t ) = 0 18 dt 6
+ At t = 0+ 1 1 d vb ( 0 (2 A1  3 A2 ) = 18 18 dt ) = v ( 0 )v ( 0 )  i
+ +
a b 6 (0+ ) = 1260  0 = 2 So
0 = vb (0+ ) =36+ A1 + A 2 1 ( 2 A 1  3 A 2 ) = 2 18 A1 = 72, A2 = 36 Finally vb ( t ) = 36  72e 2 t + 36e 3t V for t 0 953 PSpice Problems
SP 91 Make three copies of the circuit: one for each set of parameter values. (Cut and paste, but be sure to edit the labels of the parts so, for example, there is only one R1.) 954 V(C1:2), V(C2:2) and V(C3:2) are the capacitor voltages, listed from top to bottom. 955 SP 92 Make three copies of the circuit: one for each set of parameter values. (Cut and paste, but be sure to edit the labels of the parts so, for example, there is only one R1.) 956 V(R2:2), V(R4:2) and V(R6:2) are the output voltages, listed from top to bottom. 957 SP 93 958 SP 94 959 Verification Problems
VP 91 This problem is similar to the verification example in this chapter. First, check the steadystate inductor current v ( t ) 25 i (t ) = s = = 250 mA 100 100 This agrees with the value of 250.035 mA shown on the plot. Next, the plot shows an underdamped response. That requires 12 103 = L < 4 R 2C = 4(100) 2 (2 106 ) = 8 102 This inequality is satisfied, which also agrees with the plot. The damped resonant frequency is given by =
d 1 LC 1  2 RC 2 1 1 =  = 5.95 103 6 6 3 2(100)(2 10 ) ( 2 10 )(12 10 ) 2 The plot indicates a maxima at 550.6s and a minima at 1078.7s. The period of the damped oscillation is T d = 2 (1078.7 s  550.6 s) = 1056.2 s Finally, check that
5.95 103 = d = 2 2 = = 5.949 103 6 1056.2 10 Td The value of d determined from the plot agrees with the value obtained from the circuit. The plot is correct. VP 92 This problem is similar to the verification example in this chapter. First, check the steadystate inductor current. v ( t ) 15 i (t ) = s = = 150 mA 100 100 960 This agrees with the value of 149.952 mA shown on the plot. Next, the plot shows an underdamped response. This requires 8 103 = L < 4 R 2C = 4 (100)2 (0.2 106 ) = 8 103 This inequality is not satisfied. The values in the circuit would produce a critically damped, not underdamped, response. This plot is not correct. Design Problems
DP 91 When the circuit reaches steady state after t = 0, the capacitor acts like an open circuit and the inductor acts like a short circuit. Under these conditions vC ( ) = The specifications require that vC ( ) = 1 so 2 R2 R2 R1 + R 2 1 1 = 2 R1 + R 2 R1 = R 2 Next, represent the circuit by a 2nd order differential equation: KCL at the top node of R2 gives: KVL around the outside loop gives: Use the substitution method to get vC ( t ) R2 vs ( t ) = L +C d vC ( t ) = iL ( t ) dt d iL ( t ) + R1 iL ( t ) + vC ( t ) dt 961 vs ( t ) = L v (t ) d vC ( t ) d d + C vC ( t ) + R1 C + C vC ( t ) + vC ( t ) R2 dt R 2 dt dt L d R1 d2 + R1 C vC ( t ) + 1 + vC ( t ) + v t R2 dt R2 C ( ) dt 2 = s 2 + 6 s + 8 = ( s + 2 )( s + 4 ) = 0 = LC The characteristic equation is
R1 1+ 1 R1 R2 + s+ s2 + R 2 C L LC Equating coefficients of like powers of s:
1 R2 C Using R1 = R 2 = R gives 1 R + =6 RC L 1 =4 LC 1 H and 4 + R1 L 1+ = 6 and R1 R2 =8 LC These equations do not have a unique solution. Try C = 1 F. Then L = 1 3 1 + 4 R = 6 R 2  R + = 0 R = 1.309 or R = 0.191 R 2 4 Pick R = 1.309 . Then vc ( t ) = iL ( t ) = At t = 0+ vC ( t ) 1.309 1 + A1 e 2 t + A2 e4 t V 2 + d vC ( t ) = 1.236 A1 e2 t  3.236 A2 e4 t + 0.3819 dt 0 = vc 0+ = A1 + A2 + 0.5
1 2 0 = iL 0
( ) = 1.236 A  3.236 A
+ ( ) + 0.3819 Solving these equations gives A1 = 1 and A2 = 0.5, so vc ( t ) = 1 2 t 1 4 t e + e V 2 2 962 DP 92 When the circuit reaches steady state after t = 0, the capacitor acts like an open circuit and the inductor acts like a short circuit. Under these conditions vC ( ) = The specifications require that vC ( ) = 1 so 4 R2 R2 R1 + R 2 1 1 = 4 R1 + R 2 3 R 2 = R1 Next, represent the circuit by a 2nd order differential equation: KCL at the top node of R2 gives: KVL around the outside loop gives: Use the substitution method to get vs ( t ) = L v (t ) d vC ( t ) d d + C vC ( t ) + R1 C + C vC ( t ) + vC ( t ) R2 dt R 2 dt dt vC ( t ) R2 vs ( t ) = L +C d vC ( t ) = iL ( t ) dt d iL ( t ) + R1 iL ( t ) + vC ( t ) dt L d R1 d2 v t + + R1 C vC ( t ) + 1 + v t 2 C ( ) R2 dt R2 C ( ) dt The characteristic equation is R1 1+ 1 R1 R2 2 2 2 + s+ = s + 4s + 4 = ( s + 2 ) = 0 s + R 2 C L LC Equating coefficients of like powers of s: R 1+ 1 R1 R2 1 + = 4 and =4 R2 C L LC = LC 963 Using R 2 = R and R1 = 3R gives 1 3R + =4 RC L 1 =1 LC These equations do not have a unique solution. Try C = 1 F. Then L = 1 H and 1 4 1 1 + 3 R = 4 R 2  R + = 0 R = 1 or R = R 3 3 3 Pick R = 1 . Then R1 = 3 and R 2 = 1 . vc ( t ) = iL ( t ) = vC ( t ) + At t = 0+ 1 + ( A1 + A2 t ) e 2 t V 4 d 1 vC ( t ) = + dt 4 (( A 2  A1 )  A2 t e 2 t ) 0 = vc 0+ = A1 + 0 = iL 0+ = ( ) 1 4 ( ) 1 + A2  A1 4 Solving these equations gives A1 = 0.25 and A2 = 0.5, so vc ( t ) =
DP 93 1 1 1 2 t  + t e V 4 4 2 When the circuit reaches steady state after t = 0, the capacitor acts like an open circuit and the inductor acts like a short circuit. Under these conditions R2 vC ( ) = 1 R1 + R 2 4 The specifications require that vC ( ) = so 5 964 R2 4 = 5 R1 + R 2 4 R1 = R 2 Next, represent the circuit by a 2nd order differential equation: KCL at the top node of R2 gives: KVL around the outside loop gives: Use the substitution method to get vs ( t ) = L v (t ) d vC ( t ) d d + C vC ( t ) + R1 C + C vC ( t ) + vC ( t ) R2 dt R 2 dt dt L d R1 d2 v t + + R1 C vC ( t ) + 1 + v t 2 C ( ) R2 dt R2 C ( ) dt = s 2 + 4s + 20 = ( s + 2  j 4 )( s + 2 + j 4 ) = 0 vC ( t ) R2 vs ( t ) = L +C d vC ( t ) = iL ( t ) dt d iL ( t ) + R1 iL ( t ) + vC ( t ) dt = LC The characteristic equation is
R1 1+ 1 R1 R2 + s+ s2 + R 2 C L LC Equating coefficients of like powers of s: R1 1 + = 4 and R2 C L Using R1 = R and R 2 = 4 R gives 1 = 16 LC 1 1 These equations do not have a unique solution. Try C = F . Then L = H and 8 2 2 + 2 R = 4 R2  2R + 1 = 0 R = 1 R Then R1 = 1 and R 2 = 4 . Next vc ( t ) = 0.8 + e 2 t ( A1 cos 4 t + A2 sin 4 t ) V 1 R + = 4 and 4R C L 1+ R1 R2 = 20 LC 965 iL ( t ) = At t = 0
+ vC ( t ) 4 + A 2 2 t A1 1d vC ( t ) = 0.2 + e cos 4 t  e2 t sin 4 t 8 dt 2 2 0 = vc 0+ = 0.8 + A1 0 = iL 0+ = 0.2 + ( ) ( ) A2 2 Solving these equations gives A1 = 0.8 and A2 = 0.4, so
vc ( t ) = 0.8  e 2 t ( 0.8cos 4 t + 0.4sin 4 t ) V DP 94 When the circuit reaches steady state after t = 0, the capacitor acts like an open circuit and the inductor acts like a short circuit. Under these conditions vC ( ) = The specifications require that vC ( ) = 1 so 2 R2 R2 R1 + R 2 1 1 = 2 R1 + R 2 R1 = R 2 Next, represent the circuit by a 2nd order differential equation: KCL at the top node of R2 gives: KVL around the outside loop gives: Use the substitution method to get vC ( t ) R2 vs ( t ) = L +C d vC ( t ) = iL ( t ) dt d iL ( t ) + R1 iL ( t ) + vC ( t ) dt 966 vs ( t ) = L v (t ) d vC ( t ) d d + C vC ( t ) + R1 C + C vC ( t ) + vC ( t ) R2 dt R 2 dt dt L d R1 d2 vC ( t ) + + R1 C vC ( t ) + 1 + v t R2 dt R2 C ( ) dt 2 = s 2 + 4s + 20 = ( s + 2  j 4 )( s + 2 + j 4 ) = 0 = LC The characteristic equation is
R1 1+ 1 R1 R2 + s+ s2 + R 2 C L LC Equating coefficients of like powers of s: R1 1 + = 4 and R2 C L Using R1 = R 2 = R gives 1 R + = 4 and RC L Substituting L = 1 into the first equation gives 10 C 1 = 10 LC 1+ R1 R2 = 20 LC ( RC ) 2 0.4 0.42  4 ( 0.1) 4 1  ( RC ) + = 0 RC = 10 10 2 Since RC cannot have a complex value, the specification cannot be satisfied. DP 95 When the circuit reaches steady state after t = 0, the capacitor acts like an open circuit and the inductor acts like a short circuit. Under these conditions 967 vC ( ) = R2 R1 + R 2 1, iL ( ) = 1 so 2 R2 1 R1 + R 2 and vo ( ) = R2 R1 + R 2 1 The specifications require that vo ( ) = 1 = 2 R1 + R 2 R1 = R 2 Next, represent the circuit by a 2nd order differential equation: KVL around the righthand mesh gives: KCL at the top node of the capacitor gives: Use the substitution method to get
vs ( t ) = R1 C = R1 LC d d d L iL ( t ) + R 2 iL ( t ) + L iL ( t ) + R 2 iL ( t ) + R1 iL ( t ) dt dt dt d2 d i t + L + R1 R 2 C ) iL ( t ) + ( R1 + R 2 ) iL ( t ) 2 L( ) ( dt dt d iL ( t ) + R 2 iL ( t ) dt vs ( t )  vC ( t ) d  C vC ( t ) = iL ( t ) R1 dt vC ( t ) = L Using iL ( t ) = vo ( t ) gives R2 vs ( t ) = R1 R2 LC L d R1 + R 2 d2 + R1 C vo ( t ) + v t + v t 2 o( ) R2 dt R2 o ( ) dt = s 2 + 6 s + 8 = ( s + 2 )( s + 4 ) = 0 The characteristic equation is
R2 1+ 1 R2 R1 + s2 + s+ R1 C L LC Equating coefficients of like powers of s: R2 1 + = 6 and R1 C L Using R1 = R 2 = R gives 1 R + =6 RC L 1+ R2 R1 =8 LC 1 =4 LC 1 H and 4 These equations do not have a unique solution. Try C = 1 F. Then L = 968 1 3 1 + 4 R = 6 R 2  R + = 0 R = 1.309 or R = 0.191 R 2 4 Pick R = 1.309 . Then 1 + A1 e 2 t + A2 e 4 t V 2 A1 2 t A2 4 t v (t ) 1 iL ( t ) = o e + e V = + 1.309 2.618 1.309 1.309 vo ( t ) = vC ( t ) = 1.309 iL ( t ) + At t = 0+ 1 d 1 iL ( t ) = + 0.6167 A1 e2 t + 0.2361 A2 e4 t 4 dt 2 0 = iL 0+ = 0 = vC 0+ = ( ) A1 A2 1 + + 2.618 1.309 1.309 ( ) 1 + 0.6167 A1 + 0.2361 A2 2 Solving these equations gives A1 = 1 and A2 = 0.5, so vo ( t ) = 1 2 t 1 4 t e + e V 2 2 DP 96 When the circuit reaches steady state after t = 0, the capacitor acts like an open circuit and the inductor acts like a short circuit. Under these conditions vC ( ) = R2 R1 + R 2 1, iL ( ) = 3 so 4 3R1 = R 2 1 R1 + R 2 and vo ( ) = R2 R1 + R 2 1 The specifications require that vo ( ) = R2 3 = 4 R1 + R 2 969 Next, represent the circuit by a 2nd order differential equation: KVL around the righthand mesh gives: KCL at the top node of the capacitor gives: Use the substitution method to get
vs ( t ) = R1 C = R1 LC d d d L iL ( t ) + R 2 iL ( t ) + L iL ( t ) + R 2 iL ( t ) + R1 iL ( t ) dt dt dt d2 d i t + L + R1 R 2 C ) iL ( t ) + ( R1 + R 2 ) iL ( t ) 2 L( ) ( dt dt d iL ( t ) + R 2 iL ( t ) dt vs ( t )  vC ( t ) d  C vC ( t ) = iL ( t ) R1 dt vC ( t ) = L Using iL ( t ) = vo ( t ) gives R2 vs ( t ) = R1 R2 LC L d R1 + R 2 d2 + R1 C vo ( t ) + vo ( t ) + v t R2 dt R2 o ( ) dt 2 = s 2 + 4 s + 4 = ( s + 2 )2 = 0 The characteristic equation is
R2 1+ 1 R2 R1 + s2 + s+ R1 C L LC Equating coefficients of like powers of s: R2 1 + = 4 and R1 C L Using R1 = R and R 2 = 3R gives 1 3R + = 4 and RC L 1+ R2 R1 =4 LC 1 =1 LC These equations do not have a unique solution. Try C = 1 F. Then L = 1 H and 1 4 1 1 + 3 R = 4 R 2  R + = 0 R = 1 or R = R 3 3 3 Pick R = 1 . Then R1 = 1 and R 2 = 3 . vo ( t ) = 3 + ( A1 + A2 t ) e 2 t V 4 970 iL ( t ) = vo ( t ) 3 = 1 A1 A2 2 t t e V + + 4 3 3 vC ( t ) = 3 iL ( t ) + At t = 0+ 3 A1 A2 A2 2 t d iL ( t ) = + + t e + 4 3 3 3 dt 0 = iL ( 0 + ) = A1 + 1 4 3 3 A1 A2 0 = vC ( 0 + ) = + + 4 3 3 Solving these equations gives A1 = 0.75 and A2 = 1.5, so vo ( t ) = 3 3 3 2 t  + t e V 4 4 2 DP 97 When the circuit reaches steady state after t = 0, the capacitor acts like an open circuit and the inductor acts like a short circuit. Under these conditions vC ( ) = R2 R1 + R 2 1, iL ( ) = 1 R1 + R 2 and vo ( ) = R2 R1 + R 2 1 1 The specifications require that vo ( ) = so 5 R2 1 = 5 R1 + R 2 R1 = 4 R 2 Next, represent the circuit by a 2nd order differential equation: KVL around the righthand mesh gives: KCL at the top node of the capacitor gives: d iL ( t ) + R 2 iL ( t ) dt vs ( t )  vC ( t ) d  C vC ( t ) = iL ( t ) R1 dt vC ( t ) = L 971 Use the substitution method to get
vs ( t ) = R1 C = R1 LC d d d L iL ( t ) + R 2 iL ( t ) + L iL ( t ) + R 2 iL ( t ) + R1 iL ( t ) dt dt dt d2 d i t + L + R1 R 2 C ) iL ( t ) + ( R1 + R 2 ) iL ( t ) 2 L( ) ( dt dt Using iL ( t ) = vo ( t ) gives R2 vs ( t ) = R1 R2 LC L d R1 + R 2 d2 + R1 C vo ( t ) + v t + v t 2 o( ) R2 dt R2 o ( ) dt = s 2 + 4s + 20 = ( s + 2  j 4 )( s + 2 + j 4 ) = 0 The characteristic equation is
R2 1+ 1 R2 R1 + s2 + s+ R1 C L LC Equating coefficients of like powers of s: R2 1 + = 4 and R1 C L Using R 2 = R and R1 = 4 R gives 1 R + = 4 and 4R C L These equations do not have a unique solution. Try C = 1 = 16 LC 1 1 F . Then L = H and 8 2 1+ R2 R1 = 20 LC 2 + 2 R = 4 R2  2R + 2 = 0 R = 1 R Then R1 = 4 and R 2 = 1 . Next vo ( t ) = 0.2 + e 2 t ( A1 cos 4 t + A2 sin 4 t ) V iL ( t ) = vo ( t ) 1 = 0.2 + e 2 t ( A1 cos 4 t + A2 sin 4 t ) V vC ( t ) = iL ( t ) + At t = 0+ 1 d iL ( t ) = 0.2 + 2 A2 e2 t cos 4 t  2 A1 e2 t sin 4 t 2 dt 972 0 = iL 0+ = 0.2 + A1 0 = vC
+ ( ) ( 0 ) = 0.2 + 2 A 2 Solving these equations gives A1 = 0.8 and A2 = 0.4, so
vc ( t ) = 0.2  e 2 t ( 0.2 cos 4 t + 0.1sin 4 t ) V DP 98 When the circuit reaches steady state after t = 0, the capacitor acts like an open circuit and the inductor acts like a short circuit. Under these conditions vC ( ) = R2 R1 + R 2 1, iL ( ) = 1 so 2 R2 1 R1 + R 2 and vo ( ) = R2 R1 + R 2 1 The specifications require that vC ( ) = 1 = R1 = R 2 2 R1 + R 2 Next, represent the circuit by a 2nd order differential equation: KVL around the righthand mesh gives: KCL at the top node of the capacitor gives: Use the substitution method to get
vs ( t ) = R1 C = R1 LC d d d L iL ( t ) + R 2 iL ( t ) + L iL ( t ) + R 2 iL ( t ) + R1 iL ( t ) dt dt dt d2 d i t + L + R1 R 2 C ) iL ( t ) + ( R1 + R 2 ) iL ( t ) 2 L( ) ( dt dt d iL ( t ) + R 2 iL ( t ) dt vs ( t )  vC ( t ) d  C vC ( t ) = iL ( t ) R1 dt vC ( t ) = L Using iL ( t ) = vo ( t ) gives R2 973 vs ( t ) = R1 R2 LC L d R1 + R 2 d2 + R1 C vo ( t ) + v t + v t 2 o( ) R2 dt R2 o ( ) dt = s 2 + 4s + 20 = ( s + 2  j 4 )( s + 2 + j 4 ) = 0 The characteristic equation is
R2 1+ 1 R2 R1 + s2 + s+ R1 C L LC Equating coefficients of like powers of s: R2 1 + = 4 and R1 C L Using R1 = R 2 = R gives 1 R + =4 RC L Substituting L = 1 into the first equation gives 10 C 1 = 10 LC 1+ R2 R1 = 20 LC ( RC ) 2 0.4 0.42  4 ( 0.1) 4 1  ( RC ) + = 0 RC = 10 10 2 Since RC cannot have a complex value, the specification cannot be satisfied. 974 DP 99 Let's simulate the three copies of the circuit simultaneously. Each copy uses a different value of the inductance. The PSpice transient response shows that when L = 1 H the inductor current has its maximum at approximately t=0.5 s. Consequently, we choose L = 1 H. 975 Chapter 10 Sinusoidal SteadyState Analysis
Exercises
Ex. 10.31 (a) (b)
T = 2 / = 2 / 4 v leads i by 30  (70) = 100 Ex. 10.32
v ( t ) = 3cos 4 t + 4sin 4 t = (3) 2 + (4) 2 cos 4 t  tan 1 4 ( ( 3 )) = 5 cos(4 t 53 ) Ex. 10.33 12 i ( t ) = 5 cos 5t + 12 sin 5t = (5) 2 + (12) 2 cos 5 t  180 + tan 1 = 13 cos (5 t 112.6) 5 Ex. 10.41 KCL: is ( t ) = v( t ) d + C v (t ) R dt v( t ) d I v (t ) + = m cos t dt RC C Try v f ( t ) = A cos t + B sin t & plug into above differential equation to get  A sin t + B cos t + 1 I ( A cos t + B sin t ) = m cos t RC C Equating sin t & cos t terms yields R Im R2 C Im and B = A = 1+ 2 R 2 C 2 1+ 2 R 2 C 2
Therefore
v f (t ) = R Im R2 C Im cos t + sin t = 1+ 2 R 2 C 2 1+ 2 R 2 C 2 R Im 1+ R C
2 2 2 cos t  tan 1 ( RC ) 101 Ex. 10.42 KVL :  10 + j 3 I + 2 I = 0 I =
Therefore
i (t ) = 10 = 2+ j 3 100 13 56.3 = 10  56.3 A 13 10 cos (3 t  56.3 ) A 13 Ex. 10.51
10 = 4.24 e j 45 = 3 j 3 2.36 e j 45 Ex. 10.52 j 32 32e j 90 32 j (90111) = = = 3.75 e  j 21 e 3+ j 8 8.54 e j111 8.54 Ex. 10.61 (a) i = 4 cos( t  80 ) = Re{4 e j t e  j 80 } I = 4 e  j 80 = 4  80 A (b) i = 10 cos( t + 20 ) = Re{10 e j t e j 20 } I = 10e j 20 = 1020 (c) i = 8sin ( t  20 ) = 8cos ( t  110 ) = 8 Re{e j t e  j110 } I = 8e  j110 = 8  110 A Ex. 10.62 (a) V = 10  140 = 10 e  j140 V v(t ) = Re{10 e  j140 e j t } = 10 cos ( t  140) V (b) V = 80 + j 75 = 109.743.2 = 109.7 e j 43.2 v (t ) = Re{109.7 e j 43.2 e j t } = 109.7 cos( t + 43.2) V 102 Ex. 10.63 d v + v = 10 cos 100 t dt ( 0.01)( j 100 )V + V =10 0.01 10 =7.071  45 1+ j v = 7.071 cos 100 t V V= Ex. 10.64 vs = 40 cos100t = Re 4 e j100 t KVL:
i (t ) + 10 10 3 di (t ) 1 + dt 510 3 { } t  i (t ) dt = vS Assume i (t ) = Ae j100 t where A is complex number to be determined. Plugging into the differential equation yields Ae j100 t + j Ae j100 t + ( j 2 A)e j100 t = 4 e j100 t In the time domain: A= 4 = 2 2 e j 45 1 j i (t ) = Re 2 2 e j100 t e j 45 = Re 2 2 e j (100 t 45) = 2 2 cos (100 t + 45 ) A Ex. 10.71 (a) v = R i = 10 (5 cos100 t ) = 50 cos 100 t (b) di v = L = 0.01[5(100) sin100 t ] = 5sin100 t = 5cos (100 t + 90 ) V dt (c) 1 v = i dt = 103 5cos100 t dt = 50sin100 t = 50 cos (100 t  90) V C { } { } Ex. 10.72
i=C dv = 10 106 [100(500) sin (500 t + 30)] dt =  0.5sin (500 t +30) = 0.5sin (500 t + 210) = 0.5cos(500t +120) A 103 Ex. 10.73 From Figure E10.73 we get
i (t ) = I m sin t = I m cos( t  90) A I = I m  90A v(t ) = Vm cos t V = Vm 0 V The voltage leads the current by 90 so the element is an inductor:
Z eq = V 0 V V = m = m 90 I m 90 Im I Vm Im L = Vm Im Also
Z eq = j L = L 90 L = Ex. 10.81 ZR = 8 , ZC =
1 j5 1 12 ZL2 = j 5 (4) = j 20 and VS = 5 90 V. = 2.4 j 2.4 = =  j 2.4 , ZL1 = j 5 (2) = j 10 , j j j Ex. 10.82 ZR = 8 , ZC =
1 j3 1 12 ZL2 = j 3 (4) = j 12 and IS = 4 15 V. = j4 4 = =  j 4 , ZL1 = j 3 (2) = j 6 , j j j 104 Ex 10.91 V1 ( ) = V 2 ( ) =
j10 5 e  j 90 = 3.9 e  j 51 8 + j10 j 20 5 e  j 90 = 5.68 e  j 90 j 20  j 2.4 V ( ) = V1 ( )  V 2 ( ) = 3.9 e  j 51  5.68 e  j 90 = 3.58 e j 47 Ex 10.92
V1 ( ) = V 2 ( ) = 8 ( j6) 4 e j15 = 19.2 e j 68 8 + j6 j12 (  j 4 ) 4 e j15 = 24 e  j 75 j12  j 4 V ( ) = V1 ( ) + V 2 ( ) = 14.4 e  j 22 105 Ex. 10.101 KCL at Va: Va V V + a b =1 4 j 2  j10 (4  j12) Va + (4 + j 2) Vb = 20  j 40 KCL at Vb: Vb  Va V + b + 0.5  90 = 0 (2  j 4) Va + (2  j 6) Vb = 10 + j 20  j10 2+ j 4 Cramer's rule yields: (20 j 40) (4+ j 2) (10+ j 20) (2  j 6) 200+ j100 = = 5296.5 V V = a (4  j12) (4+ j 2) 80 j 60 (2 j 4) (2 j 6) Therefore v (t ) = 5 cos (100 t + 296.5 ) = 5 cos (100 t  63.5 ) V a Ex. 10.102 The mesh equations are:
j15 I1 + 10 (I1  I 2 ) = 20 (10 + j15) I1  10 I 2 = 20  j 5 I 2 +10(I 2  I1 ) = 3090 10I1 + (10 j 5) I 2 = j 30 Cramer's rule yields: 20 10 j 30 10 j 5 200+ j 200 = = 2.263  8.1 A I1 = 10 + j15 10 75+ j100 10  j 5 10 Next VL = ( j15) I1 = (1590) (2.2638.1) = 24 282 V Therefore
vL (t ) = 24 2 cos ( t + 82) V 106 Ex. 10.103 The mesh equations are: (10+ j 50) I1 10 I 2 = j 30 10 I1 + (10 j 20) I 2 + j 20 I 3 = j 50 j 20 I 2 + (30 j10) I 3 = 0 Solving the mesh equations gives: I1 =  0.87  j 0.09 A, Then Va = 10 (I1  I 2 ) = 14.3  72 V and Vb = Va + j 50 = 36.6 83 V I 2 = 1.32+ j 1.27 A, I 3 = 0.5+ j 1.05 A Ex 10.111 V1 = j10 5 e  j 90 = 3.9 e j 51 8 + j10 j 20 5 e  j 90 = 5.68 e j 90 j 20  j 2.4 V2 = Vt = V1  V 2 = 3.9 e  j 51  5.68 e j 90 = 3.58 e j 47 107 Zt = 8 ( j10 )  j 2.4 ( j 20 ) + = 4.9 + j 1.2 8 + j10  j 2.4 + j 20 Ex 10.112 V1 ( ) = V 2 ( ) = j10 5 e  j 90 = 3.9 e j 51 8 + j10 j 20 5 e  j 90 = 5.68 e j 90 j 20  j 2.4 V ( ) = V1 ( )  V 2 ( ) = 3.9 e  j 51  5.68 e  j 90 = 3.58 e j 47
8 ( j6) 4 e j15 = 19.2 e j 68 8 + j6 j12 (  j 4 ) 4 e j15 = 24 e  j 75 j12  j 4 V1 ( ) = V 2 ( ) = V ( ) = V1 ( ) + V 2 ( ) = 14.4 e  j 22 Using superposition: v(t) = 3.58 cos ( 5t + 47 ) + 14.4 cos ( 3t  22 ) 108 Ex. 10.113 Use superposition. First, find the response to the voltage source acting alone: Z eq =  j 1010 = 5(1  j ) 10 j10 Replacing the parallel elements by the equivalent impedance. The write a mesh equation : 10 + 5 I1 + j15 I1 + 5(1  j) I1 = 0 I1 = Therefore:
i1 (t ) = 0.707 cos(10 t  45 ) A 10 = 0.707  45 A 10+ j10 Next, find the response to the dc current source acting alone:
10 3 = 2 A 15 Current division: I2 =  Using superposition: i (t ) = 0.707 cos(10 t  45)  2 A Ex. 10.121 2 = 1 1 = = 106 3 3 LC (110 )(110 ) = 1000 rad sec Ex. 10.122 Diagram drawn with relative magnitudes arbitrarily chosen: 109 Ex. 10.123 Two possible phasor diagrams for currents: In both cases: I CL = I LC =
In the first case: ( 25 )(15 )
2 2 = 20 A I LC = I L  I C I C = 6  20 = 14 A That isn't possible. Turning to the second case:
I CL = I C  I L I C = 20 + 6 = 26 A Ex. 10.141
Z1 = 1 1 R1 X 1 ( X 1  jR1 ) and R1 = 1 k , X 1 = = = 1 k 2 2 C1 (1000 )(106 ) R1 + X 1 Z1 = (1)(1)(1 j1) 1 1 =  j k and Z 2 = R 2 = 1 k 1+1 2 2
Vo 1 Z = 2 = = 1 j 1 1 Vs Z1 j 2 2 1010 Problems
Section 103: Sinusoidal Sources P10.31 (a) i (t ) = 2 cos(6t + 120 ) + 4 sin(6t  60 )
= 2 (cos 6t cos120 sin 6t sin120 ) + 4 (sin 6t cos 60  cos 6t sin 60 ) = 2.46 cos 6t + 0.27 sin 6t = 2.47 cos(6t  6.26 ) (b)
v(t ) = 5 2 cos8t + 10 sin(8t + 45 ) = 5 2 cos8t +10[sin 8t cos 45 + cos8t sin 45 ] = 10 2 cos8t + 5 2 sin 8t v(t ) = 250 cos(8t  26.56 ) = 5 10 sin(8t + 63.4 ) V
2 2 = = 6283 rad sec T 1103 v(t ) = Vm sin( t + ) = 100 sin(6283 t + ) P10.32 = 2 f = v(0) = 10 = 100 sin = sin 1 (0.1) = 6 v(t ) = 100 sin(6283 t + 6) V P10.33 1200 = = 600 Hz 2 2 i (2 103 ) = 300 cos(1200 (2 103 ) + 55) = 3cos(2.4 + 55)
f = 180 3 2.4 = 432 i (2 10 ) = 300 cos(432+55) = 300 cos(127) = 180.5 mA P10.34 1011 P10.35
A = 18 V T = 18  2 = 16 ms = 2 2 = = 393 rad/s T 0.016 16 = 18 cos ( ) = 27
v ( t ) = 18 cos ( 393 t + 27 ) V P10.36
A = 15 V T = 43  21 = 32 ms = 2 2 = = 196 rad/s T 0.032 8 = 15 cos ( ) = 58
v ( t ) = 15 cos (196 t + 58 ) V 1012 Section 104: SteadyState Response of an RL Circuit for a Sinusoidal Forcing Function P10.41
L di + R i =  vs dt di + 120 i = 400 cos 300 t dt Try i f = A cos 300 t + B sin 300 t then equating coefficients gives di f dt = 300 A sin 300 t + 300 B cos 300 t . Substituting and 300 A+120 B = 0 A =  0.46 B = 1.15 300 B +120 A =400 Then i (t ) = 0.46 cos 300 t  1.15sin 300 t = 1.24 cos (300 t  68) A P10.42
v dv dv +C =0 + 500 v = 500 cos1000 t dt dt 2 dv f Try v f = A cos1000 t + B sin1000 t then = 1000 A cos1000 t + 1000 B cos1000 t . dt Substituting and equating coefficients gives is + 1000 A+ 500 B =0 1000 B +500 A=500 Then A = 0.2 B = 0.4 v (t ) = 0.2 cos1000 t + 0.4 sin1000 t = 0.447 cos (1000t  63) V P10.43
( j 4) (.05) = j (0.2) I ( ) = 12 e j 45 ~ 12 e j 45 j 45 = (2 103 ) e i (t ) = 2 cos (4 t + 45) mA 6000 + j (0.2) 6000 1013 Section 10.5: Complex Exponential Forcing Function P10.51
(536.9 ) (1053.1 ) 5016.2 1016.2 = = = 2 510.36 (4 + j3)(6 j8) 10 j5 5 26.56 P10.52 3 2 45 3 5 + 81.87 4 j 3+ = 5 + 81.87[4  j 3 +  36.87] 5 5 28.13 = 5+81.87 (4.48 j 3.36) = 5+81.87 (5.636.87) = 28+ 45= 14 2 + j14 2 P10.53
A*C* (3 j 7) 5e  j 2.3 = = 0.65  j 6.31 B 6 e j15 P10.54
(6120 ) (4 + j 3 + 2e j15 ) = 12.1  j 21.3 a =12.1 and b =21.3 P10.55 3 b (a) j tan 1 2 2 j120 4 Ae = 4 + j (3  b) = 4 + (3b) e 3b 120 = tan 1 b = 3 + 4 + tan (120 ) = 3.93 4 A = 42 + (3b) 2 = (b) 42 + (3 (3.93)) 2 = 8.00 4 + 8 cos + j (b + 8 sin ) = 3e  j120 =  1.5  j 2.6 2.5 4+8 cos = 1.5 = cos 1 = 72 8 b + 8 sin (72 ) =  26 b = 10.2
10 + j 2a = Ae j 60 = A cos 60  j A sin 60 A= 10 20sin 60 = 20 and a = = 8.66 cos 60 2 (c) 1014 P 10.56
d 5 0.1 v + v = cos 2 t dt d v + 2 v = 2 cos 2 t dt Replace the real excitation by a complex exponential excitation to get d v + 2 v = 2 e j 2t dt Let ve = A e j 2t so d ve = j 2 A e j 2t and dt d ve + 2 ve = 2 e j 2t dt j 2 A e j 2 t + 2 A e j 2t = 2 e j 2 t A= 2 1 =  45 2 + j2 2 ( j 2 + 2 ) A e j 2t = 2 e j 2 t
so Finally v ( t ) = Re ( ve ) = 1 j ( 2t 45 ) 1  j 45 j 2t ve = e e e = 2 2 1 cos ( 2t  45 ) V 2 P 10.57
d d2 0.45 v + v + 0.15 2 v = 4 cos 5 t dt dt d2 d 20 80 v+3 v+ v= cos 5 t 2 dt dt 3 3 Replace the real excitation by a complex exponential excitation to get
d2 dt
2 v+3 d 20 80 j 5t v+ v= e dt 3 3 Let ve = A e j 5 t so d d2 ve = j 5 A e j 5 t , and 2 ve = 25 A e j 5 t dt dt 2 d d 20 80 j 5t 20 80 j 5t v+3 v+ v= e  25 A e j 5t + 3 j 5 A e j 5t + A e j 5t = e 2 dt 3 3 3 3 dt 80 20 80 j 5t 80 j 5t 3 e A= = = 1.126  141 25 + j15 + A e = 20 55 + j 45 3 3 25 + j15 + 3 ( ) ( ) so j 5t 141 ) ve = 1.126 e j141 e j 5t = 1.126 e ( ( ) Finally v ( t ) = Re ( ve ) = 1.126 cos ( 2t  141 ) V 1015 Section 106: The Phasor Concept P10.61
Apply KVL 6i+2 or 2 d i + 6 i = 15 cos 4t dt d i  15 cos 4 t = 0 dt j 4 t + ) Now use i = I m Re{e ( } and 15 cos 4 t = 15 Re{e 4 t } to write 2 d j 4 t + j 4 t + I m Re{e ( ) } + 6 I m Re{e ( ) } = 15 Re{e 4 t } dt d Re 2 ( I m e j 4 t e j ) + 6 ( I m e j 4 t e j ) = Re{15 e 4 t } dt Re 2 ( j 4 I m e j 4 t e j ) + 6 ( I m e j 4 t e j ) = Re{15 e 4 t } j8 ( I m e j ) + 6 ( I m e j ) = 15 I m e j = 15 15 = = 1.5  53 6 + j8 1053 ( ) ( ) { } i ( t ) = 1.5 cos ( 4 t  53 ) A Finally
v (t ) = 2 d d i ( t ) = 2 (1.5 cos ( 4 t  53 ) ) = 3 ( 4sin ( 4 t  53 ) ) dt dt = 12 ( cos ( 4 t  143 ) ) = 12 cos ( 4 t + 37 ) V 1016 P10.62 Apply KCL at node a: v  4 cos 2 t d + 0.25 v + i = 0 1 dt Apply KVL to the right mesh: 4i + 4 After some algebra: d2 d i + 5 i + 5 i = 4 cos 2t 2 dt dt d d i  v = 0 v = 4 i + 4 iL dt dt j 2 t + ) } and 4 cos 2 t = 4 Re{e 2 t } to write Now use i = I m Re{e ( d2 d j 2 t + j 2 t + j 2 t + I Re{e ( ) } + 5 I m Re{e ( ) } + 5 I m Re{e ( ) } = 4 Re{e 2 t } 2 m dt dt d2 d j 2 t + j 2 t + j 2 t + Re 2 I m e ( ) + 5 I m e ( ) + 5 I m e ( ) = Re{4 e 2 t } dt dt Re 4 e j I m e j 2 t + 5 ( j 2 e j I m e j 2 t ) + 5 e j I m e j 2 t = Re{4 e2t } 4 e j I m + 5 ( j 2 e j I m ) + 5 e j I m = 4 { } I m e j = 4 4 4 = = = 0.398  84 4 + 5 ( j 2 ) + 5 1 + j 10 10.0584 i ( t ) = 0.398 cos ( 2 t  85 ) A 1017 P10.63 VS = 2  90 V Z R = R; Z C =
j j = =  j 16000 C (500)(0.125106 )  j 16000 (1600090 )( 290 ) = 1.25  141 V V ( ) = ( 290 ) = 2561239 20000  j 16000 therefore v(t) = 1.25 cos (500t 141 ) V Section 107: Phasor Relationships for R, L, and C Elements P10.71 P10.72 1018 P10.7.3 P10.74 1019 P10.75 (a) v = 15cos (400 t + 30) V i = 3 sin(400 t+30) = 3 cos (400 t  60) V v leads i by 90 element is an inductor v 15 Z L = peak = = 5 = L = 400 L L = 0.0125 H = 12.5 mH 3 ipeak
i leads v by 90 the element is a capacitor 8 1 1 =4= = C = 277.77 F C 900 C ipeak 2 v = 20 cos (250 t + 60) V Zc = = vpeak (b) (c) i = 5sin (250 t +150) =5cos (250 t + 60) A Since v & i are in phase element is a resistor v 20 R = peak = =4 5 ipeak P10.76 V1 = 150 cos(30) + j150sin(30) = 130  j 75 V V2 = 200 cos 60+ j 200sin 60 = 100+ j173 V V = V1 + V2 = 230+ j 98 = 25023.1 V Thus v(t ) = v1 (t ) + v2 (t ) = 250 cos (377 t + 23.1) V 1020 Section 108: Impedance and Admittance P10.81 = 2 f = 2 (10 103 ) = 62830 rad sec
Z R = R = 36 YR = 1 1 = 0.0278 S = Z R 36 1 =  0.1 j S ZL Z L = j L = j (62830)(160106 ) = j10 YL = ZC = j j 1 = =  j 16 YC = = 0.0625 j S 6 ZC C (62830)(110 ) Yeq = YR + YL + YC = 0.0278  j0.00375 = 0.027 9 S Z eq = 1 = 36.5 9 = 36  j5.86 Yeq P10.82 Z= V 10 40 = =  5000  155 = 4532 + 2113 j = R + j L I 2103 195
2113 = 2113 = 1.06 m H 2106 so R =4532 and L = P10.83
j L R ( R + j L) j C C = Z( ) = C j 1  + ( R + j L) R + j L  C C  1 R L j R  j L  C C C = 2 1 R 2 + L  C = 1 R2 L 1 RL R  + L L  j C C C C C C 1 R 2 + L  C 2 Z( ) will be purely resistive when 1021 R2 L 1 1 R 2 + L  = 0 = CL L C C C when R =6 , C = 22 F, and L = 27 mH, then = 1278 rad/s. 2 P10.84
R Zc R R + j ( L  R 2 C + 3 R 2 L C 2 ) j C = j L + = 1 R +Z c 1+ ( R C ) 2 R+ j C Set real part equal to 100 to get C Z = ZL + R = 100 C = 0.158 F 1+ ( R C ) 2 Set imaginary part of numerator equal to 0 to get L ( = 2 f = 6283 rad sec ) L  R 2C + 2 R 2 LC 2 = 0 L = 0.1587 H P10.85 Z L = j L = j (6.28106 ) (47106 ) = j 300 1 ( 300 + j 300 ) j C Z eq = Z c (Z R +Z L ) = = 590.7 1 + 300+ j 300 j C 300+300 j 590.7 = 590.7 (590.7)(300 C ) + j (590.7)(300 C ) = 300 + j 300 1+300 j C 300 C Equating imaginary terms =2 f = 6.28106 rad sec ( ) (590.7) (300 C ) = 300 C = 0.27 nF 1022 Section 109: Kirchhoff's Laws Using Phasors P10.91 (a) (b) (c) Z1 =3+ j 4 = 553.1 and Z 2 =8 j8 = 8 2  45 Total impedance = Z1 + Z 2 = 3 + j 4 + 8  j8 = 11  j 4 = 11.7 20.0 I= 1000 100 100 = = 20.0 Z1 +Z 2 11.7  20 11.7 i (t ) = 8.55 cos (1250 t + 20.0) A P10.92 V1 ( ) = Vs ( )  V2 ( ) = 7.6847  1.59125 = ( 5.23 + j 5.62 )  ( 0.91 + 1.30 ) = ( 5.23 + 0.91) + j ( 5.62  1.30 ) = 6.14 + j 4.32 = 7.5135
v1 ( t ) = 7.51 cos ( 2 t + 35 ) V P10.93 I = I 1 + I 2 = 0.744  118 + 0.5405100 = ( 0.349  j 0.657 ) + ( 0.094 + j 0.532 )
= ( 0.349  0.094 ) + j ( 0.657 + 0.532 ) = 0.443  j 0.125 = 0.460196
i ( t ) = 460 cos (2 t + 196) mA P10.94 Vs = 2 30 V and I = 2 30 = 0.185  26.3 A 6+ j12+ 3 / j i (t ) = 0.185 cos (4 t  26.3) A 1023 P10.95 j 15 = j (2 796) (3 103 )
12 = 0.48  37 A 20 + j15 i (t ) = 0.48 cos (2 796 t  37) A I= P10.96
Z1 = R = 8 , Z 2 = j 3 L, I = B  51.87 and I s = 2  15 A 8 I B 51.87 Z1 = = = = 2 15 Is Z1 + Z 2 8+ j 3L Equate the magnitudes and the angle. 8 0 3L 82 + (3L) 2 tan 1 8 3L angles: + 36.87 = + tan 1 L = 2 H 8 8 B = B =1.6 magnitudes: 64+ 9 L2 2 P10.97 The voltage V can be calculated using Ohm's Law. V = (1.72  69) (4.2445) = 7.29  24 V
The current I can be calculated using KCL. 1024 I = (3.05  77)  (1.72  69) = 1.34  87 A
Using KVL to calculate the voltage across the inductor and then Ohm's Law gives: j 2L = P10.98 10 10 V10 = Vs = 200 10 2 45 10  j10 = 0 245
v10 (t ) = 10 2 cos (100 t + 45) V 24  4(1.3487) L=4 H 3.0577 P10.99 (a) 160 0 160 0 = (1326) (300 + j 37.7) 303 5.9  j1326 + 300 + j 37.7 = 0.53 5.9 A i(t ) = 0.53cos (120 t +5.9) A
I= (b) I= 1600 1600 = ( j199)(300 + j 251) 25659.9  j199+ 300+ j 251 = 0.62559.9 A i(t ) =0.625 cos (800 t +59.9) A 1025 Section 1010: Node Voltage and Mesh Current Analysis Using Phasors P10.101 Draw frequency domain circuit and write node equations: VA VA  VC + = 0 (2 + j )VA  2VC = j 20 10 j5 VC  VA VC KCL at C: +  (1+ j ) = 0 4VA + VC = 20 j 20 j5  j4 KCL at A  2 + Solve using Cramers rule:
(2 + j ) j 20 4 20  j 20 60  j100 116.6 59 Vc = = = = 11.6  64.7 V (2 + j ) 2 10 + j 101 5.7 4 1 P10.102 KCL: V V V (V 100) + + = 0 V = 57.6 22.9 V +  j125 j80 250 150
100 V = 0.667  0.384 22.9 = 0.347  25.5 A 150 IS = IC = V = 0.461 112.9 A 125 90 1026 IL = V = 0.720  67.1 A 8090 V = 0.23022.9 A 250 IR = P10.103
KCL at node A: Va Va  Vb + =0 200 j 100
KCL at node B: (1) Vb  Va V V 1.2 + b + b = 0 j 100  j 50 j 80 1 3 Va = Vb  4 2
Substitute Eqn (2) into Eqn (1) to get (2) Vb = 2.21  144 V
Then Eqn (2) gives Finally va (t ) = 1.97 cos (4000 t  171) V and vb (t ) = 2.21cos (4000 t  144) V Va = ( 0.55144 )  1.5 = 1.97  171 V 1027 P10.104 = 104 rad s
I s = 2053 A The node equations are: 1 1 j 1 KCL at a: + + Va +  Vb = 2053.13 20 40 60 40 1 1 j j KCL at b:  Va +  + Vb  j Vc = 0 80 40 40 40 80 j 1 j KCL at c: Vb + + Vc = 0 80 40 80 Solving thes equation yields Va = 2 24045 V P10.105 va (t ) = 339.4 cos ( t + 45) V
vs = sin (2 400 t ) V R = 100 LR = 40 mH 40 mH LS = 60 mH door opened door closed With the door open VA  VB = 0 since the bridge circuit is balanced. With the door closed Z LR = j (800 )(0.04) = j100.5 and Z LS = j (800 )(0.06) = j150.8 . The node equations are:
KCL at node B:
VB  VC VB j100.5 + = 0 VB = VC R j100.5+100 Z LR VA  VC VA + =0 Z LS R KCL at node A : 1028 Since VC = Vs =1 V
VB =0.70944.86 V and VA = 0.83333.55 V Therefore VA  VB = 0.83333.55  0.70944.86 = (0.694 + j.460)  (0.503 + j 0.500) = 0.191  j 0.040 = 0.195  11.83 V P10.106 The node equations are: V1 (1+ j ) V1 V1  V2 + + =0 j2 2 j2 V2  V1 V2 + I C = 0  j2  j2 Also, expressing the controlling signal of the dependent source in terms of the node voltages yields 1+ j 1 + j Ix = IC = 2 I x = 2 = 1  j A 2 j 2 j Solving these equations yields V2 = 3 j = 2  135 V v(t ) = v2 (t ) = 2 cos (40 t  135) V 1+ j 2 1029 P10.107 V2 = 0.757166.7 V V3 = 0.6064  69.8 V I1 = I 2 + I 3 I 3 = 0.3032 20.2 A V3  V2 I2 = yields I 2 = 0.1267184 A j 10 I =0.19536 A 1 V3 I3 = j2 therefore
i1 (t ) =0.195cos (2 t + 36) A P10.108 The mesh equations are (4 + j 6) I1  j 6 I 2 = 12 + j12 3  j 6 I1 + (8 + j 2) I 2 = 0
Using Cramer's rule yields I1 = Then I2 = and
VL = j 6(I1  I 2 ) = (690) (2.529  1.82105) = (690) (2.71  11.3) = 16.378.7 V (12+ j 12 3) (8+ j 2) = 2.529 = 2.2 + j 1.2 A (4+ j 6) (8+ j 2)  ( j 6) ( j 6) j6 690 (2.529) = (2.529) = 1.82105 A 8+ j 2 6814 Finally
V =  j 4I 2 = (4  90)(1.82105) = 7.2815 V c 1030 P10.109 The mesh equations are: (10  j ) I1 + ( j ) I 2 + 0 I 3 = 10 j I1  j I 2 + j I 3 = 0 0 I1 + j I 2 + (1 j ) I 3 = j10 Solving these mesh equations using Cramer's rule yields: (10 j ) j 0 I2 = (10 j ) j 0 10 0 j 0 j 10 (1 j ) 90  j 20 = = 8.3877.5 A i (t ) = 8.38cos (103 t + 77.5 ) A j 0 11 j j j j (1 j ) (checked using LNAPAC on 7/3/03) P10.1010 The mesh equations are:
1  j 4 I1 1030 (2 + j 4) 1 (2 +1/ j 4) 1 I 2 = 0  j4 (3+ j 4) I 3 0 1 Using Cramer's rule yields I3 = Then 2 + j8 (1030 ) = 3.22544 A 12+ j 22.5 V = 2 I 3 = 2 ( 3.22544 ) = 6.4544 V v(t ) = 6.45cos (105 t + 44 ) V 1031 P10.1011 Mesh Equations: j 75 I1  j 100 I 2 = 375  j 100 I1 + (100+ j 100) I 2 = 0 Solving for I 2 yields I 2 = 4.5 + j 1.5 A i 2 (t ) = 4.74 18.4 A 1032 Section 1011: Superposition, Thvenin and Norton Equivalents and Source Transformations P10.111 Use superposition I1 = 1245 = 3.311.3 mA 3000 + j 2000 I2 = 50 = 1.5153 mA 3000+ j1500 i (t ) = 3.3cos (4000 t + 11.3) + 1.5cos (3000 t + 153) mA P10.112 Use superposition I1 = 3 = 0.5 mA 6000 I 2 ( ) = 145 = 0.166 103 45 A 6000+ j 0.2 i (t ) = i 2 (t ) + i1 (t ) =  0.166 cos (4 t + 45) + 0.5 mA = 0.166 cos (4 t  135) + 0.5 mA P10.113 Use superposition 12 45 = 245 mA I1 ( ) = 6000 + j 0.2 590 = 0.833  90 mA I 2 ( ) = 6000 + j 0.15 i (t ) = i1 (t )  i 2 (t ) = 2 cos (4 t + 45)  0.833cos (3 t  90) mA 1033 P10.114 Find Voc : 80 + j80 Voc = ( 5 30 ) 80 + j80  j 20 80 2 21.9 = ( 5 30 ) 10036.90 = 4 2  21.9 V Find Z t :
Zt = (  j 20 )( 80 + j80 ) = 23  81.9
 j 20 + 80 + j80 The Thevenin equivalent is 1034 P10.115 First, determine Voc : The mesh equations are
600 I1  j 300 (I1  I 2 ) = 9 (600  j 300) I1 + j 300 I 2 = 90 2 V + 300 I 2  j 300 (I1  I 2 ) = 0 and V = j 300 (I1  I 2 ) j 3 I1 + (1  j 3) I 2 = 0 Using Cramer's rule: I 2 = 0.0124  16 A
Then Voc = 300 I 2 = 3.71  16 V Next, determine I sc : 2 V  V = 0 V = 0 I sc = 90 = 0.0150 A 600 The Thevenin impedance is ZT = The Thevenin equivalent is Voc 3.7116 = = 247  16 0.0150 I sc 1035 P10.116 First, determine Voc : The node equation is:
Voc Voc  (6 + j8) 3 Voc  (6+ j8) +  =0  j4 j2 j2 2 Voc =3+ j 4=553.1 V Vs = 1053 = 6 + j 8 V Next, determine I sc : The node equation is: V V V  (6 + j8) 3 V  (6 + j8) + +  =0 2  j4 j2 2 j2 V=
3 + j4 1 j I sc = V 3+ j 4 = 2 2 j 2 Vs = 1053 = 6 + j 8 V The Thevenin impedance is ZT =
The Thevenin equivalent is 2 j 2 Voc = 3 + j4 = 2  j2 I sc 3+ j 4 1036 P10.117 Y = G + YL + YC 1 Y = G when YL + YC = 0 or + j C = 0 j L 1 1 1 , fO = O = = 2 LC 2 39.61015 LC
= 0.07998107 Hz =800 KHz (80 on the dial of the radio) P10.118 In general: I= Voc ZL and V = Voc Z t +Z L Z t +Z L
V1 25 = = 0.5 A Z1 50 I2 = V2 100 = = 0.5 A Z 2 200 In the three given cases, we have
Z1 = 50 I1 = Z2 = 1 1 = =  j 200 j C j (2000)(2.510 6 ) Z 3 = j L = j (2000)(50 103 ) = j100 I3 = V3 50 = = 0.5 A Z 3 100 Since I is the same in all three cases, Z t +Z1 = Z t +Z 2 = Z t +Z3 . Let Z t = R + j X . Then ( R + 50) 2 + X 2 = R 2 + ( X  200) 2 = R 2 + ( X + 100) 2 This requires ( X  200) 2 = ( X + 100) 2 X = 50 Then ( R + 50) 2 + (50) 2 = R 2 + (150) 2 R = 175 so Z t =175+ j 50 and
Voc = I1 Z t + R1 =(0.5) (175+ 50) 2 + (50) 2 =115.25 V 1037 P10.119 Z1 = ( j 3)(4) = 2.4  53.1  j 3+ 4 =1.44  j1.92 Z 2 = Z1 + j 4 = 1.44 + j 2.08 = 2.5355.3 Z3 = 3.51  37.9 = 2.77  j 2.16 3.5137.9 ( 3.5137.9 ) = 1.9  92 A I = ( 2.85 78.4 ) = ( 2.85 78.4 ) ( 5.24 24.4 ) 2.77  j 2.16 + 2 1038 P10.1110 Z2 = (200)( j 4) = 4  88.8 200 j 4 I= 0.4 44 = 4  44 mA 4 j +100+ j 4 i (t ) = 4 cos (25000 t  44) mA 1039 Section 1012: Phasor Diagrams P10121 V = V1  V2 + V3 = ( 3+ j 3)  ( 4 + j 2 ) + ( 3+ j 2 ) = 4 + j 3
* * P10.122 100 = 0.7442 A 10+ j1 j10 I= VR = R I = 7.442 V VL = Z L I = (190)(0.7442) = 0.74132 V VC = Z C I = (1090)(0.7442) = 7.4 48 V VS = 100 V P10.123
I = 72 3 + 36 3(140  90) + 144210 + 25 = 40.08  j 24.23 + 25 = 46.83  31.15 + 25 To maximize I , require that the 2 terms on the right side have the same angle = 31.15. 1040 Section 1014: Phasor Circuits and the Operational Amplifier P10.141 Vo ( ) 104   j104 10  j 225 j e =  = = 10 Vs ( ) 1 j 2 1000 10  j 225  j 225 Vs ( ) = 2 Vo ( ) = e 2 = 10e 2 vo ( t ) = 10 cos (1000t  225) V H ( ) = P10.142 Node equations: V1  VS VS + j C 1 V1 = 0 V1 = 1 + j C1 R1 R1 R3 V1 V1  V0 V + = 0 V0 = 1 + R2 1 R2 R3 Solving:
R2 V0 = VS 1 + j C 1 R1 1+ R3 P10.143 Node equations:
j C 1 VS V1 + j C 1 ( V1  VS ) = 0 V1 = R1 1 + j C 1 R1 R3 V1 V1  V0 + = 0 V0 = 1 + V R2 1 R2 R3 Solving: R j C 1 1 + 3 R2 V0 = 1 + j C 1 R1 VS 1041 P10.144 Node equations: V1  VS V VS + 1 = 0 V1 = 175  j1.6 1 + j 109
V  V0 V1 + 1 = 0 V0 = 11 V1 1000 10000 Solving:
V0 = 11 11 VS = ( 0.0050 ) 1 + j 109 11089.5 = 0.589.5 mV Therefore v0 (t ) = 0.5cos ( t  89.5) mV 1042 PSpice Problems
SP101 1043 SP102 1044 SP 103 1045 SP 104 The following simulation shows that k1 = 0.4and k2 = 3 V/A. The required values of Vm and Im are Vm = 12.5 V and Im = 1.667 A. 1046 Verification Problems
VP 101 Generally, it is more convenient to divide complex numbers in polar form. Sometimes, as in this case, it is more convenient to do the division in rectangular form. Express V1 and V2 as: V1 =  j 20 and V 2 = 20  j 40 KCL at node 1: 2 KCL at node 2:
V1  V 2 j 10  V2 V1  j 20  ( 20  j 40 ) 20  j 40  j 20 + 3 =  + 3 = ( 2 + j 2)  ( 2  j4)  j 6 = 0 10 j 10 10 10 10 V1 10  V1  V 2 j 10 = 2  j 20  j 20  ( 20  j 40 )  = 2+ j22 j2 = 0 10 j 10 The currents calculated from V1 and V2 satisfy KCL at both nodes, so it is very likely that the V1 and V2 are correct. VP 102 I 1 = 0.390 39 and I 2 = 0.284 180 Generally, it is more convenient to multiply complex numbers in polar form. Sometimes, as in this case, it is more convenient to do the multiplication in rectangular form. Express I1 and I2 as: I 1 = 0.305 + j 0.244 and I 2 = 0.284 KVL for mesh 1:
8 ( 0.305 + j 0.244 ) + j 10 ( 0.305 + j 0.244 )  ( j 5) = j 10 Since KVL is not satisfied for mesh 1, the mesh currents are not correct. Here is a MATLAB file for this problem: 1047 % Impedance and phasors for Figure VP 102 Vs = j*5; Z1 = 8; Z2 = j*10; Z3 = j*2.4; Z4 = j*20; % Mesh equations in matrix form Z = [ Z1+Z2 0; 0 Z3+Z4 ]; V = [ Vs; Vs ]; I = Z\V abs(I) angle(I)*180/3.14159 % Verify solution by obtaining the algebraic sum of voltages for % each mesh. KVL requires that both M1 and M2 be zero. M1 = Vs + Z1*I(1) +Z2*I(1) M2 = Vs + Z3*I(2) + Z4*I(2) VP 103 V1 = 19.2 68 and V 2 = 24 105 V KCL at node 1 : 19.2 68 19.2 68 +  415 = 0 2 j6 KCL at node 2: 24 105 24 105 + + 415 = 0  j4 j12 The currents calculated from V1 and V2 satisfy KCL at both nodes, so it is very likely that the V1 and V2 are correct. Here is a MATLAB file for this problem:
% Impedance and phasors for Figure VP 103 Is = 4*exp(j*15*3.14159/180); Z1 = 8; Z2 = j*6; Z3 = j*4; 1048 Z4 = j*12; % Mesh equations in matrix form Y = [ 1/Z1 + 1/Z2 0; 0 1/Z3 + 1/Z4 ]; I = [ Is; Is ]; V = Y\I abs(V) angle(V)*180/3.14159 % Verify solution by obtaining the algebraic sum of currents for % each node. KCL requires that both M1 and M2 be zero. M1 = Is + V(1)/Z1 + V(1)/Z2 M2 = Is + V(2)/Z3 + V(2)/Z4 VP 104 First, replace the parallel resistor and capacitor by an equivalent impedance ZP = (3000)( j 1000) = 949  72 = 300  j 900 3000 j 1000 The current is given by I= Current division yields  j 1000 I1 = ( 0.2 53 ) = 63.3  18.5 mA 3000  j 1000 3000 I2 = ( 0.2 53 ) = 19071.4 mA 3000  j 1000 VS 100 0 = = 0.253 A j 500+ Z P j 500+ 300 j 900 The reported value of I1 is off by an order of magnitude. 1049 Design Problems
DP 101 R2 1 j C = R2 1 + j CR 2
R2 1 + j CR 2 R1 Vo ( ) = = Vi ( ) R1 1 + j CR 2 R1 Vo ( ) j (180  tan 1 CR 2 ) = e 2 Vi ( ) 1 + ( CR 2 ) R2 R2 In this case the angle of Vo ( ) tan (180  76 ) is specified to be 104 so CR 2 = = 0.004 and the 1000 Vi ( ) R2 R1 = 8 2.5 R2 = 132 . One set of values R1 1 + 16 that satisfies these two equations is C = 0.2 F, R1 = 1515 , R 2 = 20 k . magnitude of Vo ( ) 8 so is specified to be 2.5 Vi ( ) DP 102 R2 Vo ( ) = Vi ( ) where K = 1 j C = R2 1 + j CR 2 R2 1 + j CR 2 K = R2 1 + j CR p R1 + 1 + j CR 2 and R p = R1 R 2 R1 + R 2 R1 R1 + R 2 Vo ( ) K  j tan 1 CR p = e 2 Vi ( ) 1 + ( CR p ) 1050 In this case the angle of C Rp = C R1 R 2 R1 + R 2 = tan ( 76 ) V ( ) 2.5 = 0.004 and the magnitude of o so is specified to be 12 1000 Vi ( ) Vo ( ) is specified to be 76 so Vi ( ) R2 2.5 K = 0.859 = K = . One set of values that satisfies these two equations is R1 + R 2 1 + 16 12 C = 0.2 F, R1 = 23.3 k, R 2 = 142 k . DP 103 L R 2 + j L R1 Vo ( ) = = j L R 2 L Vi ( ) 1 + j R1 + Rp R 2 + j L j where R p = R1 R 2 R1 + R 2 j L R 2 Vo ( ) Vi ( ) = L R1
2 L 1+ Rp e L j 90  tan 1 Rp In this case the angle of Vo ( ) L L ( R1 + R 2 ) tan ( 90  14 ) is specified to be 14 so = = = 0.1 Rp R1 R 2 Vi ( ) 40 L 40 R1 V ( ) 2.5 L 2.5 = = 0.0322 . One so is specified to be and the magnitude of o 8 R1 Vi ( ) 8 1 + 16 set of values that satisfies these two equations is L = 1 H, R1 = 31 , R 2 = 14.76 . 1051 DP 104 L R 2 + j L R1 Vo ( ) = = j L R 2 L Vi ( ) 1 + j R1 + Rp R 2 + j L j where R p = R1 R 2 R1 + R 2 j L R 2 Vo ( ) Vi ( ) = L R1
2 In this case the angle of L L ( R1 + R 2 ) tan ( 90 + 14 ) = = = 0.1 Rp R1 R 2 40 This condition cannot be satisfied with positive DP 105 Vo ( ) is specified to be 14. This requires Vi ( ) L 1+ Rp e L j 90  tan 1 Rp Z1 =10 1 Z2 = j C Z3 = R + j L 1 S 10 Y2 = j C 1 Y3 = R + j L Y1 = v(t ) = 80 cos (1000 t  ) V V = 8  V iS (t ) = 10 cos 100 t A I s =100 A so (80 ) 1 1 + + j C = 100 R + 10  10 2 LC + j ( L + 10 RC ) = 1.25 R + j1.25 L 10 R + j L Equate real part: 40  40 2 LC = R where = 1000 rad sec Equate imaginary part: 40 RC = L Solving yields R = 40(1 4107 RC 2 ) 1052 Now try R = 20 1  2(1  4 107 (20)C 2 ) which yields C = 2.5105 F= 25 F so L = 40 RC = 0.02 H=20 mH Now check the angle of the voltage. First Y1 = 1/10 = 0.1 S Y2 = j 0.25 S Y3 = 1/(20+ j 20) = .025 j.025 S then Y = Y1 + Y2 + Y3 = 0.125 , so V =YI s = (0.1250)(100) = 1.250 V So the angle of the voltage is =0 , which satisfies the specifications. 1053 Chapter 11: AC Steady State Power
Exercises:
Ex. 11.31 Z = j3 + 4( j 2) = 0.8 + j1.4 4 j 2 = 1.6 60.3 I = V 70 = = 4.38  60.3 A Z 1.660.3 i (t ) = 4.38cos (10 t  60.3 ) A The instantaneous power delivered by the source is given by p(t ) = v(t ) i (t ) = (7 cos 10 t )(4.38cos (10 t  60.3)) = The inductor voltage is calculated as (7)(4.38) [cos (60.3) + cos (20 t 60.3)] 2 = 7.6 + 15.3cos (20 t  60.3) W VL = I Z L = (4.38  60.3)(j3) = 13.12 29.69 V vL (t ) = 13.12 cos (10 t + 29.69) V
The instantaneous power delivered to the inductor is given by pL (t ) = vL (t ) i (t ) = (13.12 cos (10t + 29.69)(4.38cos (l0t  60.3 ) 57.47 [ cos (29.69+ 60.3)+ cos (20 t + 29.6960.3)] 2 = 28.7 cos (20t  30.6) W = 111 Ex. 11.32 (a) When the element is a resistor, the current has the same phase angle as the voltage: i (t ) = v(t ) Vm cos ( t + ) A = R R The instantaneous power delivered to the resistor is given by 2 2 2 V V Vm V pR (t ) = v(t ) i (t ) = Vm cos ( t + ) cos ( t + ) = m cos 2 ( t + ) = m + m cos (2 t + ) R R 2R 2R (b) When the element is an inductor, the current will lag the voltage by 90. Z L = j L = L90 I= V V V = m = m ( 90 ) Z L90 L The instantaneous power delivered to the inductor is given by
V V pL (t ) = i (t ) v(t ) = m cos ( t +  90 ) Vm cos ( t + ) = m cos ( 2 t + 2 90 ) W L 2 L
2 112 Ex. 11.33
The equivalent impedance of the parallel resistor (1)( j ) = 1 1+ j . Then and inductor is Z = ( ) 1+ j 2 100 20 I= =  18.4 A 1 10 1+ (1+ j ) 2 (a) Psource
I V = cos = 2 (10 ) 2 20 10 cos 18.4 = 30.0 W ( ) 2 20 (1) 2 I max R1 10 (b) PR 1 = = = 20 W 2 2 Ex. 11.41
I eff =
3 1 t 2 1 2 i (t ) dt = 0 (10)2 dt + 2 (5)2 dt = 8.66 T 0 3 Ex. 11.42 (a) I 2 i (t ) = 2 cos 3 t A I eff max = = 2A 2 2
(b) i (t ) = cos (3 t  90 ) + cos (3 t + 60 ) A 1 3 +j = 0.518  15 A 2 2 0.518 i (t ) = 0.518 cos (3t  15) A I eff = = 0.366 A 2 I = (190 ) + (160 ) =  j + (c) 2 3 2 I eff = + 2 2 2 2 I eff = 2.55 A 113 Ex. 11.43 Use superposition: V1 = 50 V V2 = 2.5 V (dc) V3 = 390 V V1 and V2 are phasors having the same frequency, so we can add them: V1 + V3 = ( 50 ) + ( 3  90 ) = 5  j3 = 5.83  31.0 V
Then Finally
V
2 R eff vR (t ) = v1 (t ) + ( v2 (t ) + v3 (t ) ) = 2.5 + 5.83cos (100 t  31.0) V 5.83 = (2.5) + = 23.24 V VR eff = 4.82 V 2 2 2 Ex. 11.51 Analysis using Mathcad (ex11_5_1.mcd):
Enter the parameters of the voltage source: Enter the values of R and L R := 10 A := 12 L := 4 Z := R + j L := 2 The impedance seen by the voltage source is: The mesh current is: I := A Z 114 I ( I Z) The complex power delivered by the source is: Sv := Sv = 4.39 + 3.512i 2 I ( I R) The complex power delivered to the resistor is: Sr := Sr = 4.39 2 I ( I j L) The complex power delivered to the inductor is: Sl := Sl = 3.512i 2 Verify Sv = Sr + Sl : Sr + Sl = 4.39 + 3.512i Sv = 4.39 + 3.512i Ex. 11.52 Analysis using Mathcad (ex11_5_2.mcd):
Enter the parameters of the voltage source: A := 12 Enter the values of R, L an C d R := 10 L := 4 := 2 C := 0.1 1 j C The impedance seen by the voltage source is: Z := R + j L + The mesh current is: I := A Z Sv := Sr := Sl := I ( I Z) I ( I R) 2 is: The complex power delivered by the source Sv = 6.606 + 1.982i Sr = 6.606 Sl = 5.284i The complex power delivered to the resistor is: The complex power delivered to the inductor is: I ( I j L) 2 I I 1 2 j C The complex power delivered to the capacitor is: Sc := 2 Verify Sv = Sr + Sl + Sc : Sr + Sl + Sc = 6.606 + 1.982i Sc = 3.303i Sv = 6.606 + 1.982i 115 Ex. 11.53 Analysis using Mathcad (ex11_5_3.mcd):
Enter the parameters of the voltage source: A := 12 := 2 Q := 6 Enter the Average and Reactive Power delivered to the RL circuit: P := 8 The complex power delivered to the RL circuit is: The impedance seen by the voltage source is: S := P + j Q Z := 2 S L := Im( Z) A
2 Calculate the required values of R and L R := Re( Z) The mesh current is: I := A Z R = 5.76 L = 2.16 I ( I Z) The complex power delivered by the source is: Sv := 2 I ( I R) The complex power delivered to the resistor is: Sr := 2 I ( I j L) The complex power delivered to the inductor is: Sl := 2 Verify Sv = Sr + Sl : Sr + Sl = 8 + 6i Sv = 8 + 6i Sv = 8 + 6i Sr = 8 Sl = 6i Ex. 11.61
(377) (5) pf = cos ( Z ) = cos tan 1 L = cos tan 1 = 0.053 R 100 ( ) Ex. 11.62 pf = cos ( Z) = cos tan 1 X = cos tan 1 80 = 0.53 lagging 50 R ( ) ( ) XC = (50)2 + (80)2 = 111.25 ZC =  j 111.25 50 tan (cos 1 1) 80
116 Ex. 11.63
PT = 30 + 86 = 116 W and QT = 51 VAR S T = PT + j QT = 116+ j 51 = 126.7 23.7 VA pf plant = cos 23.7 = 0.915 Ex. 11.64
P = V I cos Z= I = P 4000 = = 44.3 A V cos (110)(.82) V cos 1 (0.82) = 2.48 34.9 = 2.03+ j 1.42 = R + j X I To correct power factor to 0.95 requires R2 + X 2 (2.03) 2 + (1.42) 2 = =  8.16 R tan (cos 1 pfc )  X (2.03) tan (18.19 ) 1.42 1 C= =325 F X1 X1 = Ex. 11.71 (a) I = I1 + I 2 = ( 0.4714135 ) + (1.414  45 ) = 0.9428  45 A 0.94282 ( 6 ) = 2.66 W 2 (b) 1.22 I1 = 1.253 A p1 = ( 6 ) = 4.32 W 2 0.47142 I 2 = 0.4714135 A p1 = ( 6 ) = 0.666 W 2 p = p1 + p2 = 4.99 W p= Ex. 11.81
For maximum power, transfer
Z L = Z* = 10  j14 t 100 I= =5 A (10+ j14) (10 j14) 5 PL = Re(10  j14) = 125 W 2 2 117 Ex. 11.82
If the station transmits a signal at 52 MHz then = 2 f = 104 106 rad/sec so the received signal is vs (t ) = 4 cos (104 106 t ) mV (a) If the receiver has an input impedance of Zin =300 then
300 1 2 1 2.4103 Zin Vin = Vs = 4 103 = 2.4 mV P = Vin = = 9.6 nW R + Zin 200+300 2 R L 2(300) 2 (b) If two receivers are connected in parallel then Zin = 300300 = 150 and Vin =
Zin 150 VS = (4 103 ) =1.71 103 V R + Zin 200+150 total P = 2 Vin 1 (1.71103 ) 2 = 9.7 nW or 4.85 nW to each set = 2 Zin 2(150) (c) In this case, we need Zin = R  R = 200 R = 400 , where R is the input impedance of each television receiver. Then Ptotal = Vm 2 (2103 ) 2 = = 10 nW 5 nW to each set 2 Zin 2(200) 118 Ex 11.91 Coil voltages: V1 = j 24 I 1 + j 16 I 2 = j 40 I V 2 = j 16 I 1 + j 40 I 2 = j 56 I Mesh equation: 24 = V1 + V 2 = j 40 I + j 56 I = j 96 I 24 1 =j 4 j 96 1 Vo = V 2 = ( j 56 )  j = 14 4 vo = 14 cos 4t V I= Ex 11.92 Coil voltages: V1 = j 24 I 1  j 16 I 2 = j 8 I V 2 =  j 16 I 1 + j 40 I 2 = j 24 I Mesh equation: 24 = V1 + V 2 = j 8 I + j 24 I = j 32 I 24 3 =j 4 j 32 3 Vo = V 2 = ( j 24 )  j = 18 4 vo = 18 cos 4t V I= Ex 11.93 0 = V 2 = j 16 I 1 + j 40 I 2 40 I 2 = 2.5 I 2 16 V s = V1 = j 24 I 1 + j 16 I 2 I1 = 
= j (24(2.5) + 16) I 2 =  j 44 I 2 24 6 = j  j 44 11 I o = I 1  I 2 = (2.5  1) I 2 I2 = = 3.5 I 2 6 = 3.5 j =  j 1.909 11 io = 1.909 cos ( 4t  90 ) A 119 Ex 11.94 0 = V 2 =  j 16 I 1 + j 40 I 2 40 I 2 = 2.5 I 2 16 V s = V1 = j 24 I 1  j 16 I 2 I1 = = j (24(2.5)  16) I 2 = j 44 I 2 24 6 =j 11 j 44 I o = I 1  I 2 = (2.5  1) I 2
I2 = = 1.5 I 2 6 = 1.5  j =  j 0.818 11 io = 0.818 cos ( 4t  90 ) A Ex. 11.101 I1 = 50 50 = = 20 A 100  j 75 (1 + j 3) + ( 4  j 3) (1 + j 3) + 52
V1 = ( 4  j 3) 20 = 10  36.9 V 1110 Ex. 11.102 I1 = 50 50 50 = = = 0.6842 A 2+ j 0.2 5.5 + j 4.95 7.4 42 5 j 5 ) + ( 22 1 I 2 = I1 = 0.3442 A 2 V2 = ( 2 + j 0.2 ) I 2 = ( 2.015.7 )( 0.3442 ) = 0.6847.7 V so v2 (t ) = 0.68cos (10 t + 47.7) V and i 2 (t ) = 0.34 cos (10 t + 42) A Ex. 11.103 Z1 = then 1 Z Z 1 Z Z = , Z 2 = 2 Z + 2 = 9 Z + and Z 3 = 2 (Z + Z 2 ) 2 n3 4 n1 n2 n3 4 1 Z Z ab = Zin = Z + Z3 = Z + Z +9 Z+ = 4.0625 Z 4 4 1111 Problems
Section 113: Instantaneous Power and Average Power P11.31 10 = V V V + + V = 14.6  43 V 20 j 63  j16 I= V = 0.23  133 A j 63 p(t ) = i (t )v(t ) = 0.23(cos (2 103 t  133 )) 14.6 cos (2 103 t  43 ) = 3.36 cos (2 103 t 133 ) cos (2 103 t  43 ) =1.68 (cos (90 ) + cos (4 103 t 176 )) =1.68 cos (4 103 t 176 ) P11.32
Current division: 1800  j 2400 I=4 5 1800 j 2400+ 600 =5
2 5  8.1 mA 2 P600 I 600 5 = = 300(25) = 1.875 104 W = 18.75 mW 2 2 5 V I cos 1 = (600) 5 4 5 cos(8.1 ) = 2.1 104 W = 21 mW 2 2 2 Psource = ( ) P11.33 1112 Node equations: 20I X 100 20I X  V + IX + = 0 I X (20  j15)  V =  j 50  j5 10 V  20I X V  3I X + = 0 I X (40 + j 30) + V (2  j ) = 0  j5 10 Solving the node equations using Cramer's rule yields IX =
Then j 50(2  j ) 50 563.4 = = 2 510.3 A (40  j 30)  (20  j15)(2  j ) 2553.1 PAVE I = X (20) = 10 2 5 2 2 ( ) 2 = 200 W P11.34
A node equation:
(V  16) V +  (2 245) = 0 j4 8 2 V = 16 18.4 V 3 Then I=
2 16  V = 3.2  116.6 A j4 PAVE 8 1 V = 2 8 2 2 16 5 1 = = 6.4 W absorbed 2 8 PAVE current source =  1 1 2 V 2 2 cos =  16 2 2 cos ( 26.6 ) = 12.8 W absorbed 2 2 5 ( ) ( ) PAVE inductor = 0 1 1 PAVE voltage source =  (16) I cos =  (16)( 3.2)cos(  116.6) = 6.4 W absorbed 2 2 1113 P11.36 A node equation: 20 + Then V1 V1 + (3 / 2)V1 + = 0 V1 = 50 5  26.6 V 10 15  j 20
V1 + ( 3/2 ) V1 ( 5 / 2 ) V1 = 5 5 26.6 A = 15  j 20 25  53.1 I= Now the various powers can be calculated: PAVE 10 PAVE current source =  1 V1 1 (50 5) = = = 625 W absorbed 2 10 2 10
2 2 1 1 V (20) cos =  (50 5)(20) cos (26.6) = 1000 W absorbed 2 2
I
2 PAVE 15 = 2 (5 5 ) (15 ) = 
2 2 (15 ) = 937.5 W absorbed PAVE voltage source =  1 3 1 I V1 cos =  5 5 75 5 cos ( 53.1 ) = 562.5 W absorbed 2 2 2 PAVE capacitor = 0 W ( )( ) P11.37
Z= 200 ( j 200 ) 200 90 200 = = 45 200 (1 + j ) 2 45 2 I = 1200 200 = 0.85  45 A, I R = I = 0.60 A 200 200 + j 200 45 2 P = I R = ( 0.6 ) ( 200 ) = 72 W and w = ( 72 )(1) = 72 J
2 2 1114 Section 114: Effective Value of a Periodic Waveform P11.41 (a) i = 2  4 cos 2t = i1 + i 2 ( Treat i as two sources of different frequencies.)
T 2A source: I eff = lim 1 T T o (2) dt = 2 A 2 and 4 cos 2t source: The total is calculated as
I eff
2 2 Ieff = 4 A 2 4 = ( 2) + = 12 A I rms = I eff = 12 = 2 3 A 2
2 (b) i ( t ) = 3cos ( t  90 ) + 2 cos t I = ( 3  90 ) + ( 2 0 ) = 2  j 3 = 3.32  64.8 A I rms = (c) 3.32 = 2.35 A 2 i ( t ) = 2 cos 2t + 4 2 cos ( 2t + 45 ) + 12 cos ( 2 t  90 ) I = ( 20 ) + 4 2 45 + (12  90 ) = ( 2 + 4 ) + ( j 4  j12 ) =10  53.1 A I rms = 10 =5 2 A 2 ( ) P11.42 (a) 1 Vrms = 5 (b)
Vrms = 1 5 1 5 ( 6 dt + 2 dt ) = 1 ( 36 dt + 4 dt ) = 5
2 2 5 2 2 5 0 2 0 2 1 84 = 4.10 V ( 72 + 12 ) = 5 5 1 116 = 4.81 V (8 + 108) = 5 5 1 84 = 4.10 V (12 + 72 ) = 5 5 ( 2 dt + 6 dt ) = 1 ( 4 dt + 36 dt ) = 5
2 2 5 2 2 5 0 2 0 2 (c) Vrms = ( 2 dt + 6 dt ) = 1 ( 4 dt + 36 dt ) = 5
3 2 5 2 3 5 0 3 0 3 1115 P11.43 2 (a) 1 4 4 2 4 4 4 4 2 2 Vrms = 1 3 t + 3 dt = 27 1 ( 2 t + 1) dt = 27 1 ( 4 t + 4 t + 1) dt 3 4 4 t3 = 27 3 = = (b) Vrms
2 4 1 4t 2 + 2 4 1 4 +t 1 4 ( (85.33  1.33) + ( 2 )(16  1) + 3) 27 4 (117 ) = 4.16 V 27 1 4 4 22 4 4 4 4 2 2 = ( 2 t + 11) dt = ( 4 t  44 t + 121) dt  t + dt = 3 1 3 3 27 1 27 1 4 4 t3 = 27 3 = =
4 1 44t 2  2 4 1 4 + 121 t 1 4 (84 + ( 22 )15 + (121) 3) 27 4 (117 ) = 4.16 V 27 (c) Vrms 1 3 4 4 3 4 3 2 2 = 0 3 t + 2 dt = 27 0 ( 2 t + 3) dt = 27 0 ( 4 t + 12 t + 9 ) dt 3 4 4 t3 = 27 3 = =
3 2 12t 2 + 2 0 3 3 + 9t 0 0 4 ( 36 + 54 + 27 ) 27 4 (117 ) = 4.16 V 27 1116 P11.44 (a) 2 v ( t ) = 1 + cos T t = vdc + vac vdc eff 2 t 1 T = 0 1dt = T T
2 2 T 0 T 2 =  0 = 1 V and vac eff = T 2 1 V 2 veff = vdc eff + vac eff (b) = 1 1 + = 1.225 V 2
2 2 =
1 T /2 A2 2 = 0 ( A sin t ) dt = T T I rms = 2 , I rms = T 1 T 2 i ( t ) dt T 0 I rms 2 T /2 0 2 T /2 1 A2 T / 2 = A A (1cos 2 t ) dt = 0 dt  0 cos 2 t dt 4 2 2T A2 A = , where A = 10 mA 4 2 I rms = 5 mA P11.45
90 t v ( t ) = 90 ( 0.2t ) 0 2 Vrms = 0 t 0.1 0.1 t 0.2 0.2 t 0.3 0.1 t 2 dt + 0.2 0.2t 2 dt ) 0.1 ( 0 .001 .001 3 + 3 = 18 V 0.2 2 1 0.1 902 2 ( 90t ) dt + 0.1 90 ( 0.2t ) dt = .3 .3 0 902 = .3 V rms = 18 = 4.24 V 1117 Section 115: Complex Power P11.51 I* =
2 ( 3.6 + j 7.2 ) 2S = = 0.6 + j 1.2 = 1.34263.43 A 120 120 R+ j4 L = 120 = 8.9463.43 = 4 + j 8 R = 4 and L = 2 H 1.342  63.43 2 (18 + j 9 ) 2S = = 3 + j 1.5 = 3.3526.56 A 120 120 P 11.52 I* = 1 1 1 1 3.35  26.56 + = j = = 0.2791  26.56 = 0.250 + j 0.125 R j4 L R 4L 120 R = 4 and L = 2 H
P11.53 Let
Zp = 8 ( j 8) j 8 1 j 8 + j 8 = = = 4+ j4 V 8 + j 8 1+ j 1 j 2 Next 120 120 I= = = 1.342  26.6 A 4 + Z p 4 + (8 + j 8) Finally (120 )(1.342  26.6 ) S=
2 * = 7.2 + j 3.6 VA 1118 P11.54 Before writing node equations, we can simplify the circuit using a source transformation: The node equations are:
V1 V1  V2 + = 0 V1 (1 + j )  V2 = 10 2 j2 V2  V1 1 V2 + V1 + = 0 V1 ( 4 + j ) + V2 ( j 8 ) = 0 j2 8 0.8 + j 0.4 5 + Using Cramers's rule
V1 = 80 = (16 / 3) 126.9 V (4  j )  j8(1+ j ) then 1 1 I =  V1  V2 =  V1  V1 (1+ j )+ j 10= 2.66126.9 A 8 8 Now the complex power can be calculated as
2.66126.9 (2 / 3)36.9 I* ( (1/ 8)V1 ) S= = 2 2 ( )( ) =j 8 VA 9 Finally
S = P + jQ = j 8 8 P = 0, Q = VAR 9 9 1119 P11.55 I=
S = VI* = 50120 50120 = = 2.583.13 A 16+ j12 2036.87
125 36.87 = 100 + j 75 VA ( 50120 )( 2.583.13 ) = P11.56 KVL: (10+ j 20 ) I1 = 50  j 2 I 2 (10 + j 20 ) I1 + j 2 I 2 = 50
KCL: I1 + I 2 = 60
Solving these equations using Cramer's rule: = 10 + j 20 1 j2 = 10 + j18 1 I1 = 1 5 j2 5  j12 = = 0.63232 A = 0.39  j 0.5 A 6 1 10 + j18
I 2 = 6  I1 = 6 + 3.9 + j.5 = 6.39 + j.5 = 6.414.47 A Now we are ready to calculate the powers. First, the powers delivered:
1 ( 50 ) I 2* = 2.5 ( 6.41(180 4.47) ) = 16.0 + j1.1 VA 2 1 S 6 0 = [5 j 2 I 2 ]( 60 ) = 5 j 2( 6.39+ j.5 ) 3 = 18.0 j 38.3 VA 2 S Total = S5 0 + S 6 0 = 2.0 j 37.2 VA S5 0 =
delivered ( ) 1120 Next, the powers absorbed:
1 10 2 2 10 I1 = (.63) = 2.0 VA 2 2 j 20 2 S j20 = I1 = j 4.0 VA 2 1 2 2 S  j2 = (  j 2 ) I 2 =  j ( 6.41) =  j 41.1 VA 2 S Total = 2.0  j 37.1 VA S10 =
absorbed To our numerical accuracy, the total complex power delivered is equal to the total complex power absorbed.
P11.57 (a) (b) Z= V 10020 = = 430 I 25  10 I V cos (100 )( 25 ) cos 30 = = 1082.5 W 2 2 P= (c) Y = 1 = 0.25  30 = 0.2165  j 0.125 S . To cancel the phase angle we add a capacitor Z having an admittance of YC = j 0.125 S . That requires C =0.125 C = 1.25 mF . P11.58 Apply KCL at the top node to get
10  V1 V1 3  V1 + = 0 V1 = 436.9 V 3 3 4 1 j 2 Then V I1 = 1 = 136.9 A 4 The complex power delivered by the source is calculated as  S= (136.9 )* (100 ) =
2 5  36.9 VA Finally pf = cos ( 36.9 ) = .8 leading 1121 Section 11.6: Power Factor P11.61 Heating: P = 30 kW Motor: = cos 1 ( 0.6 ) = 53.1 S = 150 kVA P = 150 cos 53.1 = 90 kW Q = 150sin 53.1 = 120 kVAR Total (plant): P = 30 + 90 = 120 kW S = 120 + j120 = 17045 VA Q = 0 + 120 = 120 kVAR The power factor is pf = cos 45 = 0.707 lagging. The current required by the plant is I =
S 170 kVA = = 42.5 A . V 4 kV P11.62 Load 1: Q1 = S sin ( cos 1 (.7 ) ) = (12 kVA ) sin ( 45.6 ) = 8.57 kVAR Load 2: P2 = (10 kVA )( 0.8 ) = 8 kW P = S cos = (12 kVA )( 0.7 ) = 8.4 kW 1 Q2 = 10sin ( cos 1 ( 0.8 ) ) = 10sin ( 36.9 ) = 6.0 kVAR Total:
S = P + jQ = 8.4 + 8 + j ( 8.57 + 6.0 ) = 16.4 + j14.57 = 21.941.6 kVA The power factor is pf = cos ( 41.6 ) = 0.75 . The average power is P = 16.4 kW. The apparent power is S = 21.9 kVA. 1122 P11.63 The source current can be calculated from the apparent power: 1 Vs I s = 2 S = 2( 50 cos 0.8 ) = 536.9 A S= I s Vs 200 2
I s = 5  36.9 = 4  j3 A Next
I1 = Vs 200 = = 2  53.1 = 1.2  j1.6 A 6 + j8 1053.1 I 2 = I s  I1 = 4  j 3  1.2 + j1.6 = 2.8  j1.4 = 3.13  26.6 A Finally,
Z= Vs 200 = = 6.3926.6 I z 3.13  26.6 P11.64 (Using all rms values.) 2 (a) V 2 2 P = I R= V = P R = ( 500 )( 20 ) R V = 100 Vrms (b) Is = I + I L = V V 1000 1000 + = + = 5  j 5 = 5 2  45 A 20 j 20 20 j 20 (c) Zs =  j 20 + ( 20 )( j 20 ) = 10
20 + j 20 2  45 pf = cos ( 45 ) = 1 leading 2 1123 (d) No average power is dissipated in the capacitor or inductor. Therefore,
PAVE = PAVE = 500 W source 20 Vs I s cos = 500 Vs = 500 = I s cos ( 500 = 100 V 1 5 2 2 ) P11.65 Load 1: V = 100160 V I = 2190 A = 1.97  j 0.348 A P = 23.2 W, Q1 = 50 VAR 1 S1 = P + jQ1 = 23.2 + j 50 = 55.1265.1 VA 1 pf1 = cos 65.1 = 0.422 lagging
I1 = S1 55.1265.1 = = 0.551  94.9, so I1 = 0.55194.9 A 100160 Vs Load 2: S 2 = VI 2 = (100160 )( 2.12155 ) = 212  45 = 150  j150 VA I 2 = I  I1 = 1.97  j 0.348 + 0.047  j.549 = 2.12  155 A
pf 2 = cos ( 45 ) = 0.707 leading Total: S = S1 + S 2 = ( 23.2 + j50 ) + (150  j150 ) = 173.2  j100 = 200  30 VA pf = cos ( 30 ) = 0.866 leading P11.66 Z refrig = 120 = 14.12 8.5 Z refrig = 14.1245 = 10 + j10 R lamp V 2 (120 ) = = = 144 P 100
2 R range ( 240 ) = 2 12, 000 = 4.8 (a) and refrig = 1200 1200 = 8.5  45 Arms , I lamp = = 0.830 Arms 10 + j10 144 1124 I range = 2400 = 500 A 4.8 From KCL: I1 = I refrig + I range = 56  j 6 = 56.3  6.1 A I 2 = I lamp  I range = 50.83180 A I N = I1  I 2 = 7.92  49 A (b) Prefrig = I refrig 2 Rrefrig = 722.5 W and Qrefrig = I refrig X refrig = 722.5 VAR Plamp = 100 W and Q lamp = 0 2 Ptotal = 722 + 100 + 12, 000 = 12.82 kW S = 12,822 + j 722 = 12.843.2 kVA Qtotal = 722 + 0 + 0 = 722 VAR The overall power factor is pf = cos ( 3.2 ) = 0.998 , (c) Mesh equations:
 20 30 + j10  20 164 10  j10  144  10  j10 I A 1200  144 I B = 1200 158.8 + j10 I C 0 Solve to get: I A = 54.3  j1.57 = 54.3  1.7 Arms I B = 51.3  j 0.19 = 51.3  0.5Arms I C = 50 + j 0 = 500 Arms The voltage across the lamp is Vlamp = Rlamp I B  IC = 144 1.27  8.6 = 183.2 V 1125 P11.67 (a) VI=220 ( 7.6 ) = 1672 VA P 1317 = = .788 VI 1672 =cos 1pf = 38.0 Q=VIsin =1030VAR To restore the pf to 1.0, a capacitor is required to eliminate Q by introducing Q, then V2 (220)2 X c = 47 1030 = = Xc Xc pf = (b) C= 1
(c) 1 X = (377)(47) = 56.5 F
where = 0 P = VI cos then 1317 = 220I I = 6.0A for corrected pf
* Note I = 7.6A for uncorrected pf P11.68 First load:
S1 = P + jQ = P (1 + j tan (cos 1 (.6))) = 500(1 + j tan 53.1) = 500 + j 677 kVA Second load: S 2 = 400 + j 600 kVA
Total: S = S1 + S 2 = 900 + j1277 kVA
S desired = P + jP tan (cos 1 (.90)) = 900 + j 436 VA From the vector diagram: S desired = S + Q . Therefore
900 + j 436 = 900 + j1277 + Q Q =  j841 VAR V V (1000) 2 j =  j841 Z* = = = j1189 Z =  j1189 =  *  j841  j841 377 C Z Finally, C= 1 = 2.20 F (1189)(377) 2 2 1126 P11.69 (a) S = P + jQ = P + jP tan (cos 1 pf ) = 1000 + j1000 tan (cos 1 0.8) = 1000 + j 750 VA
S 1000 + j750 = = 10 + j7.5 I = 10  j 7.5 A Let VL = 1000 Vrms. Then I* = VL 1000 V 1000 ZL = L = = 836.9 = 6.4 + j 4.8 V I 12.536.9
VL =[6.4 + j (200)(.024) + Z L )(I ) = (12.8 + j 9.6)(10  j 7.5) = 2000 V 1 For maximum power transfer, we require ( 6.4 + j 4.8 )* = Z L  Z new = . YL +Ynew 1 1 1 = YL + Ynew Ynew =  = j 0.15 S (6.4  j4.8) 6.4  j 4.8 6.4 + j 4.8 (b) Then Z new =  j 6.67 so we need a capacitor given by 1 1 = 6.67 C = = 0.075 F C (6.67)(200) Section 117: The Power Superposition Principle P11.71 Use superposition since we have two different frequency sources. First consider the dc source ( = 0): 12 I1 = 14 = 12 A 12 + 2 2 P1 = I1 R = (12) 2 (2) = 288 W Next, consider the ac source ( = 20 rad/s): 1127 After a source transformation, current division gives  j 60 25 (12 j 5) 116.6 A I 2 = 9.166 =  j 60 5 + 2+ j 4 (12  j 5) Then
I (125)(2) P2 = 2 (2) = =125 W 2 2
2 Now using power superposition
P = P + P2 = 288 + 125 = 413 W 1 P11.72 Use superposition since we have two different frequency sources. First consider = 2000 rad/s source: Current division yields 8 j2 5 I1 = 5 63.4 A = 5 8 +8 j2 Then I 8 P= 1 = 20 W 1 2 Next consider = 8000 rad/s source.
2 Current division yields 1128 8 j7 5 I 2 =  j5  171.9 A = 8 50 +8 j7 Then I 8 P2 = 2 =2W 2 Now using power superposition
2 P = P + P2 = 22 W 1
P11.73 Use superposition since we have two different frequency. First consider the dc source ( = 0): 1 i 2 (t ) = 0 and i1 (t ) = 10 = 1 A 10 PR1 = i12 R1 = 12 (10) = 10 W PR 2 = 0 W Next consider = 5 rad/s sources. Apply KCL at the top node to get 6 I 2 + I1 + I 2  ( 4 30 ) + Apply KVL to get
10 I1 + (5 j 2) I 2 = 0 (10 I1 1040) =0 j10 Solving these equations gives
I1 = 0.56  64.3 A and I 2 = 1.04  42.5 A Then 1129 PR1 = 2 I1 R1 2 = ( 0.56 ) 2 (10) 2 = 1.57 W and PR 2 = 2 I2 R2 2 = (1.04 )
2 2 (5) = 2.7 W Now using power superposition
PR = 10 + 1.57 = 11.57 W and PR 2 = 0 + 2.7 = 2.7 W
1 P11.74 Use superposition since we have two different frequency. First consider the = 10 rad/s source:
I1 =
R1 V1 40 = = 0.28 + j 0.7 A Z 2 j5 V = 2 I1 = 2(0.28 + j.7) = 0.56 + j1.4 = 1.51 68.2 V V =  j 5 I1 = 3.77  21.8 V
C1 Next consider = 5 rad/s source.
I2 =
2 V2 690 = = 0.577  j 0.12 A Z 2  j10 VR = 2 I 2 = 2(.577  j 0.12) =1.15 j 0.24 V C2 =1.1711.8 V =  j10I 2 =5.9258.3 V Now using superposition vR (t) =1.51cos (10 t + 68.2) + 1.17 cos (5 t  11.8) V vC (t) = 3.77 cos (10 t  21.8) +5.9 cos (5 t  258.3) V Then V V
2 Reff 1.51 1.17 = + = 1.82 VReff =1.35 V 2 2 3.77 5.9 = + = 24.52 VCeff = 4.95 V 2 2
2 2 2 2 2 Ceff 1130 1131 Section 118: Maximum Power Transfer Theorem P11.81
Z t = 4000   j 2000 = 800  j1600 Z L = Z* =800 + j1600 t R =800 R + j1000 L = 800 + j1600 L =1.6 H P11.82 Z t = 25, 000   j 50, 000 = 20, 000  j10, 000 Z L =Z* = 20,000+ j10,000 t R = 20 k R + j L = 20, 000 + j10, 000 100 L =10,000 L =100 H After selecting these values of R and L, I = 1.4 mA and Pmax 0.14102 3 = ( 2010 ) = 19.5 mW 2 2 Since Pmax > 12 mW , yes, we can deliver 12 mW to the load. P11.83 j R 2 C = R  j R C Z t = 800 + j1600 and Z L = j 1 + ( RC ) 2 R C j R 2 C = R  j R C = 800  j1600 Z L = Z* t j 1+ ( RC ) 2 R C Equating the real parts gives 800 = R 4000 = 2 1+ ( RC ) 1+[(5000)(4000)C ]2 C = 0.1 F 1132 P11.84 Z t = 400 + j 800 and Z L = 2000   j1000 = 400  j 800 Since Z L = Z* the average power delivered to the load is maximum and cannot be increased by t adjusting the value of the capacitance. The voltage across the 2000 resistor is VR = 5 So 5.59 1 P= = 7.8 mW 2 2000 is the average power delivered to the 2000 resistor.
2 ZL = 2.5  j 5 = 5.59e j 63.4 V Zt + ZL P11.85 Notice that Zt,not ZL, is being adjusted .When Zt is fixed, then the average power delivered to the load is maximized by choosing ZL = Zt*. In contrast, when ZL is fixed, then the average power delivered to the load is maximized by minimizing the real part of Zt. In this case, choose R = 0. Since no average power is dissipated by capacitors or inductors, all of the average power provided by source is delivered to the load. Section 119: Mutual Inductance P1191
Vs + I j L1 + I j M + I j L2  I j M = 0 j ( L1 + L2  2 M ) = Vs I Therefore Lab = L1 + L2  2M 1133 P11.92 KCL: I1 + I 2 = I s The coil voltages are given by:
V = I1 j L1 + I 2 j M V = I 2 j L2 + I1 j M Then
I2 = V  j L1I s j ( M  L1 ) and Then V= Finally V = I 2 j L2 + ( I s  I 2 ) j M (V  j L1I s ) j ( L2  M ) j ( M  L1 ) + j MI s L L M 2 V = j 1 2 Is L1 + L2  2M Lab = L1 L2  M 2 L1 + L2  2M P11.93 Mesh equations: 141.40 + 2 I1 + j 40 I1  j 60 I 2 = 0 l200 I 2 + j 60 I 2  j 60 I1 = 0 I 2 = (0.2351) I1 Solving yields
I1 = 4.17  68 A and I 2 = 0.96  17A Finally i1 ( t ) = 4.2 cos(100t 68) A and i 2 ( t ) = 1.0 cos(100t 17) A 1134 P11.94 Mesh equations: (10+ j5) I 1  j50 I 2 = 10  j 50 I1 +( 400+ j 500 ) I 2 = 0 Solving the mesh equations using Cramer's rule:
I2 = (10+ j5)( 0 )(  j50 )(10 ) 2 (10+ j5) ( 400+ j500 )  (  j50 ) = 0.062 29.7 A Then V2 400 I 2 = = 40 I 2 = 40 ( 0.062 29.7 ) = 2.5 29.7 V1 100 P11.95 Mesh equations: 100  j 5 I1 + j 9 I1 + j 3 I 2 = 0 28 I 2 + j 6 I 2 + j 3 I1 + j 9 I 2  j 3 I 2 = 0 Solving the mesh equations yields
I1 = 0.25161 A and I 2 = 2.55  86 A then Finally V = j 9(I1  I 2 ) = j 9 ( 2.6 81 ) = 23 9 V v (t ) = 23cos (30t + 9) V 1135 P11.96 (a) I 2 = 0 I1 = 10 0 A i1 (0) = 10 A
w= L1 i1 (0) 2
2 = (0.3) (10) 2 = 15 J 2 (b) Mesh equations: j 6 I 2  j 3 I1 = 0 I1 = 2 I 2 I1 = 100 A I 2 = 50 A Then w= (c) 1 1 1 1 2 2 L1i1 (0) + L 2i1 (0)  M i1 (0) i 2 (0) = (0.3)(10) 2 + (1.2)(5) 2  (0.6) (10)(5) = 0 2 2 2 2
(7 + j 6) I 2  j 3 I1 = 0 I 2 = 3.25 49.4 A i 2 (t ) = 3.25cos(5t + 49.4) A i 2 (0) = 2.12 A Finally 1 1 w = (0.3) (10) 2 + (1.2) (2.12) 2  (0.6) (10) (2.12) = 5.0 J 2 2 P11.97 Mesh equations: VT + j8 I1 + j 5(I1  I 2 )  j 6 I1 + j 6 (I1  I 2 ) + j 5 I1 = 0 3 I 2 + j 6 (I 2  I1 )  j 5 I1 = 0 1136 Solving yields I 2 = (1.64 27 ) I1 I1 ( j 18) + I 2 ( j 11) = VT Then Z = VT = 8.2 + j 2 = 8.4 14 I1 P11.98 The coil voltages are given by V2 = j 4 ( I1  I 2 )  j 2 I1 + j 2 I 2 = j 2 I1  j 2 I 2 V1 = j 6 I1  j 2 (I1  I 2 )  j 4 I 2 = j 4 I1  j 2 I 2 V3 = j8 I 2  j 4 I1 + j 2 ( I1  I 2 ) =  j 2 I1 + j 6 I 2 The mesh equations are 5 I1 + V1 + 6 (I1  I 2 ) + V2 = 100 V2 + 6 (I 2  I1 ) + 2 I 2 + V3  j 5 I 2 = 0 Combining and solving yields 11 + j 6 10 6  j 4 0 60 + j 40 = = 1.2 0.28 A I2 = 11 + j 6 6  j 4 50 + j 33 6  j 4 8 + j 3 Finally
V =  j 5 I 2 = 6.0  89.72 A v(t ) = 6sin(2 t  89.7) V 1137 Section 1110: The Ideal Transformer P11.101 Z = (2 + j 3) + I1 = (100 j 75) =6 52 120 120 = =2A Z 6 100 j 75 100 j 75 V1 = I1 = (2) = 10  36.9 V 2 n 25 V2 = nV1 = 5 (1036.9) = 50 36.9 V I2 = I1 2 = A n 5 P11.102 (a) V0 = (5 103 )(10, 000) = 50 V n= (b) V N2 50 = 0 = = 5 N1 V1 10 1 1 R2 = (10 103 ) = 400 2 n 25 Rab = Is = (c) 10 10 = = 0.025 A = 25 mA Rab 400 1138 P11.103 Z1 = 1 Z 2 = 9 Z 2 = 9(5  j8) = 45  j 72 n2 Using voltage division, the voltage across Z 1 is 45 j 72 V1 = ( 80  50 ) = 74.4  73.3 V 45 j 72+ 30 + j 20 then V2 = nV1 = Using voltage division again yields  j8 890 Vc = V2 = ( 24.873.3 ) = 21.0  105.3 V 8958 5 j 8 74.4  73.3 = 24.8  73.3 V 3 P11.104 n = 5, Z1 = 200 ( 5) 2 = 8 V1 = 8 ( 500 ) = 400 V V2 = n V1 = 2000 V 8+ 2 1139 P11.105 Z= 320 j L + 2 n2 n Maximum power transfer requires j L = j160 k and n2 320 = 80 n2 so n = 2. Then L = 640 k so 640103 L = = 6.4 H 105 P11.106
Z= 1 ( 2 + 6) = 2 22 6 2 Voc = ( 2) 160 = 120 V 6 + 2 2 + 2 Z= 1 1 2 = 2 ( ) 2 2 160 1 1 I sc = I 2 = I1 = = 3.250 A 2 2 2+ 1 2 Then
Zt = 120 = 3.750 3.20 1140 P11.107
1 V1 2 V  V2 V1 I3 = 1 = 2 4 V V I 2 = I3  2 = 1 6 6 V 1 I1 =  I 2 =  1 2 12 V I T = I 3  I1 = 1 6 V Z= 1 =6 IT V2 = P11.108 * Maximum power transfer requires Z L = Z t . First 1 1 2 1 X C1 2 = X L1 , 2 = = n 10 5 n2 2 then 1 1 RL 2 + 1 2 = 100 n2 n1 1 100 3 = n1 = 2 3 10 n1 n2 = 5 1141 P11.109 ZL = 1 20 (1+ j 7.54) 8.123 = = 0.3 + j 0.13 52 20+10+ j 7.54 25 2 2 2 V V ( 230 ) = 88 kW/home PL = L = 2 = 2 R 2 2 R L 2( 0.3) Therefore, 529 kW are required for six homes. P11.1010 (a) Coil voltages: V1 = j16 I1 V2 = j12 I 2 Mesh equations: 8 I1 + V1  545 = 0 12 I 2  V2 = 0 Substitute the coil voltages into the mesh equations and do some algebra: 1142 8 I1 + j16 I1 = 545 I1 = 0.28  18.4 12 I 2 + j12 I 2 = 0 I 2 = 0
V2 = 12 I 2 = 0 (b) Coil voltages: V1 = j16 I1 + j8 I 2 V2 = j12 I 2 + j8 I1 Mesh equations: 8 I1 + V1  545 = 0 12 I 2  V2 = 0 Substitute the coil voltages into the mesh equations and do some algebra:
8 I1 + ( j16 I1 + j8 I 2 ) = 545 12 I 2 + ( j12 I 2 + j8 I1 ) = 0 I1 =  12 + j12 3 I 2 = ( j  1) I 2 j8 2 3 ( 8 + j16 ) 2 ( j  1) + j8 I 2 = 545 I 2 = 0.138  141 V2 = 12 I 2 = 1.65639 1143 (c ) Coil voltages and currents:
10 V2 8.66 8.66 I1 =  I2 10 V1 = Mesh equations: 8 I1 + V1  545 = 0 12 I 2  V2 = 0 Substitute into the second mesh equation and do some algebra: 10 8.66 10 12  I1 = V1 V1 = 12 I1 8.66 10 8.66 10 8 I1 + 12 I1 = 545 I1 = 0.20845 8.66 10 12 (10 ) 0.20845 = 2.8845 V2 = 12 I 2 = 12  I1 = 8.66 8.66 2 2 1144 PSpice Problems
SP 111 The coupling coefficient is k = 3 = 0.94868 . 25 1145 SP 112 Here is the circuit with printers inserted to measure the coil voltages and currents: Here is the output from the printers, giving the voltage of coil 2 as 2.498107.2, the current of coil 1 as 0.448494.57, the current of coil 2 as 0.624572.77 and the voltage of coil 1 as 4.29258.74:
FREQ 7.958E01 VM(N00984) 2.498E+00 VP(N00984) 1.072E+02 FREQ IM(V_PRINT1)IP(V_PRINT1) 7.958E01 4.484E01 9.457E+01 FREQ IM(V_PRINT2)IP(V_PRINT2) 7.958E01 6.245E01 7.277E+01 FREQ 7.958E01 VM(N00959) VP(N00959) 4.292E+00 5.874E+01 The power received by the coupled inductors is p= 2 = 0.78016  .78000 0 ( 4.292 )( 0.4484 ) cos ( 58.74  ( 94.57 ) ) + ( 2.498)( 0.6245) cos
2 (107.2  ( 72.77 ) ) 1146 SP 113 The inductance are selected so that L2 L1 = N2 N1 = 3 and the impedance of these inductors 2 are much larger that other impedance in the circuit. The 1 G resistor simulates an open circuit while providing a connected circuit. Here is the output from the printers, giving the voltage of coil 2 as 24.00114.1, the current of coil 1 as 4.000114.0, the current of coil 2 as 2.66765.90 and the voltage of coil 1 as 16.00114.1:
FREQ 6.366E01 VM(N00984) 2.400E+01 VP(N00984) 1.141E+02 FREQ IM(V_PRINT1)IP(V_PRINT1) 6.366E01 4.000E+00 1.140E+02 FREQ IM(V_PRINT2)IP(V_PRINT2) 6.366E01 2.667E+00 6.590E+01 FREQ 6.366E01 VM(N00959) 1.600E+01 VP(N00959) 1.141E+02 The power received by the transformer is p= 2 = 32  32.004 0 (16 )( 4 ) cos (114  114 ) + ( 24 )( 2.667 ) cos
2 (114  ( 66 ) ) 1147 SP 114 The inductance are selected so that L2 L1 = N2 N1 = 2 and the impedance of these inductors 5 are much larger that other impedance in the circuit. The 1 G resistor simulates an open circuit while providing a connected circuit.
FREQ 6.366E01 VM(N00921) 1.011E+02 VP(N00921) 7.844E+01 VR(N00921) 2.025E+01 VI(N00921) 9.903E+01 The printer output gives the voltage across the current source as 20.25 + j 99.03 = 101.178.44 V The input impedance is Zt = 20.25 + j 99.03 = 20.25 + j 99.03 = 101.178.44 1 52 (We expected Z t = 8 + 2 ( 2 + j ( 4 )( 4 ) ) = 20.5 + j 100 . That's about 1% error.) 2 1148 Verification Problems
VP 111 The average power supplied by the source is Ps = (12 )( 2.327 ) cos
2 ( 30  ( 25.22 ) ) = 7.96 W Capacitors and inductors receive zero average power, so the sum of the average powers received by the other circuit elements is equal to the sum of the average powers received by the resistors: 2.327 2 1.1292 PR = ( 4) + ( 2 ) = 10.83 + 1.27 = 12.10 W 2 2 The average power supplied by the voltage source is equal to the sum of the average powers received by the other circuit elements. The mesh currents cannot be correct. (What went wrong? It appears that the resistances of the two resistors were interchanged when the data was entered for the computer analysis. Notice that PR = 2.327 2 1.1292 ( 2) + ( 4 ) = 5.41 + 2.55 = 7.96 W 2 2 The mesh currents would be correct if the resistances of the two resistors were interchanged. The computer was used to analyze the wrong circuit.) VP 112 The average complex supplied by the source is Ss = (1230 )(1.647  17.92 ) * = (1230 )(1.64717.92 ) = 9.8847.92 = 6.62 + j 7.33
2 2 W The complex power received by the 4 resistor is S4 = ( 4 1.647  17.92 )(1.647  17.92 ) * = 5.43 + j 0
2 VA The complex power received by the 2 resistor is S2 = ( 2 1.094  13.15 )(1.094  13.15 ) * = 1.20 + j 0
2 VA 1149 The current in the 2 H inductor is (1.647  17.92 )  (1.094  13.15 ) = 0.5640  27.19
The complex power received by the 2 H inductor is S 2H = ( j 8 0.5640  27.19 )( 0.5640  27.19 ) * = 0 + j 1.27
2 VA The complex power received by the 4 H inductor is S 4H = ( j 16 1.094  13.15 )(1.094  13.15 ) * = 0 + j 9.57
2 VA S 4 + S 2 + S 2H + S 4H = ( 5.43 + j 0 ) + (1.20 + j 0 ) + ( 0 + j 1.27 ) + ( 0 + j 9.57 ) = 6.63 + j 10.84 Ss The complex power supplied by the voltage source is equal to the sum of the complex powers received by the other circuit elements. The mesh currents cannot be correct. (Suppose the inductances of the inductors were interchanged. Then the complex power received by the 4 H inductor would be S 4H = ( j 16 0.5640  27.19 )( 0.5640  27.19 ) * = 0 + j 2.54
2 VA The complex power received by the 2 H inductor would be S 2H = ( j 8 1.094  13.15 )(1.094  13.15 ) * = 0 + j 4.79
2 VA S 4 + S 2 + S 2H + S 4H = ( 5.43 + j 0 ) + (1.20 + j 0 ) + ( 0 + j 2.54 ) + ( 0 + j 4.79 ) = 6.63 + j 7.33 S s The mesh currents would be correct if the inductances of the two inductors were interchanged. The computer was used to analyze the wrong circuit.) VP 113 The voltage across the right coil must be equal to the voltage source voltage. Notice that the mesh currents both enter the undotted ends of the coils. In the frequency domain, the voltage across the right coil is 1150 ( j 16 )(1.001  47.01) + ( j12 )( 0.4243  15 ) = 16.01642.99 + 5.09275 = (11.715 + j 10.923) + (1.318 + j 4.918 )
= 13.033 + j 15.841 = 20.51350.55 This isn't equal to the voltage source voltage so the computer analysis isn't correct. What happened? A data entry error was made while doing the computer analysis. Both coils were described as having the dotted end at the top. If both coils had the dot at the top, the equation for the voltage across the right coil would be ( j 16 )(1.001  47.01)  ( j12 )( 0.4243  15 ) = 16.01642.99  5.09275 = (11.715 + j 10.923)  (1.318 + j 4.918 )
= 10.397 + j 6.005 = 12.00730.01 This is equal to the voltage source voltage. The computer was used to analyze the wrong circuit. VP 114 First check the ratio of the voltages across the coils. n1 2 1230 = 2.5 = n2 5 ( 75 )( 0.06430 )
The transformer voltages don't satisfy the equations describing the ideal transformer. The given mesh currents are not correct. That' enough but let's also check the ratio of coil currents. (Notice that the reference direction of the i2(t) is different from the reference direction that we used when discussing transformers.) n1 2 0.06430 = 2.5 = n2 5 0.025630 The transformer currents don't satisfy the equations describing the ideal transformer. In both case, we calculated 1 . This suggests that a data 2.5 n2 entry error was made while doing the computer analysis. The numbers of turns for the two coils was interchanged. to be 2.5 instead of 0.4 = n1 1151 1152 1153 Design Problems
DP 11. 1 P 100 S= = =125 kVA P =100 W pf 0.8 pf = 0.8 Q = S sin (cos 1 0.8) =125sin (36.9) =75 kVAR (a) Now pf = 0.95 so
P 100 = =105.3 kVA pf 0.95 Q = S sin (cos 1 0.95) =105.3sin (18.2) =32.9 kVAR S= so an additional 125  105.3 = 19.7 kVA is available. (b) Now pf = 1 so
S= P 100 = =100 kVA pf 1 Q = S sin (cos 1 1) = 0 and an additional 125100= 25 kVA is available. (c) (d) Corrected power factor Additional available apparent power Reduction in reactive power 0.95 19.7 kVA 42.1 kVAR 1.0 25 kVA 75 kVAR In part (a), the capacitors are required to reduce Q by 75 32.9 = 42.1 kVAR. In part (b), the capacitors are required to reduce Q by 75 0 = 0 kVAR. 1154 DP 112 This example demonstrates that loads can be specified either by kW or kVA. The procedure is as follows: First load: Second load: P = S1 pf =( 50 )( 0.9 ) = 45 W S1 =50 VA 1 1 pf =0.9 Q1 = S1 sin (cos 0.9) =50sin (25.8) = 21.8 kVAR P 45 = 49.45 kVA S2 = 2 = P2 = 45 W pf 0.91 pf = 0.91 Q = S sin (cos 1 0.91) = 49.45sin (24.5) = 20.5 kVAR 2 2
S L = S1 + S 2 = (45 + 45) + j(21.8+20.5) = 90 + j 42.3 kVA Total load: Specified load: P 90 Ss = s = =92.8 kVA Ps =90 W pf 0.97 pf = 0.97 Q = S sin (cos 1 0.97) =92.8sin (14.1) = 22.6 kVAR s s
The compensating capacitive load is Qc = 42.3  22.6 = 19.7 kVAR . The required capacitor is calculated as Vc (7.2 103 ) 2 1 Xc = = = 2626 C = = 1.01 F 3 Qc 19.7 10 377 (2626)
2 1155 DP 113 Find the open circuit voltage: 10 + 5I + j10I  0.5 Voc = 0 and I= so Voc = 836.9 = 6.4 + j 4.8 V Find the short circuit current: I sc = 100 = 20 A 5 10  Voc 5 The the Thevenin impedance is: Zt = The short circuit forces the controlling voltage to be zero. Then the controlled voltage is also zero. Consequently the dependent source has been replaced by a short circuit. (a) (c) Voc = 3.2 + j 2.4 I sc Maximum power transfer requires Z L = Z t * = 3.2  j 2.4 . ZL can be implemented as the series combination of a resistor and a capacitor with
R = 3.2 and C = 1 = 4.17 mF . (100 ) (2.4) (b) Pmax =  Voc 2 64 = = 2.5 W 8R 8 ( 3.2 ) 1156 DP 114 Using an equation from section 11.8, the power is given as R Vs 2 n 2 P= 2 2 R 3 3 + 2 + 2 + 4 n n 2 When R = 4 , n 2 R Vs P= 25n 4 + 48n 2 + 25
0=
4 2 2 3 dP 2 2 n(25n + 48n + 25)  n (100n + 96n ) = R Vs dn (25n 4 + 48n 2 + 25) 2 5 4  50n + 50n = 0 n = 1 n = 1 2 When R = 8 , a similar calculation gives n = 1.31. 1157 DP 115 Maximum power transfer requires 10 + j 6.28 = Z1 = (1 + j 0.628 ) * n2 Equating real parts gives 10 = 1 n = 3.16 n2 Equating imaginary parts requires jX =  j 0.628 3.162 X = 6.28 This reactance can be realized by adding a capacitance C in series with the resistor and inductor that comprise Z2. Then 6.28 = X =  1 1 + 6.28 C = = 0.1267 F 5 5 ( 2 10 ) C ( 2 10 ) (12.56 ) 1158 DP 116 Maximum power transfer requires
1  R = (100 + j107 106 ) * j107 C R = 100  j10 1 + j107 R C R = (100  j10) (1 + j107 R C ) = 100 + 108 R C + j (109 R C  10 )
Equating real and imaginary parts yields R = 100 + 108 R C and 109 R C  10 = 0
then
RC = 108 108 108 R = 100 + 108 R = 99 C = = 0.101 nF 99 R 1159 Chapter 12: ThreePhase Circuits
Exercises
Ex. 12.31
VC = 120  240 so VA = 1200 and VB = 120  120 Vbc = 3 (120 )  90 Ex. 12.41 Fourwire YtoY Circuit Mathcad analysis (12v4_1.mcd):
Describe the threephase source:
j 180 0 Vp := 120
j 180  120 j 180 120 Va := Vp e Vb := Va e Vc := Va e Describe the threephase load: Calculate the line currents: IaA = 1.079  0.674i IaA = 1.272 180 arg( IaA ) = 32.005 IaA := ZA := 80 + j 50 Va ZA IbB := Vb ZB ZB := 80 + j 80 IcC := Vc ZC ZC := 100  j 25 IbB = 1.025  0.275i IbB = 1.061 180 arg( IbB) = 165 IcC = 0.809 + 0.837i IcC = 1.164 180 arg( IcC) = 134.036 121 Calculate the current in the neutral wire: INn := IaA + IbB + IcC INn = 0.755  0.112i SC := IcC IcC ZC SC = 135.529  33.882i Calculate the power delivered to the load: SA := IaA IaA ZA SB := IbB IbB ZB SA = 129.438 + 80.899i SB = 90 + 90i Total power delivered to the load: SA + SB + SC = 354.968 + 137.017i Calculate the power supplied by the source: Sa := IaA Va Sa = 129.438 + 80.899i Total power delivered by the source: Sb := IbB Vb Sb = 90 + 90i Sc := IcC Vc Sc = 135.529  33.882i Sa + Sb + Sc = 354.968 + 137.017i Ex. 12.42 Fourwire YtoY Circuit Mathcad analysis (12x4_2.mcd):
Describe the threephase source:
j 180 0 Vp := 120
j 180  120 j 180 120 Va := Vp e Vb := Va e Vc := Va e ZB := ZA Vb ZB IcC := Vc ZC Describe the threephase load: Calculate the line currents: IaA = 1.92  1.44i IaA = 2.4 180 arg( IaA ) = 36.87 IaA := ZA := 40 + j 30 Va ZA IbB := ZC := ZA IbB = 2.207  0.943i IbB = 2.4 180 arg( IbB) = 156.87 IcC = 0.287 + 2.383i IcC = 2.4 180 arg( IcC) = 83.13 122 Calculate the current in the neutral wire: INn := IaA + IbB + IcC INn = 0 SC := IcC IcC ZC SC = 230.4 + 172.8i Calculate the power delivered to the load: SA := IaA IaA ZA SB := IbB IbB ZB SA = 230.4 + 172.8i SB = 230.4 + 172.8i Total power delivered to the load: SA + SB + SC = 691.2 + 518.4i Calculate the power supplied by the source: Sa := IaA Va Sa = 230.4 + 172.8i Total power delivered by the source: Sb := IbB Vb Sb = 230.4 + 172.8i Sa + Sb + Sc = 691.2 + 518.4i Sc := IcC Vc Sc = 230.4 + 172.8i Ex. 12.43 Threewire unbalanced YtoY Circuit with line impedances Mathcad analysis (12x4_3.mcd):
Describe the threephase source:
j 180 0 Vp := 120
j 180  120 j 180 120 Va := Vp e Vb := Va e Vc := Va e Describe the threephase load: ZA := 80 + j 50 ZB := 80 + j 80 ZC := 100  j 25 Calculate the voltage at the neutral of the load with respect to the neutral of the source:
4 j 3 2 j 3 VnN := ZA ZC e + ZA ZB e + ZB ZC ZA ZC + ZA ZB + ZB ZC VnN = 28.888 Vp 180 arg( VnN) = 150.475 VnN = 25.137  14.236i 123 Calculate the line currents: IaA = 1.385  0.687i IaA = 1.546 180 Check: arg( IaA ) = 26.403 IaA := Va  VnN ZA IbB := Vb  VnN ZB IcC := Vc  VnN ZC IbB = 0.778  0.343i IbB = 0.851 180 arg( IbB) = 156.242 IcC = 0.606 + 1.03i IcC = 1.195 180 arg( IcC) = 120.475 IaA + IbB + IcC = 0 Calculate the power delivered to the load: SA := IaA IaA ZA SB := IbB IbB ZB SA = 191.168 + 119.48i Total power delivered to the load: SB = 57.87 + 57.87i SA + SB + SC = 391.88 + 141.639i SC := IcC IcC ZC SC = 142.843  35.711i Ex. 12.44 Threewire balanced YtoY Circuit with line impedances Mathcad analysis (12x4_4.mcd):
Describe the threephase source:
j 180 0 Vp := 120
j 180  120 j 180 120 Va := Vp e Vb := Va e Vc := Va e ZB := ZA Describe the threephase load: ZA := 40 + j 30 ZC := ZA Calculate the voltage at the neutral of the load with respect to the neutral of the source:
4 j 3 2 j 3 VnN := ZA ZC e + ZA ZB e + ZB ZC ZA ZC + ZA ZB + ZB ZC Vp 124 VnN = 1.31 10  14 + 1.892i 10  14 VnN = 2.301 10 IbB :=  14 180 arg( VnN) = 124.695 IcC := Vc  VnN ZC Calculate the line currents: IaA = 1.92  1.44i IaA = 2.4 180 Check: arg( IaA ) = 36.87 IaA := Va  VnN ZA Vb  VnN ZB IbB = 2.207  0.943i IbB = 2.4 180
 15 IcC = 0.287 + 2.383i IcC = 2.4 180 arg( IcC) = 83.13 arg( IbB) = 156.87  2.22i 10
 15 IaA + IbB + IcC = 1.055 10 Calculate the power delivered to the load: SA := IaA IaA ZA SB := IbB IbB ZB SA = 230.4 + 172.8i Total power delivered to the load: SB = 230.4 + 172.8i SA + SB + SC = 691.2 + 518.4i SC := IcC IcC ZC SC = 230.4 + 172.8i Ex. 12.61 Balanced delta load: (See Table 12.51) Z = 180  45 phase currents: I AB = I BC = I CA VAB 3600 = = 245 A Z 180 45 VBC 360120 = = 2 75 A Z 18 45 VCA 360120 = = = 2165 A Z 180 45 line currents: I A = I AB  I CA = 245  2165 = 2 315 A I B = 2 3105 A I C = 2 3135 A 125 Ex. 12.71 Threewire YtoDelta Circuit with line impedances Mathcad analysis (12x4_4.mcd):
Describe the threephase source:
j 180 0 Vp := 110
j 180  120 j 180 120 Va := Vp e Vb := Va e Vc := Va e Z2 := Z1 Describe the delta connected load: Z1 := 150 + j 270 Z2 Z3 Z1 + Z2 + Z3 Z3 := Z1 Z1 Z2 Convert the delta connected load to the equivalent Y connected load: ZA := Z1 Z3 Z1 + Z2 + Z3 ZB := ZC := Z1 + Z2 + Z3 ZA = 50 + 90i Describe the threephase line: ZB = 50 + 90i ZaA := 10 + j 25 ZC = 50 + 90i ZbB := ZaA ZcC := ZaA 126 Calculate the voltage at the neutral of the load with respect to the neutral of the source:
4 j 3 2 j 3 VnN := ( ZaA + ZA ) ( ZcC + ZC) e + ( ZaA + ZA ) ( ZbB + ZB) e + ( ZbB + ZB) ( ZcC + ZC) ( ZaA + ZA ) ( ZcC + ZC) + ( ZaA + ZA ) ( ZbB + ZB) + ( ZbB + ZB) ( ZcC + ZC)
 14 Vp VnN = 1.172 10 + 1.784i 10  14 VnN = 2.135 10  14 180 arg( VnN) = 123.304 Calculate the line currents: IaA = 0.392  0.752i IaA = 0.848 180 Check: arg( IaA ) = 62.447 IaA := Va  VnN ZA + ZaA IbB := Vb  VnN ZB + ZbB IcC := Vc  VnN ZC + ZcC IbB = 0.847 + 0.036i IbB = 0.848 180 arg( IbB) = 177.553 IcC = 0.455 + 0.716i IcC = 0.848 180 arg( IcC) = 57.553 IaA + IbB + IcC = 0 Calculate the phase voltages of the Yconnected load: VAN := IaA ZA VAN = 87.311 180 arg( VAN) = 1.502 VBN := IbB ZB VBN = 87.311 180 arg( VBN) = 121.502 VCN := IcC ZC VCN = 87.311 180 arg( VCN) = 118.498 Calculate the linetoline voltages at the load: VAB := VAN  VBN VAB = 151.227 180 arg( VAB) = 28.498 VBC:= VBN  VCN VBC = 151.227 180 arg( VBC = 91.502 ) VCA := VCN  VAN VCA = 151.227 180 arg( VCA) = 148.498 Calculate the phase currents of the connected load: IAB := VAB Z3 IBC := VBC Z1 ICA := VCA Z2 IAB = 0.49 180 arg( IAB) = 32.447 IBC = 0.49 180 arg( IBC) = 152.447 ICA = 0.49 180 arg( ICA) = 87.553 127 Ex. 12.81 Continuing Ex. 12.81:
Calculate the power delivered to the load: SA := IaA IaA ZA SB := IbB IbB ZB SA = 35.958 + 64.725i Total power delivered to the load: SB = 35.958 + 64.725i SA + SB + SC = 107.875 + 194.175i SC := IcC IcC ZC SC = 35.958 + 64.725i Ex. 12.91 P1 = VAB I A cos( +30 ) + VCB I C cos(  30 )= P + P2
1 pf = .4 lagging = 61.97 So P T = 450(24) cos 91.97 + cos 31.97 = 8791 W P 1 =  371 W P2 = 9162 W Ex. 12.92 Consider Fig. 12.91 with P = 60 kW P2 = 40 kW . 1 (a.) P = P + P2 = 100 kW 1 (b.) use equation 12.97 to get tan = 3 then P2  P 40 60 1 = 3 =  .346 =  19.11 PL + P2 100
pf = cos (  19.110) = 0.945 leading 128 Problems
Section 123: Three Phase Voltages P12.31 Given VC = 277 45 and an abc phase sequence:
VA = 277 ( 45120 ) = 277  75 VB = 277 ( 45 +120 ) = 277 165
VAB = VA  VB =( 277  75 )( 277 165 ) =( 71.69  j 267.56 ) ( 267.56+ j 71.69 ) =339.25 j 339.25 = 479.77  45 480  45 Similarly: VBC = 480  165 and VCA = 480 75
P12.32 VAB = VA 330 VA = VAB 330 = 12470 145 V In our case: So VAB = VBA =  (12470 35 )
VA = 12470 145 = 7200115 330 Then, for an abc phase sequence:
VC = 7200 (115 + 120 ) = 7200 235 = 7200  125 VB = 7200 (115  120 ) = 7200  5 V P12.33 Vab = Va 330 Va = Vab 330 In our case, the linetoline voltage is So the phase voltage is Vab = 1500 30 V 1500 30 Va = = 8660 V 330 129 Section 124: The YtoY Circuit P12.41 Balanced, threewire, YY circuit: where Z A = Z B = Z C = 1230 = 10.4 + j 6
MathCAD analysis (12p4_1.mcd):
Describe the threephase source: 180 Vp := 208 3
j 180  120 j 180 120 j 0 Va := Vp e Vb := Va e Vc := Va e Describe the balanced threephase load: ZA := 10.4 + j 6 ZB := ZA ZC := ZB Check: The voltage at the neutral of the load with respect to the neutral of the source should be zero:
4 j 3 2 j 3 VnN := ZA ZC e + ZA ZB e + ZB ZC ZA ZC + ZA ZB + ZB ZC IaA := Va  VnN ZA Vp VnN = 2.762 10 Vb  VnN ZB  14 Calculate the line currents: IaA = 8.663  4.998i IaA = 10.002 180 Check: arg( IaA ) = 29.982 IbB := IcC := Vc  VnN ZC
3 IbB = 8.66  5.004i IbB = 10.002 180  15 IcC = 3.205 10 IcC = 10.002 180 + 10.002i arg( IbB) = 149.982  1.066i 10
 14 arg( IcC) = 90.018 IaA + IbB + IcC = 4.696 10 1210 Calculate the power delivered to the load: SA := IaA IaA ZA SB := IbB IbB ZB SA = 1.04 10 + 600.222i Total power delivered to the load:
3 SC := IcC IcC ZC SC = 1.04 10 + 600.222i
3 3 SB = 1.04 10 + 600.222i
3 3 SA + SB + SC = 3.121 10 + 1.801i 10 Consequently: (a) The phase voltages are
Va = 208 0 = 1200 V rms, Vb = 120  120 V rms and Vc = 120120 V rms 3 (c) (b) The currents are equal the line currents
I a = I aA = 10  30 A rms, I b = I bB = 10  150 A rms and
I c = I cC = 1090 A rms (d) The power delivered to the load is S = 3.121 + j1.801 kVA . P12.42 Balanced, threewire, YY circuit: where Va = 1200 Vrms, Vb = 120  120 Vrms and Vc = 120120 Vrms
Z A = Z B = Z C = 10 + j ( 2 60 ) (100 103 ) = 10 + j 37.7 Z aA = Z bB = Z cC = 2 and Mathcad Analysis (12p4_2.mcd): 1211 Describe the threephase source:
j 180 0 Vp := 120
j 180  120 j 180 120 Va := Vp e Vb := Va e Vc := Va e ZB := ZA ZbB := ZaA Describe the threephase load: Describe the threephase line: ZA := 10 + j 37.7 ZaA := 2 ZC := ZB ZcC := ZaA Calculate the voltage at the neutral of the load with respect to the neutral of the source:
4 j 3 2 j 3 VnN := ( ZaA + ZA ) ( ZcC + ZC) e + ( ZaA + ZA ) ( ZbB + ZB) e + ( ZbB + ZB) ( ZcC + ZC) ( ZaA + ZA ) ( ZcC + ZC) + ( ZaA + ZA ) ( ZbB + ZB) + ( ZbB + ZB) ( ZcC + ZC)
 15 Vp VnN = 8.693 10 + 2.232i 10 IaA :=  14 VnN = 2.396 10 IbB :=  14 180 arg( VnN) = 111.277 IcC := Vc  VnN ZC + ZcC Calculate the line currents: IaA = 0.92  2.89i IaA = 3.033 180 Check: arg( IaA ) = 72.344 Va  VnN ZA + ZaA Vb  VnN ZB + ZbB IbB = 2.963 + 0.648i IbB = 3.033 180 arg( IbB) = 167.656  3.109i 10
 15 IcC = 2.043 + 2.242i IcC = 3.033 180 arg( IcC) = 47.656 IaA + IbB + IcC = 1.332 10  15 Calculate the phase voltages at the load: VA = 118.301 180 arg( VA) = 2.801 VA := ZA IaA VB = 118.301 180 arg( VB) = 117.199 VB := ZB IbB VC := ZC IcC VC = 118.301 180 arg( VC) = 122.801 Consequently, the linetoline voltages at the source are:
Vab = Va 330 = 1200 330 = 20830 Vrms, Vbc = 208  120 Vrms and Vca = 208120 Vrms The linetoline voltages at the load are: VAB = VA 330 = 118.33 330 = 20533 Vrms, Vbc = 205  117 Vrms and Vca = 205123 Vrms and the phase currents are I a = I aA = 10  72 A rms, I b = I bB = 3168 A rms and I c = I cC = 348 A rms
1212 P12.43 Balanced, threewire, YY circuit: where Va = 100 V = 7.070 V rms, Vb = 7.07  120 V rms and Vc = 7.07120 V rms and
Z A = Z B = Z C = 12 + j (16 )(1) = 12 + j16 MathCAD analysis (12p4_3.mcd):
Describe the threephase source: 180 Vp := 10 2
j 180  120 j 180 120 j 0 Va := Vp e Vb := Va e Vc := Va e Describe the balanced threephase load: ZA := 12 + j 16 ZB := ZA ZC := ZB Check: The voltage at the neutral of the load with respect to the neutral of the source should be zero:
4 j 3 2 j 3 VnN := ZA ZC e + ZA ZB e + ZB ZC ZA ZC + ZA ZB + ZB ZC IaA := Va  VnN ZA Vp VnN = 1.675 10 Vb  VnN ZB  15 Calculate the line currents: IaA = 0.212  0.283i IaA = 0.354 180 arg( IaA ) = 53.13 IbB := IcC := Vc  VnN ZC IbB = 0.351  0.042i IbB = 0.354 180 arg( IbB) = 173.13 IcC = 0.139 + 0.325i IcC = 0.354 180 arg( IcC) = 66.87 Calculate the power delivered to the load: SB := IbB IbB ZB SA := IaA IaA ZA SA = 1.5 + 2i Total power delivered to the load: SB = 1.5 + 2i SA + SB + SC = 4.5 + 6i SC := IcC IcC ZC
SC = 1.5 + 2i 1213 Consequently (a) The rms value of ia(t) is 0.354 A rms. (b) The average power delivered to the load is P = Re {S} = Re {4.5 + j 6} = 4.5 W P12.44 Unbalanced, threewire, YY circuit: where Va = 1000 V = 70.70 V rms, Vb = 70.7  120 V rms and Vc = 7.07120 V rms Z C = 60 + j ( 377 ) ( 20 103 ) = 60 + j 7.54 Z A = 20 + j ( 377 ) ( 60 103 ) = 20 + j 22.6 , Z B = 40 + j ( 377 ) ( 40 103 ) = 40 + j 15.1 Z aA = Z bB = Z cC = 10 + j ( 377 ) ( 5 103 ) = 10 + j 1.89 and Mathcad Analysis (12p4_4.mcd):
Describe the threephase source:
j 180 0 Vp := 100
j 180 120 j 180  120 Va := Vp e Vb := Va e Vc := Va e Enter the frequency of the 3phase source: := 377 Describe the threephase load: Describe the threephase line: ZA := 20 + j 0.06 ZB := 40 + j 0.04 ZC := 60 + j 0.02 ZcC := ZaA ZaA := 10 + j 0.005 ZbB := ZaA 1214 Calculate the voltage at the neutral of the load with respect to the neutral of the source:
4 j 3 2 j 3 VnN := ( ZaA + ZA ) ( ZcC + ZC) e + ( ZaA + ZA ) ( ZbB + ZB) e + ( ZbB + ZB) ( ZcC + ZC) ( ZaA + ZA ) ( ZcC + ZC) + ( ZaA + ZA ) ( ZbB + ZB) + ( ZbB + ZB) ( ZcC + ZC) VnN = 27.42 IaA := Va  VnN ZA + ZaA IbB := Vb  VnN ZB + ZbB 180 arg( VnN) = 63.561 IcC := Vc  VnN ZC + ZcC Vp VnN = 12.209  24.552i Calculate the line currents: IaA = 2.156  0.943i IaA = 2.353 180 arg( IaA ) = 23.619 IbB = 0.439 + 2.372i IbB = 2.412 180 arg( IbB) = 100.492 IcC = 0.99  0.753i IcC = 1.244 180 arg( IcC) = 142.741 Calculate the power delivered to the load: IbB IbB IaA IaA ZA SB := ZB SA := 2 2 ( ) ( ) SC := (IcC IcC) 2 ZC SA = 55.382 + 62.637i Total power delivered to the load: SB = 116.402 + 43.884i SC = 46.425 + 5.834i SA + SB + SC = 218.209 + 112.355i The average power delivered to the load is P = Re {S} = Re {218.2 + j112.4} = 218.2 W P12.45 Balanced, threewire, YY circuit: where Va = 1000 V = 70.70 V rms, Vb = 70.7  120 V rms and Vc = 7.07120 V rms Z A = Z B = Z C = 20 + j ( 377 ) ( 60 103 ) = 20 + j 22.6 Z aA = Z bB = Z cC = 10 + j ( 377 ) ( 5 103 ) = 10 + j 1.89 and 1215 Mathcad Analysis (12p4_5.mcd):
Describe the threephase source:
j 180 0 Vp := 100
j 180 120 j 180  120 Va := Vp e Vb := Va e Vc := Va e Enter the frequency of the 3phase source: := 377 Describe the threephase load: Describe the threephase line: ZA := 20 + j 0.06 ZaA := 10 + j 0.005 ZB := ZA ZbB := ZaA ZC := ZA ZcC := ZaA Calculate the voltage at the neutral of the load with respect to the neutral of the source:
4 j 3 2 j 3 VnN := ( ZaA + ZA ) ( ZcC + ZC) e + ( ZaA + ZA ) ( ZbB + ZB) e + ( ZbB + ZB) ( ZcC + ZC) ( ZaA + ZA ) ( ZcC + ZC) + ( ZaA + ZA ) ( ZbB + ZB) + ( ZbB + ZB) ( ZcC + ZC)
 15 Vp VnN = 8.982 10 + 1.879i 10 IaA :=  14 VnN = 2.083 10 IbB :=  14 180 arg( VnN) = 115.55 IcC := Vc  VnN ZC + ZcC Calculate the line currents: IaA = 1.999  1.633i IaA = 2.582 180 arg( IaA ) = 39.243 Va  VnN ZA + ZaA Vb  VnN ZB + ZbB IbB = 0.415 + 2.548i IbB = 2.582 180 arg( IbB) = 80.757 IcC = 2.414  0.915i IcC = 2.582 180 arg( IcC) = 159.243 Calculate the power delivered to the load: SA := ZA 2 SA = 66.645 + 75.375i (IaA IaA) SB := ZB 2 SB = 66.645 + 75.375i (IbB IbB) SC := ZC 2 SC = 66.645 + 75.375i (IcC IcC) Total power delivered to the load: SA + SB + SC = 199.934 + 226.125i The average power delivered to the load is P = Re {S} = Re {200 + j 226} = 200 W 1216 P12.46 Unbalanced, threewire, YY circuit: where Va = 10  90 V = 7.07  90 V rms, Vb = 7.07150 V rms and Vc = 7.0730 V rms and Z A = 4 + j ( 4 )(1) = 4 + j 4 , Z B = 2 + j ( 4 )( 2 ) = 2 + j 8 and Z C = 4 + j ( 4 )( 2 ) = 4 + j 8 Mathcad Analysis (12p4_6.mcd):
Describe the threephase source:
j 180  90 Vp := 10
j 180 150 j 180 30 Va := Vp e Vb := Vp e Vc := Vp e Enter the frequency of the 3phase source: := 4 Describe the threephase load: ZA := 4 + j 1 ZB := 2 + j 2 ZC := 4 + j 2 Calculate the voltage at the neutral of the load with respect to the neutral of the source: VnN := VnN = 1.528  0.863i Calculate the line currents: IaA = 1.333  0.951i IaA = 1.638 180 arg( IaA ) = 144.495 IaA := ZA ZC Vb + ZA ZB Vc + ZB ZC Va ZA ZC + ZA ZB + ZB ZC VnN = 1.755 Va  VnN ZA IbB := Vb  VnN ZB 180 arg( VnN) = 29.466 IcC := Vc  VnN ZC IbB = 0.39 + 1.371i IbB = 1.426 180 arg( IbB) = 74.116 IcC = 0.943  0.42i IcC = 1.032 180 arg( IcC) = 24.011 1217 Calculate the power delivered to the load: IaA IaA IbB IbB SA := ZA SB := ZB 2 2 ( ) ( ) SC := (IcC IcC)
2 ZC SA = 5.363 + 5.363i Total power delivered to the load: SB = 2.032 + 8.128i SA + SB + SC = 9.527 + 17.754i SC = 2.131 + 4.262i The average power delivered to the load is P = Re {S} = Re {9.527 + j17.754} = 9.527 W P12.47 Unbalanced, threewire, YY circuit: where Va = 10  90 V = 7.07  90 V rms, Vb = 7.07150 V rms and Vc = 7.0730 V rms and Z A = Z B = Z C = 4 + j ( 4 )( 2 ) = 4 + j 8 Mathcad Analysis (12p4_7.mcd):
Describe the threephase source:
j 180  90 Vp := 10
j 180 150 j 180 30 Va := Vp e Vb := Vp e Vc := Vp e Enter the frequency of the 3phase source: := 4 Describe the threephase load: ZA := 4 + j 2 ZB := ZA ZC := ZA The voltage at the neutral of the load with respect to the neutral of the source should be zero: VnN := ZA ZC Vb + ZA ZB Vc + ZB ZC Va ZA ZC + ZA ZB + ZB ZC
 15 VnN = 1.517 10 1218 Calculate the line currents: IaA = 1  0.5i IaA = 1.118 180 IaA := Va  VnN ZA IbB := Vb  VnN ZB IcC := Vc  VnN ZC IbB = 0.067 + 1.116i IbB = 1.118 180 arg( IbB) = 86.565 IcC = 0.933  0.616i IcC = 1.118 180 arg( IcC) = 33.435 arg( IaA ) = 153.435 Calculate the power delivered to the load: IaA IaA IbB IbB SA := ZA SB := ZB 2 2 ( ) ( ) SC := (IcC IcC) 2 ZC SA = 2.5 + 5i Total power delivered to the load: SB = 2.5 + 5i SA + SB + SC = 7.5 + 15i SC = 2.5 + 5i The average power delivered to the load is P = Re {S} = Re {7.5 + j15} = 7.5 W Section 126: The  Connected Source and Load P12.51 Given I B = 50  40 A rms and assuming the abc phase sequence we have I A = 5080 A rms and I C = 50200 A rms From Eqn 12.64 I A = I AB 3  30 I AB = so IA 3  30 I AB = I BC 5080 = 28.9110 A rms 330 = 28.9  10 A rms and ICA = 28.9  130 A rms 1219 P12.52 The two delta loads connected in parallel are equivalent to a single delta load with Z = 5  20 = 4 The magnitude of phase current is 480 Ip = = 120 A rms 4 The magnitude of line current is I L = 3 I p = 208 A rms Section 126: The Y to  Circuit P12.61
We have a delta load with Z = 1230 . One phase current is 208 208 30  150 V V V 3 3 = 2080 = 17.31  30 A rms = AB = A A = Z Z 1230 1230 I AB The other phase currents are I BC = 17.31  150 A rms and I CA = 17.3190 A rms One line currents is I A = I AB 3  30 = (17.31  30 ) The other line currents are I B = 30  120 A rms and I C = 30120 A rms The power delivered to the load is
P = 3( 208 ) (30) cos ( 0  30 ) = 9360 W 3 ( 3  30 = 300 A rms ) 1220 P12.62 The balanced delta load with Z = 39 40 is equivalent to a balanced Y load with
ZY = Z = 13  40 = 9.96  j 8.36 3 Z T = Z Y + 4 = 13.96  j 8.36 = 16.3  30.9 480 30 3 then I A = = 170.9 A rms 16.3 30.9 P12.63 Vab = Va 330 Va = In our case, the given linetoline voltage is Vab 330 Vab = 380 30 V rms 380 30 So one phase voltage is Va = = 2000 V rms 330 So VAB = 38030 V rms VA = 2200 V rms
VBC = 38090 V rms VCA = 380150 V rms One phase current is VB = 220120 V rms VC = 220120 V rms IA =
The other phase currents are VA 2200 = 44  53.1 A rms Z 3+ j4 I B = 44173.1 A rms amd I C = 4466.9 A rms 1221 P12.64 Vab = Va 330 Va =
In our case, the given linetoline voltage is Vab 330 Vab = 380 0 V rms
So one phase voltage is So Va = 380 0 = 200  30 V rms 330 Va = 220  30 V rms Vb = 220150 V rms Vc = 22090 V rms Vab = 3800 V rms Vbc = 380120 V rms Vca = 380120 V rms One phase current is IA =
The other phase currents are Va 22030 = = 14.67  83.1 A rms Z 9 + j12 I B = 14.67  203.1 A rms and I C = 14.6736.9 A rms 1222 1223 Section 127: Balanced ThreePhase Circuits P12.71 Va =
25 103 0 Vrms 3 IA 25 103 0 Va = = 3 = 96  25 A rms Z 150 25 25 103 96 cos(0  25) = 3.77 mW P = 3 Va I A cos ( v  I ) = 3 3 P12.72 Convert the delta load to an equivalent Y connected load:
^ Z Z Y = 50 3 To get the perphase equivalent circuit shown to the right: The phase voltage of the source is Z = 50 Va = 45103 0 = 260 kV rms 3 The equivalent impedance of the load together with the line is 50 3 + 2 = 12 + j 5 = 1322.6 Z eq = 50 10 + j 20 + 3 (10 + j 20 ) The line current is aA = Va 26 103 0 = = 2000  22.6 A rms Z eq 1322.6 The power delivered to the parallel loads (per phase) is 50 (10 + j 20 ) 3 2 PLoads = I aA Re = 4 106 10 = 40 MW 50 10 + j 20 + 3 The power lost in the line (per phase) is 1224 PLine = I aA Re {Z Line } = 4 106 2 = 8 MW
2 The percentage of the total power lost in the line is
PLine 8 100% = 100% = 16.7% PLoad + PLine 40 +8 P12.73 Ia = Va 530 = = 0.5  23 A I a = 0.5 A Z T 6 + j8
I = 3 a Re {Z Load } = 3 0.125 4 = 1.5 W 2
2 PLoad also (but not required) :
PSource = 3 Pline (5) (0.5) cos(30  23) = 2.25 W 2
2 I = 3 a Re{Z Line } = 30.125 2 = 0.75 W 2 1225 Section 128: Power in a Balanced Load P12.81 Assuming the abc phase sequence: VCB = 20815 V rms VBC = 208195 V rms VAB = 208315 V rms Then VA = also VAB 208315 208 = = 285 V rms 330 330 3 I B = 3110 A rms I A = 3230 A rms
Finally P = 3 VAB I A cos ( V  I ) = 3( 208 ) (3) cos(285  230) = 620 W 3 P12.82 Assuming a lagging power factor:
cos = pf = 0.8 = 36.9 The power supplied by the threephase source is given by Pin = Pout = 20 ( 745.7 ) = 17.55 kW where 1 hp = 745.7 W 0.85 Pin 17.55 103 IA = = = 26.4 A rms 3 VA pf 480 3 ( 0.8 ) 3 Pin = 3 I A VA pf 480 I A = 26.4  36.9 A rms when VA = 0 V rms 3 1226 P12.83 (a) For a connected load, Eqn 12.85 gives PT 1500 = = 4.92 A rms 3 VP I L pf 3( 220 )(.8) 3 The phase current in the connected load is given by PT = 3 VP I L pf I L = I IL 4.92 IP = L = = 2.84 A rms 3 3 3 The phase impedance is determined as: IP =
Z= V 220 VL VL = ( V  I ) = L cos 1 pf = cos 1 0.8 = 77.4436.9 IP IP IP 2.84 (b) For a connected load, Eqn 12.84 gives PT = 3 VP I L pf I L = The phase impedance is determined as: 220 VP VP V Z= P = ( V  I ) = cos 1 pf = 3 cos 1 0.8 = 25.836.9 IP IP IP 4.92 PT 1500 = = 4.92 A rms 3 VP I L pf 3( 220 )(.8) 3 P12.84 Parallel loads Z1Z 2 (4030 ) (5060 ) Z = = = 31.2 8.7 1 + 2 4030 + 50 60 VL = VP , P = VP 600 = = 19.2 A rms, Z 31.2 IL = 3 P = 33.3 A rms So P = 3 VL I L pf = 3 (600) (33.3) cos (  8.7 ) = 34.2 kW 1227 P12.85 We will use In our case: S = S = S cos + S sin = S pf + S sin ( cos 1 pf ) S1 = 39 (0.7) + j 39 sin ( cos 1 ( 0.7 ) ) = 27.3 + j 27.85 kVA S 2 = 15 + 15 sin ( cos 1 ( 0.21) ) = 15  j 69.84 kVA 0.21 S S3 = S1 + S 2 = 42.3  j 42.0 kVA S = 3 = 14.1 j 14.0 kVA 3 The line current is S (14100+ j 14000) S = Vp I L I L = = = 117.5 + j 116.7 A rms = 167 45 A rms V 208 p 3 208 0 = 1200 V rms. The source must The phase voltage at the load is required to be 3 provide this voltage plus the voltage dropped across the line, therefore
* * VS = 1200 + (0.038 + j 0.072)(117.5 + j 116.7) = 115.9 + j 12.9 = 116.6 6.4 V rms
Finally VS = 116.6 V rms P12.86 The required phase voltage at the load is VP = 4.16 0 = 2.4020 kVrms . 3 Let I1 be the line current required by the connected load. The apparent power per phase 500 kVA required by the connected load is S1 = = 167 kVA . Then 3 S1 = S1 = S1 cos 1 ( pf ) = 167 cos1 ( 0.85) = 16731.8 kVA
and
* 3 S1 (167 10 ) 31.8 = 69.6  31.8 = 59  j36.56 A rms I1 = = 3 VP ( 2.402 10 ) 0 * S1 = VP I1 * 1228 Let I2 be the line current required by the first Yconnected load. The apparent power per phase 75 kVA required by this load is S 2 = = 25 kVA . Then, noticing the leading power factor, 3 S 2 = S 2 = S 2 cos 1 ( pf ) = 25 cos 1 ( 0 ) = 25  90 kVA
and S 2 = VP I 2
* * 3 S 2 ( 25 10 )  90 = 10.490 = j10.4 A rms I2 = = VP ( 2.402 103 ) 0 * Let I3 be the line current required by the other Yconnected load. Use Ohm's law to determine I3 to be 24020 24020 I3 = + = 16  j 10.7 A rms 150 j 225 The line current is I L = I1 + I 2 + I 3 = 75 j 36.8 A rms The phase voltage at the load is required to be VP = 4.16 0 = 2.4020 kVrms .The source 3 must provide this voltage plus the voltage dropped across the line, therefore VS = 24020 + (8.45 + j 3.9) (75  j 36.8) = 3179 0.3 Vrms
Finally VSL = 3 (3179) = 5506 Vrms P12.87 The required phase voltage at the load is VP = 4.16 0 = 2.4020 kVrms . 3 Let I1 be the line current required by the connected load. The apparent power per phase 1.5 MVA required by the connected load is S1 = = 0.5 MVA . Then 3 S1 = S1 = S1 cos 1 ( pf ) = 0.5 cos 1 ( 0.75) = 0.541.4 MVA
and S1 = VP I1
* * 6 S1 ( 0.5 10 ) 41.4 = 2081.6  41.4 = 1561.4  j1376.6 A rms I1 = = VP ( 2.402 103 ) 0 * 1229 Let I2 be the line current required by the first Yconnected load. The complex power, per phase, is 0.67 S 2 = 0.67 + sin ( cos 1 ( 0.8 ) ) = 0.67 + j 0.5 MVA 0.8
* 6 S 2 ( 0.67 + j 0.5 ) 106 ( 0.833 10 )  36.9 = I2 = = 3 3 VP ( 2.402 10 ) 0 ( 2.402 10 ) 0 = 346.9  36.9 = 277.4  j 208.3 A rms The line current is I L = I1 + I 2 = 433.7  j 345.9 = 554.7  38.6 A rms * * The phase voltage at the load is required to be VP = 4.16 0 = 2.4020 kVrms .The source 3 must provide this voltage plus the voltage dropped across the line, therefore VS = 24020 + (0.4 + j 0.8) (433.7  j 345.9) = 2859.6  38.6 Vrms
Finally VSL = 3 (2859.6) = 4953 Vrms The power supplied by the source is PS = 3 (4953) (554.7) cos (4.2 + 38.6 ) = 3.49 MW The power lost in the line is PLine = 3 ( 554.7 2 ) Re {0.4+ j 0.8} = 0.369 MW
The percentage of the power consumed by the loads is 3.49  0.369 100% = 89.4% 3.49 1230 P12.88 The required phase voltage at the load is VP = 600 0 = 346.40 Vrms . 3 = cos 1 (0.8) = 37 Let I be the line current required by the load. The complex power, per phase, is
S = 160 + 160 sin ( cos 1 ( 0.8 ) ) = 160 + j 120 kVA 0.8
* The line current is S (160 + j 120 ) 103 I= = = 461.9  j 346.4 A rms 346.40 VP * 600 0 = 346.40 Vrms .The source 3 must provide this voltage plus the voltage dropped across the line, therefore The phase voltage at the load is required to be VP = VS = 346.40 + (0.005 + j 0.025) (461.9  j 346.4) = 357.5 1.6 Vrms
Finally VSL = 3 (357.5) = 619.2 Vrms The power factor of the source is pf = cos ( V  I ) = cos (1.6  (  37)) = 0.78 1231 Section 129: TwoWattmeter Power Measurement P12.91
W = 14920 W hp P 14920 Pin = out = = 20 kW 0.746 Pout = 20 hp 746 Pin = 3 VL I L cos cos = Pin 20 103 = = 0.50 3 VL I L 3 (440) (52.5) cos 1 ( 0.5 ) = 60 The powers read by the two wattmeters are
P = VL I L cos ( + 30 ) = (440) (52.5)cos ( 60 + 30 ) = 0 1 and P2 = VL I L cos (  30 ) = (440) (52.5)cos ( 60  30 ) = 20 kW P12.92
VP = VL = 4000 V rms IP = VP 4000 = = 80 A rms Z 50 Z = 40 + j 30 = 50 36.9 L = 3 I P = 138.6 A rms pf = cos = cos (36.9 ) = 0.80 P1 = VL I L cos ( + 30 ) = 4000 (138.6) cos 66.9 = 217.5 kW P2 = VL I L cos ( 30 ) = 4000 (138.6) cos 6.9 = 550.4 kW PT = P1 + P2 = 767.9 kW Check : PT = 3 L VL cos = 3 (4000) (138.6) cos 36.9 = 768 kW which checks 1232 P12.93 Vp = Vp = 200 = 115.47 Vrms 3 VA =115.470 V rms, VB = 115.47120 V rms and VC = 115.47120 V rms IA = VA 115.470 = = 1.633  45 A rms Z 70.745 I B = 1.633  165 A rms and I C = 1.633 75 A rms
PT = 3 VL I L cos = 3 (200) (1.633) cos 45 = 400 W PB = VAC I A cos 1 = 200 (1.633) cos (45  30 ) = 315.47 W PC = VBC I B cos 2 = 200 (1.633) cos (45 + 30 ) = 84.53 W P12.94 ZY = 10  30 and Z = 1530 Convert Z to Z Y Z Y = ^ ^ then Zeq = Z = 530 3 1030+530 208 Vp = Vp = = 120 V rms 3
VA = 1200 V rms I A = (1030 ) ( 530 ) = 500 = 3.7810.9 13.228 10.9 1200 = 31.75 10.9 3.78 10.9 I B = 31.75130.9 I C = 31.75109.1 PT = 3VL I L cos = 3 ( 208 ) ( 31.75 ) cos (10.9 ) =11.23 kW W1 = VL I L cos ( 30) = 6.24 kW W2 = VL I L cos ( + 30) = 4.99 kW 1233 P12.95 PT = PA + PC = 920 + 460 = 1380 W tan = 3 ( 460 ) = 0.577 = 30 PA  PC = 3 1380 PA + PC
1380 PT = =7.67 A rms 3 VL cos 2 120cos( 30 ) 120 = 27.1 r Z = 27.1 30 4.43 PT = 3 VL I L cos so I L = IP = IL = 4.43 A rms 3 Z = P12.96 Z = 0.868 + j 4.924 = 580 VL = 380 V rms, VP = I L = I P and I P = = 80 380 = 219.4 V rms 3 VP = 43.9 A rms Z P = ( 380 ) ( 43.9 ) cos ( 30 ) = 10,723 W 1 P2 = ( 380 ) ( 43.9 ) cos ( + 30 ) = 5706 W PT = P + P2 = 5017 W 1 1234 PSpice Problems
SP 121 FREQ 6.000E+01 FREQ 6.000E+01 FREQ 6.000E+01 FREQ 6.000E+01 IM(V_PRINT3)IP(V_PRINT3)IR(V_PRINT3)II(V_PRINT3) 3.142E+00 1.644E+02 3.027E+00 8.436E01 IM(V_PRINT1)IP(V_PRINT1)IR(V_PRINT1)II(V_PRINT1) 3.142E+00 4.443E+01 2.244E+00 2.200E+00 VM(N01496) 2.045E14 VP(N01496) 2.211E+01 VR(N01496) 1.895E14 VI(N01496) 7.698E15 IM(V_PRINT2)IP(V_PRINT2)IR(V_PRINT2)II(V_PRINT2) 3.142E+00 7.557E+01 7.829E01 3.043E+00 3.1422 20 = 98.7 W 2 3.1422 I B = 3.14275.57 A and RB = 20 PB = 20 = 98.7 W 2 3.1422 I C = 3.142  164.4 A and RC = 20 PC = 20 = 98.7 W 2
I A = 3.142  43.43 A and RA = 20 PA = P = 3 ( 98.7 ) = 696.1 W 1235 SP 122 FREQ 6.000E+01 FREQ 6.000E+01 FREQ 6.000E+01 FREQ 6.000E+01 IM(V_PRINT3)IP(V_PRINT3)IR(V_PRINT3)II(V_PRINT3) 1.612E+00 1.336E+02 1.111E+00 1.168E+00 IM(V_PRINT1)IP(V_PRINT1)IR(V_PRINT1)II(V_PRINT1) 2.537E+00 3.748E+01 2.013E+00 1.544E+00 VM(N01496) VP(N01496) 1.215E+01 1.439E+01 VR(N01496) VI(N01496) 1.177E+01 3.018E+00 IM(V_PRINT2)IP(V_PRINT2)IR(V_PRINT2)II(V_PRINT2) 2.858E+00 1.084E+02 9.023E01 2.712E+00 I A = 2.537  37.48 A and 2.537 2 20 = 64.4 W 2 2.8582 I B = 2.858108.4 A and RB = 30 PB = 30 = 122.5 W 2 1.6122 I C = 1.612  133.6 A and RC = 600 PC = 60 = 78 W 2
RA = 20 PA = P = 64.4 + 122.5 + 78 = 264.7 V 1236 Verification Problems
VP 121
416 = 240 V = VA 3 Z = 10 + j4 = 10.77 21.8 VA = VA 240 = = 22.28 A rms 38.63 A rms Z 10.77 38.63 = 22.3 . It appears that the linetoline voltage was The report is not correct. (Notice that 3 mistakenly used in place of the phase voltage.) IA = VP 122
VL = VP = 2400 Vrms Z = 40 + j 30 = 50 36.9 IP = VP 2400 = = 4.8 36.9 A rms Z 5036.9 The result is correct. Design Problems
DP 121
P = 400 W per phase, 0.94 = pf = cos 400 = = cos1 ( 0.94 ) =20 208 I L 0.94 I L = 3.5 A rms 3 I I = L = 2.04 A rms 3 V 208 = 101.8 Z = L = 2.04 I Z = 101.8 20 1237 DP 122 VL = 240 V rms PA = VL I L cos (30 + ) = 1440 W PC = VL I L cos (30  ) = 0 W then 1440 = 240 I L cos (30 ) IL
= IP = 30 = 90 or = 60 I L = 6.93 A rms VP Z 240 V Z = P = 3 = 20 IP 6.93 Finally, Z = 20  60 DP 123
Pin = Pout 100 hp (746 = 0.8 W ) hp = 93.2 kW, P = Pin = 31.07 kW 3 VL = 480 V rms, pfc = 0.9 and pf = 0.75. We need the impedance of the load so that we can use Eqn 11.67 to calculate the value of capacitance needed to correct the power factor.
0.75 = pf = cos 31070 = = cos1 ( 0.75) = 41.4 480 I P 0.75 I P = 149.5 A rms 3 480 VP 3 = 1.85 Z = = IP 149.5 Z = 1.85 41.4 = 1.388 + j1.223 The capacitance required to correct the power factor is given by tan (cos 1 0.75)  tan (cos 1 0.9) 1.365 = 434 F C= 2 2 1.365 +1.204 377 (Checked using LNAPAC 6/12/03) 1238 DP 124
VL = 40 kV rms Try n2 = 25 then V2 = n2 25 VL = 40000 = 1000 kVrms n1 1 VL 41030 = 30 kA rms = IL = 4 ZL 3 30000 The line current in 2.5 is I = = 1200 A rms 25 Thus V1 = ( R + j X ) I + V2 = (2.5 + j 40) (1200) + 100103 = 100.4 2.7 kV Step need : n1 = Ploss = I =
2 100.4 kV = 5.02 5 20 kV
2 R = 120 (2.5) = 36 kW, P = (4103 ) (3 103 ) = 12 MW 12  .036 100% = 99.7 % of the power supplied by the source 12 is delivered to the load. 1239 Chapter 13: Frequency Response
Exercises
Ex. 13.31 H ( ) = gain = Vo ( ) 1 = Vs ( ) 1 + j C R 1 1 + ( C R) 2 phase shift =  tan 1 C R 1 When R = 104 , = 100, and C = 106 , then gain = = 0.707 and phase shift =  45o 2 Ex. 13.32 H ( ) =
gain = Vo ( ) R = Vs ( ) R + j L
R R 2 + ( L) 2 0.6 = 30 30 + (2 ) 2
2 30 2  30 .6 = = 20 rad s 2 2 Ex. 13.33 H ( ) = gain = I ( ) 1 = R + j L Vs ( ) 1 R 2 + ( L) 2 phase shift =  tan 1 L
R When R = 30 , L = 2 H, and = 20 rad/s, then
gain = 1 30 + 40
2 2 = 0.02 A 40 and phase shift =  tan 1 =  53.1 V 30 131 Ex. 13.34 H ( ) = Vo ( ) 1 = Vs ( ) 1 + j C R gain = 1 1 + ( C R) 2 phase shift =  tan 1 C R 45 =  tan 1 (20 106 R )
Ex. 13.35 H ( ) = Vo ( ) 1 = 1 + j C R Vs ( ) R= tan (45 ) = 50 103 6 2010 gain = 1 1 + ( C R) 2 , C , and R are all positive, or at least nonnegative, so gain 1. These specifications cannot be met. Ex. 13.41 (a) dB = 20 log (.5) = 6.02 dB (b) dB = 20 log 2 = 6.02 dB Ex. 13.42 1 20 log H = 20 log 2 = 20 log ( )2 = 40 log slope = 20 log H ( 2 )  20 log H (1 ) = 40 log 2 + 40 log 1 = 40 log 2 1 let 2 = 10 1 to consider 1 decade, then slope =  40 log10 =  40 dB decade 132 Ex. 13.43 When C >> B, H ( )  (d ) (b) j A A = j C C A H ( ) in dB = 20 log10 H ( ) = 20 log10 C H ( ) does not depend on so slope = 0 j A A = j B B When C << B, H ( )  A H ( ) in dB = 20 log10 H ( ) = 20 log10 +20 log10 B (c) The slope is the coefficient of 20 log10 , that is, slope = 20 dB decade B (a) The break frequency is the frequency at which C = B, that is, = C Ex. 13.44 R Vo ( ) = 1+ 1 Vc ( ) R2 R 1 = 1+ 1 Vs ( ) R2 1 + j C R H ( ) = Vo ( ) R1 1 =1+ Vs ( ) R2 1+ j C R When R C = 0.1 and then H ( ) = 4 1+j R1 = 3, R2 10 133 Ex. 13.45 a)
Zo = R2 + 1 j C R2 + 1 1+ j Vo Zo 1 j C = = = 1 R1 + Z o Vs R1 + R2 + 1+j j C 2
where 1 = and 2 =
vs ( t ) = 10 cos 20 t or Vs = 100 1+ j 20 Vo 16.7 = 20 Vs 1+ j 5.56 1+ j 1.20 = = 0.417  24.3 1+ j 3.60 b) So
Vo = 4.17  24.3 vo (t ) = 4.17 cos(20t  24.3) V 1 R2 C = 16.7 rad/s 1 = 5.56 rad/s ( R1 + R2 )C ( ( ) ) 134 Ex. 13.46 Ex. 13.51 a) Q o RC = R C b) BW = 2.5 107 = 8000 = 20 L 40 103
1 1 = = 500 rad s 3 7 Q LC 20 (4010 ) (2.510 ) o
Q = Ex. 13.52 Q= 0 BW 7 = 10 2 105 = 50 1 Now o = 1 LC L = o C 2 = 1 = 1 mH (10 ) (10 1012 )
7 2 Ex. 13.53 o = 1
Q = LC BW =
4 = 10 1 (103 )(105 ) 2 (15.9)
1 2 = 104 rad s o = 100 (104 )(103 ) R= = = 0.1 Q 100 o L 135 Ex. 13.54 a) o = 1 Q= o LC BW BW 1 C = = 1 1 (106 ) 2 (0.01) BW = 100 pF b) Q =
H= o o RC R = 2 o
103 = = 1000 103 = = 10 (106 ) 2 (1010 ) C 6 = 10 1 1.05106 106  1+ j 1000 6 1.05104 10 1+ j Q  o o 1 1+ j 97.6 H= 136 Problems
Section 133: Gain, Phase Shift, and the Network Function P13.31 R 2  1 j C = R2 1 + j C R 2 R2 1 + j C R 2 R2 R1 + 1 + j C R 2 R2 R1 + R 2 1 + j C R p H ( ) = Vo ( ) = Vi ( ) = When R1 = 40 W, R2 = 10 W and C = 0.5 F where Rp = R1  R2. 0.2 1 + j 4 (checked using ELab on 8/6/02) H ( ) = P13.32 H ( ) = Vo ( ) j C = Vi ( ) R + R + 1 1 2 j C 1 + j C R 2 = 1 + j C R1 + R 2
R2 + 1 ( ) When R1 = 40 kW, R2 = 160 kW and C = 0.025 F H ( ) = 1 + j ( 0.004 ) 1 + j ( 0.005 ) (checked using ELab on 8/6/02) 137 P13.33
H ( ) = R2 Vo ( ) = Vi ( ) R1 + R 2 + j L R2 = R1 + R 2 L 1 + j R1 + R 2 When R1 = 4 W, R2 = 6 W and L = 8 H
H ( ) = 0.6 1 + j ( 0.8 ) (checked using ELab on 8/6/02) P13.34
H ( ) = R 2 + j L Vo ( ) = Vi ( ) R + R 2 + j L L 1 + j R R2 2 = R + R2 L 1 + j R + R2 Comparing the given and derived network functions, we require R2 = 0.6 R + R2 R 2 = 12 L R + R2 = 20 L L 1 + j R R2 2 R + R2 L 1 + j R + R2 1+ = ( 0.6 ) 1+ j j 12 20 Since R2 = 60 W, we have L = 60 = 5 H , then R = ( 20 )( 5 )  60 = 40 . 12 (checked using ELab on 8/6/02) 138 P13.35 R 2  1 j C = R2 1 + j C R 2 R2 1 + j C R 2 R2 R+ 1 + j C R 2 R2 R + R2 1 + j C R p H ( ) = Vo ( ) = Vi ( ) = where Rp = R  R2. Comparing the given and derived network functions, we require
R2 0.2 = 1 + j C R p 1 + j 4 R + R2 R2 = 0.2 R + R2 CR =4 p Since R2 = 2 W, we have Finally, C = 4 = 2.5 F . 1.6 ( 2 )(8 ) = 1.6 . 2 = 0.2 R = 8 . Then R p = R+2 2+8
(checked using ELab on 8/6/02) P13.36 Vi ( ) R + j L 1 Vo ( ) = ( A I a ( ) ) j C I a ( ) = A Vo ( ) CR = L Vi ( ) ( j ) 1 + j R 139 When R = 20 W, L = 4 H, A = 3 A/A and C = 0.25 F H ( ) = 0.6 ( j ) (1 + j ( 0.2 ) ) (checked using LNAP on 12/29/02) P13.37 In the frequency domain, use voltage division on the left side of the circuit to get: 1 1 j C VC ( ) = Vi ( ) = Vi ( ) 1 1 + j C R1 R1 + j C Next, use voltage division on the right side of the circuit to get: 2 A R3 2 3 Vo ( ) = A VC ( ) = A VC ( ) = Vi ( ) R 2 + R3 3 1 + j C R1 Compare the specified network function to the calculated network function: 2 2 A A 2 1 3 3 = = 4 = A and = 2000 C 1 + j C R1 1 + j C 2000 3 100 1+ j 100 4 Thus, C = 5 F and A = 6 V/V. (checked using ELab on 8/6/02) 1310 P13.38 H ( ) = Vo ( ) = Vi ( )
R2 1 j C R1 R2  R1 = 1+ j C R2
When R 1 = 10 k, R 2 = 50 k , and C = 2 F, then R2 R1
= 5 and R2 C = 1 5 so H ( ) = 10 1+ j 10 P13.39 H ( ) = Vo ( ) = Vi ( )
R2 R1 1 j C2 1 j C1 R2 1 + j C2 R2 =  R1 1 + j C1R1 R 1 + j C1R1 H ( ) =  2 R1 1 + j C2 R2 When R1 = 10 k, R2 = 50 k , C1 = 4 F and C2 = 2 F, then so R2 R1 = 5 , C1R1 = 1 1 and C2 R 2 = 25 10 1 + j 25 H ( ) =  5 1+ j 10 1311 gain = H( ) = ( 5 ) 1+ 1+ 2
625 2
100 phase shift = ( ) = 180 + tan 1  tan 1 25 10 P13.310
R3 1 = j C 1 R1 j C = 1 1 + j C R3 R3 + j C R3 R3 1+ j C R3 R + R + j R2 R3C = 2 3 R1 R1 + j R1 R3C R2 + R3 R1 R2 R2 = 2 R1 = 20 k R1 H ( ) =  R2 + 5 = lim H ( ) = 0 2 = lim H ( ) = then R3 = 5 R1  R2 = 30 k P13.311 H ( ) = 
R2 + 1 j C = 1 + j C R 2 j C R1 R1 H ( ) = 180 + tan 1 C R 2  90 H ( ) = 135 tan 1 CR2 = 45 C R 2 = 1 R2 = 10 = lim H ( ) = 1 = 10 k 10 107
3 R2 R R1 = 2 = 1 k R1 10 1312 P13.312 H ( ) = R2 j C R 2 =  1 1+ j C R1 j C R 10 = lim H( ) = 2 R2 = 10 R1 R1 tan (270 H( )) = 104 tan(270H( )) = 104 = 10 k C H( ) = 180+90 tan 1 C R1 R1 = R2 = 100 k
P13.313
1 j C2 V ( ) = H ( ) = o 1 Vs ( ) R1 + j C1 R2 = ( C1R2 ) j (1 + j R1C1 ) (1 + j R2C2 ) When R1 = 5 k, C1 = 1 F, R2 = 10 k and C2 = 0.1 F, then H ( ) = so ( 0.01) j 1 + j 1 + j 200 1000 H ( ) 0 1.66 0.74 H ( ) 90 175 116 0 500 2500 Then v ( t ) = (0) 50 + (1.66) ( 30 ) cos(500t + 115 + 175)  (0.74) ( 20 ) cos(2500t + 30 + 116) o =49.8cos(500t  70) 14.8cos (2500t +146) mV When R1 =5 k, C1 =1 F, R 2 =10 k and C2 = 0.01 F, then 1313 H ( )=  0.01 j 1+ j 1+ j 200 10,000 So 0 500 2500 Then H ( ) 0 1.855 1.934 H ( ) 90 161 170 v (t ) = (0) ( 50 ) + (1.855) ( 30 ) cos(500t + 115  161)  (1.934) ( 20 ) cos(2500t + 30 + 170) o = 55.65 cos(500t  46)  38.68cos(2500t + 190) mV P13.314 a) 2 V (8 div) div = 8 V Vs = 2 2 V (6.2 div) div = 6.2 V Vo = 2 V 6.2 gain = o = = 0.775 8 Vs 1 b) H ( ) = Vo ( ) 1 j C = = 1 Vs ( ) 1 + j C R R+ j C
1 1 1 g
2 1 Let g = H ( ) = then C = R 1 + 2C 2 R 2
In this case = 2 500 = 3142 rad s , H ( ) = 0.775 and R = 1000 so C = 0.26 F. c) tan(  H ( )) RC Recalling that R = 1000 and C=0.26F, we calculate H ( )=  tan 1 R C so = 1314 2 (200) 2 (2000) H ( ) 0.95 0.26 H ( ) 18 73 tan  45 = 3846 rad s H ( )=  45 requires = 1000 .26106 ( ) ( ( ) ) ( ) = 135 requires = tan ( (135)) =  3846 rad s (1000)(0.26106 ) A negative frequency is not acceptable. We conclude that this circuit cannot produce a phase shift equal to 135 . d) tan ((60 )) = 0.55 F C= (2 500) (1000) tan (H ( )) C= R C = tan ((300 )) = 0.55 F (2 500 ) (1000) A negative value of capacitance is not acceptable and indicates that this circuit cannot be designed to produce a phase shift at 300 at a frequency of 500 Hz. e) tan(  (120 )) C = = 0.55 F (2 500)(100) This circuit cannot be designed to produce a phase shift of 120 at 500 Hz. 1315 Section 134: Bode Plots P13.41 20 20 j 5 20 j 5 = 200 j 50 <5 20 1 + j 5 H ( )= 1 + j 50 5 < < 50 50 < P13.42 H1 ( ) = 1+ j 1+ j 50 5 H 2 ( ) = 10 1+ j 1+ j 50 5 Both H1() and H2() have a pole at = 50 rad/s and a zero at = 5 rad/s. The slopes of both magnitude Bode plots increase by 20 dB/decade at = 5 rad/s and decrease by 20 dB/decade at = 50rad/s. The difference is that for < 5rad/s
H1 ( ) 1 = 0 dB and H 2 ( ) 10 = 20 dB 1316 P13.43 R2 j 1+ j C2 R2 H ( ) =  = C1 R2 1 (1+ j R1C1 )(1+ j R2C2 ) R1 + j C1 This network function has poles at p1 = so (C R ) j 1 2 j R = 2 =2 (C1 R2 ) j C1 R1 R1 1 j = (C1 R2 ) ( j C1 R1 )( j C2 R2 ) j C2 R1 1 1 = 2000 rad s and p2 = = 1000 rad s R1C1 R2C2 < p1
p1 < < p2 H ( ) > p2 1317 P13.44 R2 R (1+ j C1 R1 ) R 1 1 1+ j C2 R2 H ( ) =  = 2 so K =  2 , z = and p = R1 R1 (1+ j C2 R2 ) R1 C1 R1 C2 R2 1+ j C1 R1 When z < p When z > p P13.45 Using voltage division twice gives: V2 ( ) = Vi ( ) and Vo ( ) = V2 ( ) R4 A R4 R 3 + j C R 4 A R4 R3 + R 4 A= = R4 C R3 R 4 R3 + R 4 + j C R3 R 4 R3 + 1 + j R 3 + j C R 4 R3 + R 4 j L R 2 R 2 + j L j L R 2 L j = = j L R 2 R1 R 2 + j L ( R1 + R 2 ) R1 L ( R1 + R 2 ) R1 + 1 + j R 2 + j L R1 R 2 Combining these equations gives 1318 H ( ) = ALR 4 Vo ( ) j = Vi ( ) R1 ( R 3 + R 4 ) L ( R1 + R 2 ) CR 3 R 4 1 + j 1 + j R1 R 2 R3 + R 4 The Bode plot corresponds to the network function:
H ( ) = k j k j = 1 + j 1 + j 1 + j 200 1 + j 20000 p1 p2 k j = k j 1 1 k j H ( ) = k p1 j 1 p1 k j k p1 p2 = j j j p p 1 2 p1
p1 p2 p2 This equation indicates that H()=k p1 when p1 p2. The Bode plot indicates that H()=20 dB = 10 when p1 p2. Consequently k= Finally, 10 10 = = 0.05 p1 200 H ( ) = 0.05 j 1 + j 1 + j 200 20000 Comparing the equation for H() obtained from the circuit to the equation for H()obtained from the Bode plot gives: 0.05 = R1 ( R 3 + R 4 ) ALR 4 , 200 = L ( R1 + R 2 ) R1 R 2 and 20000 = R3 + R 4 C R3 R 4 Pick L = 1 H, and R1 = R2 , then R1 = R2 = 400 . Let C = 0.1 F and R3 = R4 , then R3 = R4 = 1000 . Finally, A=40. (Checked using ELab 3/5/01) 1319 P13.46 From Table 13.42:
R2 R1 = k = 32 dB = 40 R 2 = 40 (10 103 ) = 400 k 1 1 = p = 400 rad/s C 2 = = 6.25 nF C 2 R2 ( 400 ) ( 400 103 ) 1 1 = z = 4000 rad/s C 1 = = 25 nF C 1 R1 ( 4000 ) (10 103 ) P13.47
H ( ) = R 2 + j L Vo ( ) = Vi ( ) R + R 2 + j L L 1 + j R R2 2 = R + R2 L 1 + j R + R2 H ( ) = ( 0.2 ) (1 + j ( 0.25 ) ) 1 + j ( 0.05 ) k = 0.2 1 z= =4 0.25 1 p = 0.05 = 20 P13.48 The slope is 40dB/decade for low frequencies, so the numerator will include the factor (j)2 . The slope decreases by 40 dB/decade at = 0.7rad/sec. So there is a second order pole at 0 = 0.7 rad/s. The damping factor of this pole cannot be determined from the asymptotic Bode plot; call it 1. The denominator of the network function will contain the factor
1 + 2 1 j  0.7 0.7 2 The slope increases by 20 dB/decade at = 10 rad/s, indicating a zero at 10 rad/s. 1320 The slope decreases by 20 dB/decade at = 100 rad/s, indicating a pole at 100 rad/s. The slope decreases by 40 dB/decade at = 600 rad/s, indicating a second order pole at 0 = 600rad/s. The damping factor of this pole cannot be determined from an asymptotic Bode plot; call it 2. The denominator of the network function will contain the factor  1 + 2 2 j 600 600 K (1+ j 2 10 H ( ) = )( j ) 2 2 2   1+ 21 j 1+ 2 2 j 1+ j 0.7 0.7 600 600 100 To determine K , notice that H ( ) = 0 dB=1
1= K (1)( j ) 2  (1)(1) 0.7 2 when 0.7 < < 10. That is = K (0.7) 2 K = 2 P13.49 (a) K 1+ j z H ( ) = j
H ( ) = K 1+ z K 2 H ( ) dB = 20 log10 1+ z 2 = 20 log10 K  20 log10 + 20 log10 Let H L ( ) dB = 20 log10 K  20 log10 K z H ( ) dB _ L Then H ( ) dB ~ H H ( ) dB 1+ z 2 and H H ( ) dB = 20 log10 < < z >z > 1321 So H L ( ) dB and H H ( ) dB are the required low and highfrequency asymptotes. The Bode plot will be within 1% of H() dB both for << z and for >> z. The range when << z is characterized by H L ( ) = 0.99 H ( ) or equivalently
20 log10 ( 0.99 ) = H L ( ) dB  H ( ) dB = 20 log10 K  20 log10  20 log10 =  20 log10 1+ = 20 log10 z
2 (gains not in dB) (gains in dB) 1+ z K 1 1+ z
2 2 Therefore
0.99 = 1 1+ z
2 z 1 = z 1 = 0.14 z  7 .99 2 The range when >> z is characterized by
H H ( ) = .99 H ( )
(gains not in dB) or equivalently 1322 20 log10 0.99 = H H ( ) dB  H ( ) dB (gains in dB) K
2 = 20 log10 K  20 log10 z  20 log10 1+ z 1 =  20 log10 1+ = 20 log10 2 z z +1 z
2 Therefore 1 = 1 .99 z 2 = z 1 1 .99 2 = z  7z 0.14 The error is less than 1% when < z and when > 7z. 7 P13.410 H ( ) = V0 ( ) = Vs ( ) Rt R t + R1 1 j C = Rt + Rt R1 1+ j C R1 1+ j C R1 1+ j C R1 R t R1 + R t = Rt = R1 + R t + j C R1 R t R1 + R t R t (1+ j C R1 ) When R1 = 1 k, C = 1 F and R t = 5 k 1+ j 1000 5 H ( ) = 6 1+ j 1200 5 <1000 6 5 1000< <1200 H ( ) j 6 1000 1 <1200 1323 P13.411 Mesh equations:
Vin ( ) = I ( ) [ R1 + ( j L1  j M ) + ( j M + j L2 ) + R2 ] Vo ( ) = I ( ) [( j M + j L2 ) + R2 ] Solving yields:
H ( ) = V0 ( ) R2 + j ( L2  M ) = Vin ( ) R1 + R2 + j ( L1 + L2  2M ) Comparing to the given Bode plot yields:
lim K1 = H ( ) = z = L2  M R2 = 0.75 and K 2 = lim  H ( )  = = 0.2 0 L1 + L2  2 M R1 + R2 R2 R1 + R2 = 333 rad s and p = =1250 rad s L2  M L1 + L2  2 M 1324 P13.412 1 1+ j R1 C1 1 (1+ j R1 C1 ) j C2 H ( ) =  = = j R1 C2 R1 C2 j 1 R1 j C1 1 1  R C j H ( )  1 2  1 ( R C ) =  C1 R1 C2 1 1 C2 < > 1 R1 C1 1 R1 C1 With the given values: C1 1 = = 6 dB, C2 2 1 = 4000 rad / s R1 C1 1325 P13.413 Pick the appropriate circuit from Table 13.42. We require
200 = z = 1 1 p C , 500 = p = and 14 dB = 5 = k = 1 C 1 R1 C2 R 2 z C2 Pick C1 = 1 F, then C2 = 0.2 F, R1 = 5 k and R 2 = 10 k. P13.414 Pick the appropriate circuit from Table 13.42. We require 500 = p = R2 1 and 34 dB = 50 = C R2 R1 Pick C = 0.1 F, then R 2 = 20 k and R1 = 400 . 1326 P13.415 Pick the appropriate circuit from Table 13.42. We require
500 = z = 1 1 p C , 200 = p = and 14 dB = 5 = k = 1 C 1 R1 C2 R 2 z C2 Pick C1 = 0.1 F, then C2 = 0.05 F, R1 = 20 k and R 2 = 100 k. 1327 P13.416 Pick the appropriate circuit from Table 13.42. We require
200 = p 1 = 1 1 , 200 = p 2 = and 34 dB = 50 = k = C 1 R 2 C 1 R1 C2 R 2 Pick C1 = 1 F, then C2 = 0.04 F, R1 = 5 k and R 2 = 50 k. P13.417 H ( ) = 10(1+ j 50) (1+ j 2)(1+ j 20)(1+ j 80) 1328 = H ( ) = tan 1 ( 50 )  ( tan 1 ( 2 ) + tan 1 ( 20 ) + tan 1 ( 80 ) ) P13.418 (a) H ( ) = Vo ( ) R2 R1 = Vs ( ) 1+ j R2C = 1+ j 10 10,000 (b) (c) 10 = 20 dB 10,000 rad/s 1329 P13.419 Vo (1 + j C 1 R1 )(1 + j C 2 R 2 ) = j C 1 R1Vo + Vs Va ( )  Vs ( ) 0= + j C 1 (Va ( )  Vo ( )) R1 1 j C 2 Vo ( ) = Va ( ) 1 R+ j C 2
T( ) = Vo ( ) 1 1 = = 2 2 Vs ( ) 1+ C 2 R 2 j  C 1C 2 R1 R 2  + 0.8 j +1 This is a second order transfer function with o = 0 and = 0.4 . 1330 Section 135: Resonant Circuits P13.51 0 = 1 1 = = 60 k rad sec LC 1 1 x 106 120 30 1 106 C = 10, 000 30 = 20 Q= R 1 L 120 2 2 + 0 + 0 = 58.52 k rad s and 2 = 0 + 0 + 0 = 61.52 k rad s 1 =  2Q 2Q 2Q 2Q 1 1 = = 3 krad s BW = RC 1 6 (10000 ) 10 30 Notice that BW = 2  1 = P13.52 0 2 2 0
Q . H ( ) = k 1+ Q  0 0 2 2 so R = k = H ( 0 ) = At = 897.6 rad s , H ( ) = 8 = 400 and 0 = 1000 rad s 20103 4 = 200, so 20.103 200 = 400 897.6 1000  1+ Q 2 1000 897.6 2 Q =8 Then 1 = 0 = 1000 LC C = 20 F L = 50 mH C =Q=8 400 L 1331 P13.53 0 = 1 1 L R = 105 rad s , Q = = 10, BW = = 104 rad s R C L LC P13.54 0 = 1 1 L R = 104 rad s , Q = = 10, BW = = 103 rad s R C L LC P13.55 R = Z ( 0 ) = 100 1 = BW = 500 C = 20 F 100 C 1 = 0 = 2500 L = 8 mH 20106 ) L ( P13.56
R=
Y ( 0 ) 1 = 100 100 = BW = 500 L = 0.2 H L 1 = 0 = 2500 C = 0.8 F ( 0.2 )C 1332 P13.57 Y ( ) = j C +
= 1 1 + R1 + j L R 2  2C L R 2 ) + j ( L +C R1 R 2 ) R1  j L R1  j L R 2 ( R1 + j L ) (R +R
1 2 = R1 ( R1 + R 2  2C L R 2 )  2 L( L +C R1 R 2 )+ j R1 ( L C R1 R 2 )  j L( R1 + R 2  2C L R 2 ) R 2 ( R1  2 L2 ) = 0 is the frequency at which the imaginary part of Y ( ) is zero :
R1 ( L C R1 R 2 )  L ( R1 + R 2  C L R 2 ) = 0
2 0 0 = L R 2 C R12 R 2 C L2 R 2 = 12.9 M rad sec 1333 P13.58 (a) Using voltage division yields Vo = 10000 ( 100 j100 ) (100)(  j100) + j100 100  j100 (100 )(  j100 ) 105 100 2 135 = 10000 = 2135 = 100090 V 100 2 135+ j100 50 2135 ( ) Vo  = 1000 V (b) Do a source transformation to obtain This is a resonant circuit with 0 = 1 LC = 400 rad/s. That's also the frequency of the input, so this circuit is being operated at resonance. At resonance the impedances of the capacitor and inductor cancel each other, leaving the impedance of the resistor. Increasing the resistance by a factor of 10 will increase the voltage Vo by a factor of 10. This increased voltage will cause increased currents in both the inductance and the capacitance, causing the sparks and smoke. 1334 P13.59 Let G 2 = 1 . Then R2
1 G 2 + j C G 2 + j C Z = R1 + j L + (R G =
1 2 + 1  2 L C ) + j ( LG 2 + C R1 ) At resonance, Z = 0 so
tan 1 L G2 + C R1 C = tan 1 2 G2 ( R1G 2 +1 L C )
and C > G 22 L so
C  L G 22 L G 2 + C R1 C 2 = = LC2 ( R1 G 2 +1 2 L C ) G 2
With R1 = R 2 = 1 and 0 = 100 rad s , 0 = 104 =
2 CL . Then choose C and calculate L: LC2 C = 10 mF L = 5 mH Since C > G 22 L , we are done. 1335 P13.510 (a)
R ( R  2 R L C )+ j L j C Z in = j L + = 1 1+ j R C R+ j C Consequently,  Zin  = ( R  2 R L C ) + ( L )
2 2 2 1+( R C ) (b) (c) = 1 LC  Zin  = 1 C R2 C 1 + L L
P13.511
Let V ( ) = A0 and V2 ( ) = B . Then I ( ) = Y ( ) = V ( ) V ( )  V2 ( ) A  B A  B cos  j B sin R = = AR AR V ( )  Y ( )  = ( A  B cos ) + ( B sin )
2 2 AR 1336 PSpice Problems
SP13.1 Here are the magnitude and phase frequency response plots: From the magnitude plot, the low frequency gain is k = 200m = 0.2. From the phase plot, the angle is 45 at p = 2 ( 39.891) = 251 rad/s . 1337 SP132 Here is the magnitude frequency response plot: The low frequency gain is 0.6 = lim H ( ) = k k = 0.6 . 0 The high frequency gain is 1 = lim H ( ) = k At = 2 ( 2.8157 ) = 17.69 rad/s , p z z = ( 0.6 ) p 17.69 1+ 0.6 p 0.8 = 0.6 2 17.69 1+ p 2 16 p 2 + 869 = 2 9 p + 313 16 2 p + 313 = p 2 + 869 9 ( ) ( 0.77778 ) p 2 = 312.56
p = 20 rad/s z = 12 rad/s 1338 SP133 From the magnitude plot, the low frequency gain is k = 4.0. From the phase plot, the angle is 45 at p = 2 (15.998 ) = 100.5 rad/s . 1339 SP134 From the magnitude plot, the low frequency gain is k = 5.0. From the phase plot, the angle is 18045=135 at p = 2 (1.5849 ) = 9.958 rad/s . 1340 SP135
104 104 R R H ( ) =  =  tan 1 ( C 104 ) 4 2 1 + j C 10 1 + ( C 104 ) When = 200 rad/sec = 31.83 Hertz
1.8565158 = 104 R  tan 1 ( C 104 ) 1 + ( C 10 4 2 ) Equating phase shifts gives C 104 = 103
Equating gains gives
1.8565 = C R 104 = tan(22) = 0.404 C = 0.2 F R + 104
104 R 104 R 1 + ( 0.404 )
2 1 + ( C 10 4 2 ) = R = 5 k SP136 104 104 C R 104 R + 104 R + 104 = =  tan 1 H ( ) = 4 2 104 C R 104 R + 10 C R 104 + R 1 + j 1 + 1 + j C 104 R + 104 4 R + 10 When = 1000 rad/sec = 159.1 Hertz 104 C R 104 R + 104  tan 1 0.171408  59 = 4 2 R + 10 C R 104 1+ 4 R + 10 Equating phase shifts gives C R 104 C R 104 = 103 = tan(59) = 1.665 R + 104 R + 104 Equating gains gives 104 1 + j C R 2 1341 0.171408 = 104 R + 104 C R 104 1+ 4 R + 10 2 = 104 R + 104 1 + (1.665 )
2 R = 20 k Substitute this value of R into the equation for phase shift to get: C ( 20 103 ) 104 C R 104 3 = 10 1.665 = 10 R + 104 ( 20 103 ) + 104
3 C = 0.25 F Verification Problems
VP131 When < 6300 rad/s, H() 0.1, which agrees with the tabulated values of  H() corresponding to = 200 and 400 rad/s. When > 6300 rad/s, H() 0.1, which agrees with the tabulated values of  H() corresponding to = 12600, 25000, 50000 and 100000 rad/s. At = 6300 rad/s, we expect  H() = 3 dB = 0.707. This agrees with the tabulated value of  H() corresponding to = 6310 rad/s. At = 630 rad/s, we expect  H() = 20 dB = 0.14. This agrees with the tabulated values of  H() corresponding to = 400 and 795 rad/s. This data does seem reasonable. VP132 BW = 0
Q = 10,000 = 143 71.4 rad s . Consequently, this report is not correct. 70 VP133 1 1 L R = 10 k rad s = 1.59 kHz, Q = = 20 and BW = = 500 rad s = 79.6 Hz R C L LC The reported results are correct. 0 = 1342 VP134 The network function indicates a zero at 200 rad/s and a pole at 800 rad/s. In contrast, the Bode plot indicates a pole at 200 rad/s and a zero at 800 rad/s. Consequently, the Bode plot and network function don't correspond to each other. Design Problems
DP131 Pick the appropriate circuit from Table 13.42. We require
2 1000 < z = R2 1 1 p C , 2 10000 > p = , 2=k = and 5 = k = 1 C 1 R1 C2 R 2 z C2 R1 Try z = 2 2000. Pick C1 = 0.05 F. Then
R1 = 1 C C = 1.592 k, R 2 = 2 R1 = 3.183 k and C2 = 1 = 1 = 0.01 F p 2 C1 z k z Check: p = 1 = 31.42 k rad s < 2 10, 000 rad s. C 2 R2 1343 DP132 1 V ( ) j C 1+ j C R LC H ( ) = o = = = R 1 1 Vs ( ) 1  2 + j +  R j L + j L + 1+ j C R RC LC j C  R 1 R Pick 1 = 0 = 2 (100 103 ) rad s . When = 0 LC 1 LC H 0 ( ) = 1 1 1 1  +j + LC LC RC LC So H ( 0 ) = R
C . We require L 3 dB = 0.707 = H ( 0 ) = R C C = 1000 L L Finally 1 = 2 (100103 ) LC C =1.13 nF C L = 2.26 mH 0.707 =1000 L 1344 DP133
R1 = 10 k R 2 = 866 k R 3 = 8.06 k R 4 = 1 M R 5 = 2.37 M R 6 = 499 k C 1 = 0.47 F C 2 = 0.1 F Circuit A Va =  R3 R2 Vc  R5 R3 R1 Vs = H 1 Vc  H 2 Vs Circuit B Vo =  R4 1 + j C 1 R 5 Va =  H 3 Va Circuit C Then Vc =  1 Vo = H 4 Vo j C 2 R 6 Vc = H 3 H 4 Va Va = H 2 Vs  H1 H 3 H 4 Va Vo = H 3 Va = Va = H 2 Vs 1 + H1 H 3 H 4 H 2 H3 Vs 1 + H1 H 3 H 4 After some algebra j
Vo = R3 R1 R 4 C 1  + j
2 R3 R 2 R 4 R 6 C1 C 2 R5 C1 Vs This MATLAB program plots the Bode plot:
R1=10; R2=866; R3=8.060; R4=1000; % units: kOhms and mF so RC has units of sec 1345 R5=2370; R6=449; C1=0.00047; C2=0.0001; pi=3.14159; fmin=5*10^5; fmax=2*10^6; f=logspace(log10(fmin),log10(fmax),200); w=2*pi*f; b1=R3/R1/R4/C1; a0=R3/R2/R4/R6/C1/C2; a1=R5/C1; for k=1:length(w) H(k)=(j*w(k)*b1)/(a0w(k)*w(k)+j+w(k)*a1); gain(k)=abs(H(k)); phase(k)=angle(H(k)); end subplot(2,1,1), semilogx(f, 20*log10(gain)) xlabel('Frequency, Hz'), ylabel('Gain, dB') title('Bode Plot') subplot(2,1,2), semilogx(f, phase*180/pi) xlabel('Frequency, Hz'), ylabel('Phase, deg') 1346 DP134 Pick the appropriate circuits from Table 13.42. We require
10 =  k1k2 = R 2C1 R4 R3 , 200 = p1 = 1 1 and 500 = p2 = R1 C 1 C 2 R4 Pick C 1 = 1 F. Then R1 = 1 1 = 5 k. Pick C 2 = 0.1 F. Then R 4 = = 20 k. p1 C1 p2C2 Next 10 =
Let R 2 = 500 k and R 3 = 1 k. R2 R3 (106 )(20 103 ) R2 R3 = 500 1347 DP135 Pick the appropriate circuits from Table 13.42. We require
20 dB = 10 =  k1k2 = R 2C1 R4 R3 , 0.1 = p1 = 1 1 and 100 = p2 = R1 C 1 C 2 R4 Pick C 1 = 20 F. Then R1 = 1 1 = 500 k. Pick C 2 = 1 F. Then R 4 = = 10 k. p1 C 1 p2C2 Next 10 =
Let R 2 = 200 k and R 3 = 4 k. R2 R3 (20 106 )(10 103 ) R2 R3 = 50 1348 DP136 1+ The network function of this circuit is H ( ) = R2 R3 1+ j R1C R3 R2 = R3 R2
2 The phase shift of this network function is =  tan 1 R1C 1+ The gain of this network function is G = H ( ) = 1+ 1+ ( R1C ) 2 1+ ( tan ) Design of this circuit proceeds as follows. Since the frequency and capacitance are known, R1 is tan( ) . Next pick R2 = 10k (a convenient value) and calculated R3 using calculated from R1 = C
R 3 = (G 1+ (tan ) 2  1) R 2 . Finally = 45 deg, G = 2, = 1000 rad s R1 = 10 k, R 2 = 10 k, R 3 = 18.284 k, C = 0.1 F DP137 From Table 13.42 and the Bode plot:
800 = z = 1 R1 = 2.5 k R1 (0.5106 ) 32 dB = 40 = 200 = p = (Check: 20 dB = 10 = k
DP138 R2 R1 R 2 = 100 k 1 1 C = = 0.05 F R2C (200)(100103 ) p 0.5106 0.5106 = = ) z C 0.05106 R2 j C R 2 =  1 1+ j C R1 1+ j C tan(270195) 195 = 180 + 90  tan 1 C R1 R1 = = 37.3 k (1000)(0.1106 ) R 10 = lim H ( ) = 2 R 2 = 10 R1 = 373 k R1 H ( ) = 1349 Chapter 14: The Laplace Transform
Exercises
Ex. 14.31 f ( t ) = cos t = e + j t + e  jt 1 and L e at = s a 2 1 1 1 s s  j + s + j = s 2 + 2 2 F ( s ) = L[cos t ] = Ex. 14.32
F ( s ) = L [e
2 t s2 + s + 3 1 1 e 2t + L [sin t ] = + sin t ] = L + = s + 2 s 2 +1 ( s + 2)( s 2 + 1) Ex. 14.41 F ( s ) = L [2u (t ) + 3e 4t u (t )] = 2L [u (t )] + 3L [e4t u (t )] =
Ex. 14.42 2 3 + s s+4 1 F ( s ) = L [sin(t  2)u (t  2)] = e 2 s L [sin t ] = e 2 s 2 s +1 Ex. 14.43
F ( s ) = L[t e  t ] = L[t ] s s +1= 1 s2 =
s s +1 1 ( s + 1) 2 Ex. 14.44 5 5 f ( t ) =  t + 5 u ( t )   ( t  4.2 ) u ( t  4.2 ) 3 3 4.2 s  1) 5 5 4.2 s 5 15 s + 5 ( e  2= F (s) =  2 +  e s 3 s2 3s 3s 141 Ex. 14.45 F (s) = 0 3 e  st f (t ) e dt = 0 3 e dt = s
 st 2  st 2 =
0 3(1e 2 s ) s Ex. 14.46 5 2 t 0<t < 2 f (t ) = otherwise 0 5 5 5 5 t u ( t ) u ( t  2 ) = t u ( t )  t u ( t  2 ) = t u ( t ) ( t  2 )u ( t  2 ) 2u (t  2) 2 2 2 2 5 1 e 2 s 2e 2 s 5 1 2 s 2 s F ( s ) = L f ( t ) = 2  2  = 2 s 2 1 e  2 se 2 s s s f (t ) = Ex. 14.51 F (s) = c + jd c  jd me j me j where m = c 2 + d 2 , = tan 1 d + = + c s + a  j s + a + j s + a  j s + a + j f ( t ) = e  at [ c cos t  d sin t ] u ( t ) = e at c 2 + d 2 cos( t + ) u ( t ) = m e at cos( t + ) u ( t ) Ex. 14.52 (a) F (s) = 8s 3 1 2( 8s 3) = s + 4s +13 2 ( s + 2 )2 + 9
2 a = 2, c =8, =3 & ca  d =3 d = 3( 8 )( 2 ) = 6.33 3 2 2 6.33 = tan 1 =38.4 , m = ( 8 ) + ( 6.33) =10.2 8 f ( t ) =10.2 e 2 t cos( 3 t +38.40 ) u ( t ) 142 (b) Given F ( s ) = ( 2( 3 ) ) . 3e  s 3 1 = , first consider F1 ( s ) = 2 2 s + 2s +17 s + 2s +17 2 ( s +1)2 +16 Identify a =1, c = 0, = 4 and  d =3 d =3 4. Then m =d =3 4, = tan 1 ( 3 ( 4 0 ) )=90 So f1 (t ) = (3 4)e t sin 4t u ( t ) . Next, F ( s ) = e  s F1 ( s ) f ( t ) = f1 ( t 1) . Finally f ( t ) =(3 4)e  (t 1) sin 4( t 1) u ( t 1) Ex. 14.53 (a) F (s) = s 2 5 s ( s +1)
2 = A B C + + s s +1 ( s +1)2 where
A = sF ( s ) s = 0 = 5 15 2 = 5 and C = ( s +1) F ( s ) s = 1 = =4 1 1
2 Multiply both sides by s ( s + 1) s 2  5 = 5 ( s +1) + Bs ( s +1) + 4 s 2 B=6 Then F (s) = Finally 5 6 4 + + s s +1 ( s +1)2 f ( t ) = ( 5 + 6 e  t + 4 t e  t ) u ( t ) (b) Where A= and F (s) = 4s 2 ( s + 3) 3 = A B C + + 2 ( s +3) ( s +3) ( s+3)3 1 d2 d 2 3 s + 3) F ( s ) s + 3) F ( s ) = 4, B = = 24 2 ( s =3 ( s =3 2 ds ds C = ( s + 3) F ( s ) s =3 = 36
3 Then F (s) = Finally 4 24 36 + + 2 ( s + 3 ) ( s + 3 ) ( s + 3 )3 f ( t ) = ( 4  24 t + 18t 2 ) e 3t u ( t ) 143 Ex. 14.61 (a) F ( s ) = 6s +5 s + 2s +1
2 s( 6s +5) f ( 0 ) = lim sF ( s ) = lim 2 =6 s s s + 2 s +1 s( 6s +5) f ( ) = lim sF ( s ) = lim 2 =0 s 0 s 0 s + 2 s +1 (b) F ( s ) = 6 s  2s +1
2 6s =0 f ( 0 ) = lim 2 s s  2s +1 6s = undefined no final value f ( ) = lim 2 s 0 s  2s +1 Ex. 14.71 KCL: v1 5 + i = 7 e 6 t KVL: 4 di di + 3 i  v1 = 0 v1 = 4 + 3 i dt dt di 4 + 3i 35 di Then dt + i = 7 e 6 t + 2 i = e 6 t dt 5 4 Taking the Laplace transform of the differential equation: s I ( s )  i (0) + 2 I ( s ) = 35 1 35 1 I (s) = 4 s +6 4 ( s + 2)( s + 6) Where we have used i (0) = 0 . Next, we perform partial fraction expansion.
1 A B 1 where A = = + ( s + 2) ( s + 6) s + 2 s + 6 s+6 Then I ( s) = 35 35 35 1 35 1  i (t ) = e 2t  e 6t 16 s + 2 16 s + 6 16 16 =
s =2 1 1 1 and B = = 4 s + 2 s = 6 4 144 Ex. 14.72 Apply KCL at node a to get 1 d v1 v 2  v1 = 48 dt 24 2 v1 + d v1 dt = 2 v2 Apply KCL at node b to get v 2  50 cos 2 t 20 + v 2  v1 24 + v2 30 + d v2 1 d v2 = 0  v1 + 3 v 2 + = 60 cos 2t 24 dt dt Take the Laplace transforms of these equations, using v1 (0) = 10 V and v2 (0) = 25 V , to get ( 2+ s ) V1 ( s)  2V2 ( s) = 10 and  V1 ( s) + ( 3+ s ) V2 (s) =
Solve these equations using Cramer's rule to get 25s 2 + 60s +100 s2 + 4 25s 2 + 60s +100 ( 2+ s ) +10 ( 2+ s ) ( 25s 2 + 60 s +100 ) +10 ( s 2 + 4 ) s2 +4 V2 ( s ) = = ( 2+ s ) (3+ s)  2 ( s 2 + 4 ) ( s +1)( s + 4 ) = Next, partial fraction expansion gives 25s 3 +120s 2 + 220 s + 240 ( s 2 + 4 ) ( s +1)( s + 4 ) V2 ( s ) =
where
A = A A* B C + + + s + j 2 s  j 2 s +1 s + 4
= 240 j 240 = 6 + j6 40 25s 3 +120 s 2 + 220 s + 240 ( s +1) ( s + 4 ) ( s  j 2 ) 25s 3 +120 s 2 + 220 s + 240 ( s2 +4) ( s+4) 25s 3 +120 s 2 + 220 s + 240 ( s 2 + 4 ) ( s +1) s = j 2 A* = 6  j 6 B = C =
s =1 = = 115 23 = 15 3 320 16 = 60 3 s =4 Then 145 V2 ( s ) = Finally 6+ j 6 6 j 6 23 3 16 3 + + + s + j 2 s  j 2 s +1 s + 4
23  t 16 4t e + e V t0 3 3 v2 (t ) = 12 cos 2 t + 12 sin 2 t + Ex. 14.73 Taking Laplace Transform of the differential equation:
s 2 F ( s ) = s f ( 0 )  f ' ( 0 ) + 5 s F ( s ) f ( 0 ) + 6 F ( s ) = 10 s +3 Using the given initial conditions ( s 2 + 5s + 6) F ( s ) = 10 2 s 2 +16s + 40 + 2s + 10 = s +3 s +3 2 s 2 +16s + 40 A B C F (s) = = + + 2 ( s + 3) ( s + 2 ) ( s + 3) ( s + 3) ( s + 3) ( s + 2 )
where A =  10, B =  14, and C = 16 . Then F ( s) = 10 + 14 16 + s +3 s + 2 f (t ) =  10te3t  14e 3t + 16e2t for t 0 ( s + 3) 2 Ex. 14.81 KCL at top node: VC ( s ) 3 s 2 + VC ( s ) = + 2 s 2
6 2  s s+ 2 3
 ( 2 / 3) t VC ( s ) = v C (t ) = 6  2 e ( ) u(t ) V 2 VC ( s ) I C (s) = 2= 3 2 2 s+ 3 s iC (t ) = 2  ( 2 / 3) t e u (t ) A 3 146 Ex. 14.82 Mesh Equations: 4 1 4 1   I C ( s )  6 ( I ( s )  I C ( s )) = 0  = 6 + I C ( s ) + 6 I ( s ) 2s s 2s s 10 6 ( I ( s )  I C ( s )) + 3 I ( s ) + 4 I C ( s ) = 0 I ( s ) =  I C ( s ) 9 Solving for Ic(s): 4 2 1 6  =  + I C (s) I C (s) = 3 s 3 2s s 4 So Vo(s) is 24 Vo ( s ) = 4 I C ( s ) = 3 s 4 Back in the time domain: v o ( t ) = 24 e0.75t u (t ) V Ex. 14.83 KVL: 8 20 + 4 = + 8 + 4s I L ( s ) s s so I L ( s) = ( s + 1) + 1 2+ s = s + 2 s + 5 ( s + 1) 2 + 4
2 Taking the inverse Laplace transform: 1 i ( t ) = e  t cos 2 t + e  t sin 2 t u ( t ) A 2 147 Ex. 14.91 10 5  5t 10 t (a) impulse response = L1  ) u(t ) = ( 5 e  10 e s + 5 s + 10 1 1 10 t 5t (b) step response = L1  = ( e  e ) u (t ) s + 10 s + 5 Ex. 14.92 H ( s ) = L 5 e  2 t sin ( 4 t ) u ( t ) = 5 ( 4) ( s + 2) 2 +4 2 = 20 s + 4 s + 20
2 H (s) s+4 1 1 1  2t step response = L1 =L  2 = (1  e (cos 4t  2 sin 4t )) u (t ) s s + 4 s + 20 s Ex. 14.101 Voltage division yields
2 s 2 8+ V ( s) s = H (s) = c 2 V1 ( s ) ( 8 ) s 2+ 2 8+ s 16 16 1 s = = = 4 16 16 s + 20 s +1.25 16 + + s s so h ( t ) = L1 H ( s ) = 1.25 e 1.25 t u ( t ) ( 8 ) 148 Ex. 14.102 h ( t ) = e 2 t f (t ) = u(t ) H (s) = 1 s+2 1 F(s) = s 1 1 1 2 1 2 1 2t + = e u ( t ) h( t ) f ( t ) = L1 H ( s ) F ( s ) = L1 = L s( s + 2 ) s+2 2 s Ex. 14.111 The poles of the transfer function are p1,2 = a.) When k = 2 V/V, the poles are p1,2 =  (3  k ) (3  k )
2 2 8 . 1 7 so the circuit is stable. The transfer function is 2
Vo ( s ) Vi ( s ) = 2s s +s+2
2 H (s) = The circuit is stable when k =2 V/V so we can determine the network function from the transfer function by letting s = j.
V o ( ) V i ( ) = H ( ) = H ( s ) s = j = 2s 2 j = s + s + 2 s = j ( 2  2 ) + j
2 The input is v i ( t ) = 5cos 2 t V . The phasor of the steady state response is determine by multiplying the phasor of the input by the network function evaluated at = 2 rad/s. 2 j V o ( ) = H ( ) = 2 V i ( ) = 2  2 ) + j ( ( 50 ) = j 4 ( 50 ) = 7.07  45 2 + j 2 =2 The steady state response is vo ( t ) = 7.07 cos ( 2 t  45 ) V . b. When k = 3  2 2 , the poles are p1,2 = transfer function is H (s) = The impulse response is
149 2 2 0 =  2,  2 so the circuit is stable. The 2 = 0.17  0.17 2 (s + 2) (s + 2) (s + 2)
2 0.17 s 2 h ( t ) = L 1 H ( s ) = 0.17 e  2t (1  2 t u (t ) ) We see that when k = 3  2 2 the circuit is stable and lim h(t ) = 0 .
t c. When, k = 3 + 2 2 the poles are p1,2 = transfer function is H (s) = The impulse response is 2 2 0 = 2, 2 so the circuit is not stable. The 2 = 5.83 + 5.83 2 (s  2) (s  2) (s  2)
2 2t 5.83s 2 h ( t ) = L 1 H ( s ) = 5.83 e (1 +
t 2 t u (t ) ) We see that when k = 3 + 2 2 the circuit is unstable and lim h(t ) = .
Ex. 14.121 For the poles to be in the left half of the splane, the sterm needs to be positive. 2 s +5 10 2s + 20 2 + V0 ( s ) = 0.1  2 = 0.1  2 2 2 ( s +5 ) +102 ( s +5 ) +102 s s +10 s + 125 s = 0.1 2( s 2 +10 s +125 ) ( 2s + 20 ) s s 2 +10s +125 250 25 = 0.1 2 = 2 s +10s +125 s +10s +125 These specifications are consistent. 1410 Problems
Section 143: Laplace Transform P14.31 L A f1 ( t ) = A F1 ( s ) f1 ( t ) = cos ( t ) As s F ( s ) = s2 + 2 F1 ( s ) = 2 2 s + n! s n +1 1 1! = 2 1+1 s s P14.32 L1 t n = P14.33 F ( s ) = L1 t1 = Linearity: L a1 f1 ( t ) + a2 f 2 ( t ) = a1 F1 ( s ) + a2 F2 ( s ) Here a1 = a2 = 1 L f1 ( t ) = L e 3t = L f 2 ( t ) = L[t ] = so F ( s ) = 1 1 + 2 s +3 s 1 = F1 ( s ) s+3 1 = F2 ( s ) s2 P14.34 f ( t ) = A (1e bt ) u ( t ) = L [ Af1 (t ) ] = AF1 ( s ) f1 ( t ) = A(1 e  bt ) u ( t ) = 1u ( t ) e  bt u ( t ) = f 2 ( t ) + f3 ( t ) 1 1 , F3 ( s ) = s s +b 1 Ab 1 F (s) = A  = s( s +b ) s s +b F2 ( s ) = 1411 Section 144: Impulse Function and Time Shift Property P14.41 (1e A Ae  sT F ( s ) = AL u ( t )  AL u ( t T ) =  =A s s s
P14.42 f ( t ) = A u ( t )  u ( t T )  sT ) f ( t ) = 1 u ( t ) u ( t T ) eat L u ( t ) u ( t T ) = F ( s ) = L e at u ( t )u ( t T ) 1 e sT s 1 e( s  a )T F (s) = ( s a ) L eat g ( t ) =G ( s  a ) P14.43 (a) F (s) = 2 ( s +3) 3 (b) (c) f ( t ) = ( t T ) u ( t T ) F ( s ) = e  sT L ( t ) = e  sT F (s) = 5 ( s + 4 ) +( 5)
2 2 = 5 5 = 2 ( s + 8 s + 16 ) + 25 s + 8 s + 41
2 P14.44 g ( t ) = e  t u ( t 0.5 ) = e  (t + (0.50.5))u ( t  0.5 ) = e0.5 e ( t  0.5)u ( t  0.5 ) L e 0.5 e  (t 0.5)u ( t  0.5 ) = e0.5 L e (t  0.5)u ( t  0.5 ) = e0.5 e0.5 s L e t u ( t ) = e0.5 e 0.5 s e0.5  0.5 s = s +1 s +1 P14.45
 sT e  sT t T  sT t e L  L  t u( t ) = u( t  T ) = e L  u( t ) = T s2 T T T 1412 Section 145: Inverse Laplace Transform P14.51
F (s) = s +3 s +3 A Bs + C = = + 2 2 2 s + 3s + 6s + 4 ( s +1) ( s +1) + 3 s +1 s + 2s + 4 3 where
A= s +3 ( s +1) 2 +3 s =1 = 2 3 Then 2 2 8 Bs + C 4 = 3 + 2 ( s + 3) = ( + B ) s 2 + + B + C s + + C 2 3 3 3 ( s +1) ( s + 2s + 4 ) s +1 s + 2s + 4 ( s + 3) Equating coefficient yields
2 2 + B B=  3 3 4 2 1 s : 1=  + C C = 3 3 3 s2 : 0 = Then
1 2 2 1 2 2 3  s+  ( s +1) 3 3 + 3 3 = 3 + 3 F (s) = + s +1 ( s +1)2 + 3 s +1 ( s +1)2 + 3 ( s +1)2 + 3 Taking the inverse Laplace transform yields f (t ) = 2 t 2 t 1 t e  e cos 3t + e sin 3 3 3 3 1413 P14.52 F (s) = where s 2  2s + 1 s 2  2s + 1 a a* b = = + + 3 2 s + 3s + 4s + 2 ( s +1) ( s +1 j )( s +1+ j ) s +1 j s +1+ j s +1
b= a= s 2  2s +1 =4 ( s +1) 2 +1 s =1 3 j 4 3 s 2  2s +1 = = + j 2 ( s +1) ( s +1+ j ) s =1+ j 2 2 3 a* =   j 2 2 Then
3 3  + j2   j2 4 F (s) = 2 + 2 + s +1 j s +1+ j s +1 Next m= From Equation 14.58 ( 3 2 )2 + ( 2 ) 2 2 5 = = 126.9 and = tan 1 3 2  2 f ( t ) = 5 e  t cos ( t + 127 ) + 4 e t u ( t ) P14.53
F (s) = where B= Then
A= 5 s 1 ( s +1) ( s  2 )
2 = A B C + + 2 s +1 ( s +1) s 2 5 s 1 =1
s=2 5 s 1 s 2 = 2 and C =
s =1 ( s +1)
9
2 2 d 2 s +1) F ( s ) ( ds s =1 = ( s 2) = 1
s =1 Finally F (s) = 1 2 1 + + 2 s +1 ( s +1) s2 f ( t ) = e  t + 2 t e  t + e 2t u ( t ) 1414 P14.54 Y (s) =
where 1 1 A Bs +C = = + 2 ( s +1) ( s + 2s + 2 ) ( s +1) ( s +1) + 1 s +1 ( s +1)2 +1
2 A= 1 s + 2s + 2
2 =1
s =1 Next 1 1 Bs +C = + 2 1 = s 2 + 2 s + 2 + ( Bs + C ) ( s + 1) ( s +1) ( s + 2s + 2 ) s +1 s + 2s + 2
2 1 = ( B +1) s 2 + ( B + C + 2 ) s + C + 2 Equating coefficients: s 2 : 0 = B + 1 B = 1 s : 0 = B + C + 2 C =1 Finally Y (s) = 1 s +1  s +1 ( s +1)2 +1 y ( t ) = e t  e  t cos t u ( t ) P14.55 F (s) = ( s +1) ( s 2( s + 3)
2 + 2 s +5) = ( s +1) 1 2 + + 2 s +1 ( s +1) + 4 ( s +1)2 + 4 f ( t ) = e t  e  t cos ( 2t ) + e t sin ( 2t ) u ( t ) P14.56 F (s) = where
A = sF ( s ) s =0 = 2( s+3) A B C = + + s( s+1) ( s + 2 ) s s +1 s + 2
= 3, B = ( s +1) F ( s ) s =1 = 2( s + 3) s( s + 2 ) =4 2( s + 3 ) ( s +1) ( s + 2 ) s =0 s =1 and ( s + 2 ) F ( s ) s = 2 =
Finally
3 4 1 + F (s) = + s s +1 s + 2 2( s + 3) s( s +1) s =2 = C =1 f ( t ) = ( 3  4e t + e 2t ) u ( t ) 1415 Section 146: Initial and Final Value Theorems P14.61 (a) 2s 2 3s + 4 2s 2 f ( 0 ) = lim sF ( s ) = lim = 2 =2 2 s s s s +3s + 2
4 f ( ) = lim sF ( s ) = = 2 2 s 0 (b) P14.62 Initial value: s( s +16 ) s 2 + 16 s v ( 0 ) = lim sV ( s ) = lim 2 = lim 2 =1 s s s + 4 s + 12 s s + 4 s + 12 s +16 s 2 + 16 s = lim 2 =0 v ( ) = lim s 2 s 0 s + 4 s + 12 s 0 s + 4 s +12 (Check: V(s) is stable because Re { pi } < 0 since pi =  2 2.828 j . We Final value: expect the final value to exist.)
P14.63 Initial value: s 2 +10 s v(0) = lim sV ( s ) = lim = 0 s s 3 s 3 + 2 s 2 +1 Final value: v ( ) = lim sV ( s ) = lim
s 0 s 0 s ( 3s 2 + 2s +1) s ( s +10 ) = 10 (Check: V(s) is stable because pi = 0.333 0.471 i . We expect the final value to exist.)
P14.64 Initial value: f ( 0 ) = lim s F ( s ) = lim
s s 2 s 2 14 s = 2 s 2  2 s + 10 Final value: F(s) is not stable because Re { p1} > 0 since pi = 1 3i . No final value exists. 1416 Section 147: Solution of Differential Equations Describing a Circuit P14.71 KVL:
4 di + v = 2 e210 t dt The capacitor current and voltage are related by 50 i + 0.001 i = ( 2.5 106 ) dv dt v1 = 2 e 210 V , i (0) = 1 A, v(0) = 8 V 4t Taking the Laplace transforms of these equations yields 50 I ( s) + 0.001 [ s I ( s)  i (0) ] + V ( s) = I ( s) = ( 2.5 106 ) sV ( s )  v( 0 ) Solving for I(s) yields I (s) = where
A = ( s + 10 ) I ( s )
4 s = 10 4 2 s + 2104 s 2 + 1.4 104 s  1.6 108 ( s +104 ) ( s + 2 104 ) ( s + 4 104 ) = A B C + + 4 4 s +10 s + 2 10 s + 4104
2108 2 = = 3 108 3 =
s =  2 10 4 s 2 + 1.4 104 s 1.6 108 = ( s + 2 104 )( s + 4 104 )
4 = s = 10 4 B = ( s + 2104 ) I ( s ) C = ( s + 4104 ) I ( s ) s =  2 10 s 2 + 1.4 104s 1.6 108 ( s+ 104 ) ( s + 4104 ) s 2 + 1.4 104s 1.6 108 ( s+104 ) ( s+ 2 104 ) .4 108 1 = 8 2 10 5 8.8 108 22 = 8 6 10 15 s =  4 10 4 = =
s =  4 10 4 Then I (s) =  23 15 22 15 + + 4 s +10 s + 210 s + 4 104 i (t ) =
4 4 4 1 10 e10 t + 3e2x10 t + 22 e4x10 t u ( t ) A 15 1417 P14.72 We are given v ( t ) = 160 cos 400t . The capacitor is initially uncharged, so v C ( 0 ) = 0 V . Then i ( 0) = 160 cos ( 400 0 )  0 = 160 A 1 KCL yields 103 dvC dt + vC 100 =i Apply Ohm's law to the 1 resistor to get v v C i= vC = v i 1 Solving yields di + 1010 i = 1600 cos 400t  ( 6.4 104 ) sin 400t dt Taking the Laplace transform yields
s I ( s )  i (0) + (1010 ) I ( s ) = 1600s s 2 + ( 400 )
2  ( 6.410 ) ( 400 )
2 s 2 + ( 400 ) 2 so I (s) = Next A B B* 1600s  2.5107 = + + ( s + 1010 ) s 2 + (400)2 s + 1010 s + j 400 s  j 400 where
A =
1600 s  2.5 x 107 ( s +1010 ) ( s  j 400 ) 160 1600s  2.5107 + s + 1010 ( s + 1010 ) s 2 + (400) 2 1600s  2.5107 s 2 + ( 400 )
=
2 s = 1010 =  23.1 , B = 2.56 x 107 1.4 8.69 x 10 68.4
5 = 11.5  j 27.2 and B* = 11.5 + j 27.2 s =  j 400 Then I (s) = Finally 136.9 11.5 j 27.2 11.5 + j 27.2 + + s + 1010 s + j 400 s  j 400 i ( t ) = 136.9e1010t + 2 (11.5 ) cos 400t  2 ( 27.2 ) sin 400t for t > 0 = 136.9e1010t + 23.0 cos 400t  54.4sin 400t for t > 0 1418 P14.73 vC (0) = 0 vc +15 i = 10 cos 2t 1 d vc i= 30 dt Taking the Laplace Transform yields: sVc ( s )  vc ( 0 ) + 2Vc ( s) = 20 where A= Then 20 s s2 +4 =
s = 2 d vc + 2 vc = 20 cos 2t dt s A B B* 20s Vc ( s ) = = + + s2+ 4 ( s + 2 )( s 2 + 4 ) s + 2 s + j 2 s  j 2 =
s =  j2 40 20s = 5, B = 8 ( s + 2 )( s  j 2 ) j5 5 5 5 5 = + j and B* =  j 1+ j 2 2 2 2 5 5 5 5 +j j 5 2 2 2 2 Vc ( s ) = + + s+2 s+ j2 s j2 vc ( t ) = 5e 2t + 5 ( cos 2t + sin 2t ) V P14.74 vc + 12i L + 2 diL dt = 8 and i L = C d vc dt Taking the Laplace transform yields Vc ( s ) + 12 I L ( s ) + 2 sI L ( s ) iL ( 0 ) =  I L ( s ) = C sVc ( s ) vc ( 0 ) 8 s vc (0) = 0, iL (0) = 0 Solving yields
1419 Vc ( s ) = 4 C C s s 2 + 6s + 2 72 s ( s + 3)
2 (a) C = 1 F 18 Vc ( s ) = = c a b + + s s + 3 ( s + 3) 2 24 8 8 + + s s + 3 ( s + 3) 2 a =  8, b = 8, and c = 24 Vc ( s ) = vc ( t ) = 8 + 8 e 3t + 24 t e 3t (b) C = 1 F 10 Vc ( s ) = c a b 40 = + + s ( s +1) ( s +5 ) s s +1 s + 5 a =  8, b = 10, and c = 2 Vc ( s ) = 2 8 10 + + s s +1 s + 5 vc ( t ) =  8 + 10 e  t  2 e 5 t P14.75 vc (0 ) = 10 V, i L( 0 ) = 0 A d vc di and 400 i + 1 + vc = 0 dt dt i = ( 5 106 ) Taking Laplace transforms yields 1  400 I ( s ) = ( 5 10 ) ( sVc ( s )  10 ) 10 40 = I (s) = 2 2 5 s + 400 s + 2 10 400 I ( s ) + ( s I ( s )  0 ) + Vc ( s ) = 0 ( s + 200 ) + 4002 6 so i (t ) =  1 200t e sin ( 400t ) u ( t ) A 40 1420 Section 148: Circuit Analysis Using Impedance and Initial Conditions P14.81 6 6  0.010  0.002 s .003 .005 s s I L ( s) = = = = 5s + 2000 s ( s + 400) s s + 400 2 mA iL (t ) = 400 t mA 35e t <0 t >0 P14.82 10 8 VL ( s )  ( .015 ) s + VL ( s ) + 3 VL ( s ) = 0= 4000 2000 4000 5s s+ 15 8 V ( s ) + 0.15 0.005 0.002 15 I L ( s) = L = + 0.015 =  4000 5s 5 4000 s+ s s+ 15 15 VL ( s )  iL (t ) = 5  3e
 4000 t 15 mA, t > 0 1421 P14.83  0.006 Vc ( s ) + + s 2000 Vc ( s )  106 .5s 8 s =0  6000 8 + 500 Vc ( s ) + 0.5s Vc ( s )  = 0 s s 8 s + 12000 12 4 =  s ( s +1000) s s +1000 Vc ( s ) = Vc (t ) = 12  4e 1000t V, t > 0 P14.84 Vc ( s )  6 s + Vc ( s ) + 0.5s V ( s )  8 = 0 c s 2000 4000 106 6 8 500 Vc ( s )  + 250Vc ( s ) + 0.5s Vc ( s )  = 0 s s Vc ( s ) = 6000 + 8s 4 4 = + s ( s + 1500 ) s s + 1500 vc (t ) = 4 + 4e1500t V, t > 0 1422 P14.85 Node equations: Va ( s )  VC ( s ) Va ( s ) 1 6 6 + = Va ( s ) = VC ( s ) + s 6 s s+6 s+6 6 6 6 VC ( s )  VC ( s ) + VC ( s )  3 s+6 1 s s+6 s+3 + + + VC ( s )  = 0 4 2 s s 4 After quite a bite of algebra: VC ( s ) = Partial fraction expansion:
44 1 6 s + 56 s + 132 9 V (s) = = 3  + 3 c ( s +3)( s + 2 )( s +5) s + 2 s +3 s +5 Inverse Laplace transform: v (t ) = 44 3 e 2t  9e 3t + (1 3)e 5t V c
2 6 s 2 + 56s + 132 ( s + 2 )( s + 3)( s + 5) 1423 P14.86 Write a node equation in the frequency domain:
10 s = Vo ( s )  5 C + Vo ( s ) V ( s ) = o 1 R1 R2 Cs 10 +5s R1C 10 R2 R1 s 5  10 R2 1 ss + R 2C = + R1 1 s+ R 2C Inverse Laplace transform: vo ( t ) = 10 R2 R 2 t + 5  10 e R1 R1 R 2C = 10  5 e1000t V for t > 0 1424 P14.87 Here are the equations describing the coupled coils: v1 (t ) = L1 di1 di +M 2 dt dt di di v2 (t ) = L2 2 + M 1 dt dt V1 ( s) = 3 ( s I1 ( s )  2 ) + ( sI 2 ( s)  3) = 3s I1 ( s ) + sI 2 ( s )  9 V2 ( s) = s ( I1 ( s )  2 ) + 2( sI 2 ( s ) 3) = sI1 ( s) + 2sI 2 ( s )  8 Writing mesh equations:
5 5 = 2 ( I1 ( s ) + I 2 ( s ) ) + V1 = 2 ( I1 ( s ) + I 2 ( s ) ) + 3s I1 ( s ) + sI 2 ( s )  9 ( 3s + 2 ) I1 + ( s + 2 ) I 2 = 9 + s s V1 ( s ) = V2 ( s ) + 1I 2 ( s ) 3s I1 ( s ) + sI 2 ( s )  9 = sI1 ( s ) + 2 sI 2 ( s )  8+ I 2 ( s ) 2s I1  ( s +1) I 2 =1 Solving the mesh equations for I2(s): I2 ( s ) = 15s + 8 3s + 1.6 0.64 2.36 = + = s + 0.26 s + 1.54 5s 2 + 9s + 2 ( s + 0.26 )( s +1.54 ) Taking the inverse Laplace transform:
i2 (t ) = 0.64e 0.26t + 2.36e 1.54t A for t > 0 P14.88 t<0 time domain Mesh equations in the frequency domain: 6 I 1 ( s ) + 6 ( I 1 ( s )  I 2 ( s )) + 6 I 1 ( s ) + frequency domain 12 2 2 = 0 I1 (s) = I 2 (s)  s 3 3s 1425 2 6 2 6 I 2 ( s )   6 ( I 1 ( s )  I 2 ( s )) = 0 6 + I 2 ( s )  6 I 1 ( s ) = s s s s Solving for I2(s): 1 2 2 2 6 I 2 (s) = 2 6 + I 2 (s)  6 I 2 (s)  = 1 s 3 3s s s+ 2 Calculate for Vo(s):
1 6 Vo ( s ) = I 2 ( s )  = 2 s 1 1 2 6 4 2   = 2 s+ 1 s s+ 1 s 2 2 Take the Inverse Laplace transform: vo ( t ) =  ( 4 + 2 e t / 2 ) V for t > 0 (Checked using LNAP, 12/29/02)
P14.89 t<0 time domain Writing a mesh equation: frequency domain 2 6 s + 3 12 3 5 ( 4 + 5 s ) I ( s ) + 30 + = 0 I ( s ) = 4 =  + 4 s s s+ ss + 5 5 Take the Inverse Laplace transform: i ( t ) = 3 (1 + e0.8 t ) A for t > 0 (Checked using LNAP, 12/29/02) 1426 P14.810 Steadystate for t<0: From the equation for vo(t): vo ( ) = 6 + 12 e From the circuit: vo ( ) = Therefore: 6= 3 (18) R = 6 R+3 3 (18) R+3  2 () =6 V Steadystate for t>0: 6 1 18 6 I (s) 2 + +  = 0 I (s) = 1 Cs s s s+ 2C 6 18 12 1 18 1 12 18 12 6 + = + + = + Vo ( s ) = I (s) + = 1 s 1 1 Cs s Cs s + s s s+ s s+ 2C 2C 2C Taking the inverse Laplace transform:
vo ( t ) = 6 + 12 e  t / 2C V for t > 0 Comparing this to the given equation for vo(t), we see that 2 = 1 2C C = 0.25 F . (Checked using LNAP, 12/29/02) 1427 Section 149: Transfer Function and Impedance P14.91 R1 R1 R2 C1s and Z 2 = = R 1 R1C1s + 1 R2C2 s +1 R1 + C1s R 2( 1 s + 1) Let 1 = R1C1 and 2 = R2C2 then H ( s ) = R 1 ( 2s + 1) + ( 1 s + 1) R 2 H (s) = where Z1 =
When 2 = 2 = H ( s ) = we require R1C 1 = R2C2 Z2 Z1 + Z 2 R2( 1s + 1) R2 = = constant, as required. ( R1 + R2 ) ( s + 1) R1 + R2 P14.92 Let Z1 = R + 1 and Z 2 = R + Ls then the input impedance is Cs 1 L 2 R + ( R + Ls ) LCs + RC + R s +1 ZZ Cs Z (s) = 1 2 = = R 2 1 Z1 + Z 2 LCs + 2 RCs +1 R+ + R + Ls Cs L Now require : RC + = 2 RC L = R 2C then Z = R R P14.93 The transfer function is R2
H (s) = R 2 C s +1 = R2 R1 + s+ R 2 C s +1 R1 R 2 C 1 R1 C R1 + R 2 Using R1 = 2 , R 2 = 8 and C = 5 F gives
H (s) = 0.1 s + 0.125 The impulse response is h (t ) = L 1 H ( s ) = 0.1 e0.125 t u (t ) V . The step response is 1428 H ( s) 0.1 0.8 1 0.8 0.125 t = L 1 L 1 u (t ) V s ( s + 0.125) = L s  s + 0.125 = 0.8 1 e s ( ) (Checked using LNAP, 12/29/02)
P14.94 The transfer function is: H ( s ) = L 12 t e 4 t u ( t ) = The Laplace transform of the step response is: 12 ( s + 4) 2 = 12 s + 8s + 16
2 3 H (s) 12 k 3 = = 4+ + 2 2 s s ( s + 4) s+4 s ( s + 4) The constant k is evaluated by multiplying both sides of the last equation by s ( s + 4) . 3 3 3 2 12 = ( s + 4)  3s + ks ( s + 4) = + k s 2 + (3 + 4k ) s + 12 k =  4 4 4 The step response is H ( s ) 3 4 t =  e 3 t + 3 u (t ) V L 1 s 4 4 P14.95 The transfer function can also be calculated form the circuit itself. The circuit can be represented in the frequency domain as
2 We can save ourselves some work be noticing that the 10000 ohm resistor, the resistor labeled R and the op amp comprise a noninverting amplifier. Thus R V s Va ( s ) = 1 + 10000 c ( ) Now, writing node equations, 1429 Vc ( s ) Vi ( s ) Vo ( s ) Va ( s ) Vo ( s ) + CsVc ( s ) = 0 and + =0 1000 5000 Ls Solving these node equations gives R 5000 1 1 + 10000 L 1000 C H (s) = 1 5000 s + s + 1000C L Comparing these two equations for the transfer function gives 1 1 = ( s + 2000) or s + = ( s + 5000) s + 1000C 1000C 5000 5000 = ( s + 2000) or s + = ( s + 5000) s + L L 1 R 5000 = 15 10 6 1 + 1000C 10000 L The solution isn't unique, but there are only two possibilities. One of these possibilities is s + 1 = ( s + 2000) C = 0.5 F 1000C 5000 s + = ( s + 5000) L 1 L =1H 1 + R 5000 = 15106 R = 5 k 1000 0.5106 10000 1 ( ) (Checked using LNAP, 12/29/02) 1430 P14.96 The transfer function of the circuit is The give step response is vo ( t ) = 4 (1  e250 t ) u ( t ) V . The correspond transfer function is calculated as H (s) 4 1000 1000 4 = L 4 (1  e  250 t ) u ( t ) =   H (s) = = s s + 250 s s + 250 s ( s + 250 ) 1 1+ R2 C s R1 C H (s) =  = 1 R1 s+ R2 C R2 { } Comparing these results gives 1 1 1 = 250 R 2 = = = 40 k 250 C 250 ( 0.110  6 ) R2 C 1 1 1 = 1000 R1 = = = 10 k 1000 C 1000 ( 0.110  6 ) R1 C (Checked using LNAP, 12/29/02)
P14.97 4 2 Va ( s ) = Vi ( s ) = Vi ( s ) s+2 4+ 2s 12 Vo ( s ) = s 12 6+ s The transfer function is: H (s) = 2 2 2 2 Vb ( s ) = Vb ( s ) = 5 Va ( s ) = 5 Vi ( s ) s+2 s+2 s+2 s+2 Vo ( s ) 20 = Vi ( s ) ( s + 2 )2 1431 The Laplace transform of the step response is: 20 5 5 10 Vo ( s ) = = + + 2 s s + 2 ( s + 2 )2 s ( s + 2) Taking the inverse Laplace transform: vo ( t ) = 5  5 e 2 t (1 + 2t ) u ( t ) V (checked using LNAP 8/15/02)
P 14.98 From the circuit: 1 1 4 6C Cs L 4 H (s) = = (k ) (k ) 4 + Ls s+ 1 6+ 1 s+ 4 Cs L 6C From the given step response: H (s) 2 4 6 12 = L ( 2 + 4 e 3 t  6 e  2 t ) u ( t ) = + s s + 3  s + 2 = s ( s + 3)( s + 2 ) s so 12 H (s) = s ( s + 3)( s + 2 ) Comparing the two representations of the transfer functions let
4 = 2 L = 2 H and 2 3 k = 12 k = 2 V/V . L 1 1 =3 C = F, 6C 18 (Checked using LNAP, 12/29/02)
P 14.9.9 From the circuit: 1432 R V (s) R+ Ls L = = H (s) = o Vi ( s ) 12 + R + L s s + 12 + R L From the given step response: s+
H (s) s+2 0.5 0.5 = L 0.5 (1 + e 4 t ) u ( t ) = + = s s s + 4 s ( s + 4) H (s) = s+2 s+4 Comparing these two forms of the transfer function gives: R =2 12 + 2 L L = 4 L = 6 H, R = 12 12 + R L =4 L (Checked using LNAP, 12/29/02)
P14.910 Mesh equations:
1 1 1 V ( s ) = R1 + + I1 ( s )  I2 ( s ) Cs Cs Cs 1 1 0 = R+ R+ I2 ( s )  I1 ( s ) Cs Cs Solving for I2(s): Then Vo ( s ) = R I 2 ( s ) gives H (s) = 1 V (s) Cs I2 ( s ) = 2 1 1 R1 + 2 R +  (Cs) 2 Cs Cs V0 ( s ) RCs = = V (s) [ R1Cs + 2][ 2 RCs +1]  1 s 1 s 2 + 4 RC + R1C s + 2 R1C 2 2 2 RR1C 2 ( 2RR1C ) 1433 P14.911 Let 1 R R Cs Z2 = = 1 RCs + 1 R+ Cs Z1 = Rx + Lx s Then
V2 Z2 = = V1 Z1 + Z 2 Rx + Lx s + V2 V1 R RCs + 1 R RCs + 1 = R Lx RCs + ( Lx + Rx RC ) s + Rx + R
2 1 LC = ( L + R RC ) s + Rx + R s2 + x x Lx RC Lx RC P14.912 Node equations: (V1  Vin ) sC1 + V1  Vout =0 R1 ( R C s + 1)V
1 1 1 = R1C1sVin + Vout V0 + Vout + sC2 = 0 V1 =  R 2C2 sVout R2 Solving gives:
H (s) =
 R1C1s Vout = = Vin R1 R 2C1C2 s 2 + R 2C2 s +1 s2 +  1 s R 2 C2 1 1 s+ R1C1 R1 R 2C1C2 1434 P14.913
Node equations in the frequency domain: V1  Vi V1  V2 V1  V0 + + =0 R1 R2 R3 1 V 1 1 V V1 + +  0 = i R1 R2 R3 R3 R1 V2  V1  sC2V0 = 0 V1 =  sC2 R2 V0 R2 After a little algebra: H ( s )= V0  R3 = Vi sC2 R2 R3 + sC2 R1 R3 + sC2 R1 R2 + R1 P14.914
1 1 Vo ( s ) Cs LC H (s) = = = R 1 1 Vi ( s ) Ls + R + s2 + s + Cs L LC L, H
2 2 1 2 C, F
0.025 0.025 0.391 0.125 R, 18 8 4 8
2 2 H(s)
20 20 = s + 9 s + 20 ( s + 4 )( s + 5 ) 20 20 = s + 4s + 20 ( s + 2 )2 + 44
2 2.56 2.56 = s + 4 s + 2.56 ( s + 0.8 )( s + 3.2 ) 20 20 = s + 4s + 4 ( s + 2 )2
2 1435 a) H ( s ) = 20 ( s + 4 )( s + 5) 20 20  h ( t ) = ( 20e 4t  20e 5t ) u (t ) s + 4 s +5 20 1 5 4 H ( s) L {step response} = = = + + s s ( s + 4) ( s + 5) s s + 4 s +5 L {h(t )} = H ( s ) = step response = (1+ 4e 5t 5e 4t ) u (t ) b) H ( s ) = 20 ( s + 2) 2 +4 4 5(4) h ( t ) = 5e 2t sin 4t u (t ) ( s + 2) 2 + 42 H ( s) 20 1 K s + K2 = = + 21 L {step response} = 2 s s ( s + 4s + 20) s s + 4s + 20 L {h( t )} = H (s) = 20 = s 2 + 4s + 20 + s ( K1s + K 2 ) = s 2 (1+ K1 ) + s ( 4+ K 2 ) + 20 K1 = 1, K 2 =  4 1  ( 4) ( s + 2 ) 1 2 L {step response} = + + s ( s + 2 )2 + 42 ( s + 2 ) + 42 1 step response = 1 e 2t cos 4t + sin 4t u (t ) 2 c)
2.56 H (s) = ( s + 0.8)( s + 3.2 )
L {h( t )} = H ( s ) = 1.07 1.07  h ( t ) = 1.07 ( e .8t  e 3.2t ) u(t) s + .8 s + 3.2 1 4 2.56 1 H (s) L {step response} = = = + 3 + 3 s s ( s + .8) ( s + 3.2) s s + .8 s + 3.2 4 1 step response = 1+ e 3.2t  e .8t u (t ) 3 3 d) H ( s ) = 20 ( s + 2) 2 step response = (1(1+ 2t )e 2t ) u (t ) h( t ) = 4te 2t u (t ) 1436 P14.915 For an impulse response, take V1 ( s ) = 1 . Then
3( s + 2 ) A B B* V0 ( s ) = = + + s ( s + 3 j 2 ) ( s + 3+ j 2 ) s s + 3 j 2 s + 3+ j 2 Where
A = sV0 ( s )
s =0 =.462, B = (s + 3  j 2) V0 ( s ) s =3+ j 2 = 0.47  119.7 o and B* = 0.47 119.7 o Then
V0 ( s ) = 0.462 0.47 119.7 o 0.47 119.7 o + + s s +3 j 2 s +3+ j 2 The impulse response is v0 (t ) = 0.462 + 2(0.47)e 3t cos ( 2 t  119.7 o ) u ( t ) V Section 1410: Convolution Theorem P14.101
1 e s 1  e s f ( t ) = u ( t )  u ( t  1) F ( s ) = L u ( t )  u ( t  1) =  s s = s s 2 1  2 e  s + e2 s 2 1 1 1  e f ( t ) * f ( t ) = L F ( s ) = L = L 1 s2 s = t u ( t )  2 ( t  1) u ( t  1) + ( t  2 ) u ( t  2 ) P14.102
f ( t ) = 2 u ( t )  u ( t  2 ) F ( s ) = 2 2e 2 s  s s 4 8e 2 s 4e 4 s f = L1 F ( s ) F ( s ) = L1 2  2 + 2 = 4t u ( t )  8 ( t  2 ) u ( t  2 ) + 4 ( t  4 ) u ( t  4 ) f s s s 1437 P14.103
v1 ( t ) = t u ( t ) V1 ( s ) = V2 ( s ) 1 s2 1 1 H (s) = = Cs = RC 1 V1 ( s ) R + 1 s+ Cs RC v2 ( t ) = h ( t ) v1 ( t ) = L1 V1 ( s ) H ( s ) 1 1 V2 ( s ) = V1 ( s ) H ( s ) = 2 RC s s+ 1 RC v2 ( t ) = t  RC (1  e  t / RC ), t 0 P14.104
1 1 h ( t ) f ( t ) = L1 H ( s ) F ( s ) where H ( s ) = 2 and F ( s ) = s s+a 1 1 A B C So H ( s ) F ( s ) = + 2 + = s s s+a s 2 s +a Solving the partial fractions yields: A = 1 a 2 , B = 1 a, C = 1 a 2 So h( t ) f ( t ) = 1 t e  ( at ) + + 2 , a2 a a t0 1438 Section 1411: Stability P14.111 a. From the given step response:
H (s) =L s From the circuit: R H (s) = R + 5 + Ls Comparing gives R = 75 R = 15 L R+5 L = 0.2 H = 100 L b. The impulse response is 75 h ( t ) = L 1 = 75 e 100 t u ( t ) s + 100 c. R H (s) L = R+5 s ss + L 3 100 t ) u ( t ) = s ( s 75 ) 4 (1  e + 100 H ( ) =100 = 75 3 = 45 j 100 + 100 4 2 15 3 45 ( 50 ) = 45 V Vo ( ) = 4 2 4 2 vo ( t ) = 2.652 cos (100 t  45 ) V (Checked using LNAP, 12/29/02) P14.112 The transfer function of this circuit is given by
H (s) 5 5 10 20 = L ( 5  5 e 2 t (1 + 2t ) ) u ( t ) = + s s+2+ s+2 2 = s+2 2 s ( ) ( ) H (s) = 20 s ( s + 2)
2 This transfer function is stable so we can determine the network function as H ( ) = H ( s ) s = j = 20 ( s + 2) 2 s= j = 20 (2 + j ) 2 1439 The phasor of the output is Vo ( ) = 20 ( 2 + j 2) 2 ( 545 ) = (2 20 245 ) 2 ( 545 ) = 12.5  45 V The steadystate response is vo ( t ) = 12.5cos ( 2 t  45 ) V
(Checked using LNAP, 12/29/02) P 14.113
The transfer function of the circuit is H ( s ) = L 130 t e 5t u (t ) = so we can determine the network function as 30 ( s + 5) 2 . The circuit is stable H ( ) = H ( s ) s = j =
The phasor of the output is 30 ( s + 5)
30 2 s= j = 30 (5 + j ) 2 Vo ( ) = 30 ( 5 + j 3) 2 (100 ) = ( 5.8331 ) 2 (100 ) = 8.82  62 V The steadystate response is vo ( t ) = 8.82 cos ( 3 t  62 ) V 1440 PSpice Problems
SP 141 1441 SP 142 v(t ) = A + B e t / 7.2 = v(0) = A + B e 0 for t > 0 7.2 = A + B B = 0.8 V  A = 8.0 V 8.0 = v() = A + B e 0.05 8  7.7728 7.7728 = v(0.05) = 8  0.8 e 0.05 /  = ln = 1.25878 0.8 0.05 = = 39.72 ms 1.25878 Therefore
v(t ) = 8  0.8 e t / 0.03972 for t > 0 1442 SP 143 i (t ) = A + B e t / 0 = i (0) = A + B e 0 4 103 = i () = A + B e  for t > 0 3 B = 4 10 A A  5106 / 0 = A+ B A = 4 103 2.4514 103 = v(5 106 ) = ( 4 103 )  ( 4 103 ) e  5 106 ( ) ( 4  2.4514 ) 103 = ln = 0.94894 4 103 = Therefore 5 106 = 5.269 s 0.94894
6 i (t ) = 4  4 e t / 5.26910 for t > 0 1443 SP 144
Make three copies of the circuit: one for each set of parameter values. (Cut and paste, but be sure to edit the labels of the parts so, for example, there is only one R1.) 1444 V(C1:2), V(C2:2) and V(C3:2) are the capacitor voltages, listed from top to bottom. 1445 SP 145
Make three copies of the circuit: one for each set of parameter values. (Cut and paste, but be sure to edit the labels of the parts so, for example, there is only one R1.) 1446 V(R2:2), V(R4:2) and V(R6:2) are the output voltages, listed from top to bottom. 1447 Verification Problems
VP 141 v L (t ) = 3 iC (t ) = d i L ( t ) = 6 e  2.1t  2 e 15.9 t dt 1 d v C ( t ) = 0.092 e  2.1t  0.575 e 15.9 t 75 dt v R1 ( t ) = 12  v L ( t ) = 12 + 6 e  2.1t + 2 e 15.9 t i R2 (t ) = 12  ( v L ( t ) + v C ( t ) ) 6 vC (t ) 6 = 1 + 0.456 e  2.1t  0.123 e 15.9 t i R3 (t ) = Thus, = 1 + 0.548 e  2.1t + 0.452 e 15.9 t 12 + v L ( t ) + v R1 ( t ) = 0 and i R 2 ( t ) = i C ( t ) +i R 3 ( t ) as required. The analysis is correct. 1448 VP 142 KVL for left mesh: KVL for right mesh: The analysis is correct. 18 20 and I 2 ( s ) = 3 3 s s 4 4 12 1 18 18 20 +  + 6 = 0 (ok) s 2s s  3 s  3 s  3 4 4 4 18 20 18 20 6  +3 4 = 0 (ok) 3 3 3 3 s s s s 4 4 4 4 I1 (s) = VP 143
Initial value of IL (s): lim s+2 s 2 = 1 (ok) s s +s+5 lim s+2 s 2 = 0 (ok) s0 s +s+5 lim 20 ( s + 2 ) s = 0 (not ok) s s ( s 2 + s + 5) lim 20 ( s + 2 ) s = 8 (not ok) s0 s ( s 2 + s + 5) Final value of IL (s): Initial value of VC (s): Final value of VC (s): 1449 Apparently the error occurred as VC (s) was calculated from IL (s). Indeed, it appears that VC (s) was calculated as  VC ( s ) =  20 20 8 I L ( s ) instead of  I L ( s ) + . After correcting this error s s s 20 s + 2 8 + . s s2 + s+5 s 20 ( s + 2 ) 8 s + = 8 (ok) s s ( s 2 + s + 5) s lim 20 ( s + 2 ) 8 + = 0 (ok) s s 0 s ( s 2 + s + 5) s lim Initial value of VC (s): Final value of VC (s): 1450 Design Problems
DP 141 Equating the Laplace transform of the step response of the give circuit to the Laplace transform of the given step response: kR 5 L = Vo ( s ) = 2 R 1 ( s + 4) s2 + s+ L LC Equating the poles: R 4 R   L L LC s 1,2 = = 4 0 2 Summarizing the results of these comparisons: R = 4, R = 2L 2 kR and =5 L LC
2 Pick L = 1 H, then k = 0.625 V/V, R = 8 and C = 0.0625 F. DP 142 Equating the Laplace transform of the step response of the give circuit to the Laplace transform of the given step response: 1451 kR 10 10 L Vo ( s ) = = = 2 2 R 1 ( s + 4 ) + 4 s + 8 s + 20 s2 + s+ L LC Equating coefficients: R 1 kR = 8, = 20, and = 10 L LC L Pick L = 1 H, then k = 1.25 V/V, R = 8 and C = 0.05 F. DP 143 Equating the Laplace transform of the step response of the give circuit to the Laplace transform of the given step response: kR 5 5 10 L Vo ( s ) = =  = 2 R 1 ( s + 2) ( s + 4) s + 6 s + 8 s2 + s+ L LC Equating coefficients: R 1 kR = 6, = 8, and = 10 L LC L Pick L = 1 H, then k = 1.667 V/V, R = 6 and C = 0.125 F. DP 144 1452 Comparing the Laplace transform of the step response of the give circuit to the Laplace transform of the given step response: kR 5 5 10 s + 30 L Vo ( s ) = + = 2 R 1 ( s + 2) ( s + 4) s + 6 s + 8 s2 + s+ L LC These two functions can not be made equal by any choice of k, R, C and L because the numerators have different forms. DP 145 a) Use voltage division to get
R2 Vo ( s ) = V1 ( s ) sC2 R 2 +1 R1 R2 + sC1 R1 +1 sC2 R 2 +1 1 s+ C1 R1 C1 = R1 + R2 C1 +C2 s + R1 R 2 ( C1 + C2 ) b) To make the natural response be zero, we eliminate the pole by causing it to cancel the zero.  R1 + R 2 1 = C1 R1 R1 R 2 (C1 +C2 ) C2 R1 = C1 R 2 1 c) Let v1 (t ) = u (t ) V1 ( s ) = . Then s 1 s+ R1C1 C1 K2 K1 Vo ( s ) = = s + R1 + R 2 C1 + C2 R1 + R 2 s s + s+ R1 R 2 (C1 +C2 ) R1 R 2 (C1 +C2 ) where K1 = Then R2 C R2 t 1 vo (t ) = +  e u (t ) R1 + R 2 C1 + C2 R 1 + R 2 R2 R1 + R 2 and K 2 = R2 C1  C1 + C2 R1 + R 2 1453 where = require R1 R 2 (C1 + C2 ) R1 + R 2 . To make the step response be proportional to the step in put, we R2 C1 = C1 + C2 R1 + R 2 Then vo (t ) = R2 R1 + R 2 u (t ) DP 146 The initial conditions are vc (0) = 0.4 V and i (0) = 0 A . Consider the circuit after t = 0. A source transformation yields The mesh equations are
8 0.4 8 2 + I1 ( s )  I 2 ( s ) = s s s 8 8  I1 ( s ) + Ls + I 2 ( s ) = 0 s s Solving for I 2 ( s ) yields I2 ( s ) = Therefore, the characteristic equation is 1.6 s ( Ls + 4 Ls +8)
2 s 2 + 4s + 8 =0 L We require complex roots with significant damping. Try L = 1 H. Then I ( s) = Finally i (t ) = 0.2  0.2e 2t cos 2t  0.4e2t sin 2t u ( t ) A 1.6 0.2 0.2( s + 4) 0.2 0.2( s + 2) 0.8 = + 2 = +  2 ( s + 2) + 4 ( s + 2) 2 + 4 s ( s + 4 s +8) s s + 4 s +8 s
2 1454 Chapter 15: Fourier Series
Exercises
Ex. 15.31 Notice that
f (t  T ) = f1 (t  T ) + f 2 (t  T ) = f1 (t ) + f 2 (t ) = f ( t ) Therefore, f(t) is a periodic function having the same period, T. Next
f ( t ) = k1 f1 ( t ) + k2 f 2 ( t ) = k1 a10 + ( a1n cos ( n 0 t ) + b1n sin ( n 0 t ) ) n =1 + k2 a20 + ( a2 n cos ( n 0 t ) + b2 n sin ( n 0 t ) ) n =1 = ( k1 a10 + k2 a20 ) + ( ( k1 a1n + k2 a2 n ) cos ( n 0 t ) + ( k1 b1n + k2 b2 n ) sin ( n 0 t ) )
n =1 Ex. 15.31 f(t) = K is a Fourier Series. The coefficients are a0 = K; an = bn = 0 for n 1. Ex. 15.32 f(t) = Acosw0t is a Fourier Series. a1 = A and all other coefficients are zero. 151 Ex. 15.41 2 T = 4 = , 0 = = 4 rad s T 8 2 Set origin at t = 0, so have an odd function; then an = 0 for n = 0,1, . . . Also, f(t) has half wave symmetry, so bn = 0 for n = even. For odd n, we have
bn = 2 T2 2 0 2 T2 T 2 f (t ) sin( n 0 t ) dt =  T T 2 sin( n 0 t ) dt + T 0 sin ( n 0 t ) dt T 4 T = 0 2 sin ( n 0 t ) dt T 4 4 (1cos( n 0 T )) = = n = 1, 3, 5, . . . 2 nf 0T n Finally, f (t ) =
N 1 sin n 0t; n n 4 n odd and 0 = 4 rad s Ex. 15.42 T = , 0 = 2 =2 T a0 = 0 , an = 0 for all n odd function with quarter wave symmety n = even bn = 0 2t 0<t < 6 8 4 bn = 0 f (t ) sin n 0t dt where f (t ) = 6 t < 2 6 4 24 1 n Thus bn = 2 2 sin n 3 24 N 1 n so f (t ) = 2 2 sin sin (2nt ) n =1 n 3 odd n 152 Ex. 15.43 a) is neither even nor odd. f(t) will contain both sine and cosine terms 1 b) wave symmetry no even harmonics 4 c) average value of f(t) = 0 a0 = 0 Ex. 15.51 T = 2 s, 0 = Cn = 2 = rad/s T  jn t 1 2 1 1  jn t 1 2 f (t )e dt = 0 e dt  1 e  jn t dt 2 0 2 2 1 1 e  jn +1+ e  j 2 n  e jn = (1 e jn ) = 2 jn jn 2 Cn = jn 0 Finally, f (t ) = 2 j n odd n even 1 1 j t 1 j 3 t 1 j 5 t e + e + e + ...  e  j t  e j 3 t  e j 5 t ... 3 5 3 5 Ex. 15.53
Cn = 1 T 4  j0nt 1 T  j 2 nt T T 4 e dt = T  j 2 n e T T 4 4 T = 1 e  j n / 2  e j n / 2  j 2 n (n 1) (1) 2 n Cn = 0 12 n odd n even , n 0 n =0 153 Ex. 15.61 Use the "stem plot" in Matlab to plot the required Fourier spectra:
% Fourier Spectrum of a Pulse Train A = 8; T = 4; d = T/8; pi = 3.14159; w0 = 2*pi/T; % pulse amplitude % period % pulse width %fundamental frequency N = 49; n = linspace(N,N,2*N+1); x = n*w0*d/2; % Eqn.15.63. Division by zero when n=0 causes Cn(N+1) to be NaN. Cn = (A*d/T)*sin(x)./x; Cn(N+1)=A*d/T; % Fix Cn(N+1); sin(0)/0 = 1 % Plot the spectrum using a stem plot stem(n,Cn,'filled'); xlabel('n'); ylabel('Cn'); title('Fourier Spectrum of Pules Train with d = T/8'); 154 Ex. 15.81 0 = 4 rad/s
From Example 15.41: vs (t ) = 3.24 N n =1 odd n 1 n sin n2 2 1 1 1 sin n 0t = 3.24 sin 4 t  sin12 t + sin 20 t  sin 28 t 9 25 49 The network function of the circuit is 1 1 j C = = Vs ( ) R + 1 1 + j C R 1 + j 4 j C Evaluating the network function at the frequencies of the input series 1 H ( n4 ) = n = 1,3,5... 1 + j 16 n n H(n4) 1 0.06286 3 0.02189 5 0.01289 7 0.000989 Using superposition 0.021 0.012 0.0009 vo (t ) = 3.24 ( 0.062 ) sin ( 4 t 86 ) sin (12 t 89 ) + sin ( 20 t 89 ) sin ( 28 t 89 ) 9 25 49 H ( ) = Vo ( ) 1 = vo (t ) = ( 0.2009 ) sin ( 4 t  86 )  (.00756 ) sin (12 t  89 ) + ( 0.00156 ) sin ( 20 t  89 )  ( 5.95 105 ) sin ( 28 t  89 ) Discarding the terms that are smaller than 25 of the fundamental term leaves
vo (t ) = ( 0.2009 ) sin ( 4 t  86 )  (.00756 ) sin (12 t  89 ) 155 Ex. 15.91
f (t ) = e  at u (t ) F ( ) = +  f (t ) e j t dt = e e
 at 0 j t e( ) 1 = dt =  ( a + j ) 0 a + j
 a + j t Ex. 15.101
F { f ( at )} =  f ( at ) e j t dt Let = at t =
F { f ( at )} = a  f ( ) e  j a d a = 1 1  j ( a ) d = F  f ( ) e a a a Ex. 15.102 f (t ) = 1 2 1 ( 2 ( ) A) e dt = 2 ( 2 ( ) A) dt = A j t
0+  0 Ex. 15.111
F 1 { (  0 )} = 1 2  (  0 ) e j t dt = Take the Fourier Transform of both sides to get: F e j0t = 2 (  0 ) ( 1 j0t e 2 ) e j0t + e  j0t F { A cos 0t} = F A 2 A A F e j0t + F e  j0t = ( 2 (  0 ) + 2 ( + 0 ) ) = 2 2 = A (  0 ) + A ( + 0 ) ( ( ) ( )) 156 Ex. 15.121
a)
Vin ( ) = 120 24 + j Vin ( ) = 1202 14400 = 2 2 24 + 576 + 2 b) Win = 1 0 14400 14000 1 1 d = 24 tan 24 = 300 J 2 576 + 0 14400 14000 1 1 d = 24 tan 24 = 61.3 J 2 576 + 24
48 Wout = = 1 48 24 Wout 61.3 100% = 100% = 20.5% Win 300 Ex. 15.131 f + ( t ) = te  at f  ( t ) = te at F + (s) =
Then F ( ) = F + ( s ) + F  (s) 1
2 f  ( t ) = te at and F  ( s ) =
1 +
s = j 1 (s + a)
s = j (s + a)
1
2 2 s = j = = (s + a)
1 2 (s + a)
1 s = j ( a + j ) 2  ( a  j ) 2 = (a  j 4a
2 +2 ) 2 157 Problems Section 15.3: The Fourier Series P15.31
T = 2 s 0 = 2 = rad/s and f (t ) = t 2 for 0 t 2 . The coefficients of the Fourier 2 series are given by:
a0 = 1 2 2 t dt = 4 3 2 0 2 2 4 an = 0 t 2 cos n t dt = 2 2 ( n ) bn = f (t ) = 4 2 2 2 0 t sin n t dt = n 2 4 4 N 1 4 1 + 2 2 cos n t  sin n t n =1 n 3 n =1 n 158 P15.32 an = T 2 2 2 T 4 2 0 cos n t dt + T 2 cos n t dt T T T 4 1 = n = 2 sin n T t T 4 0 T 2 2 + 2sin n t T T 4 1 n n (sin 2  0) + 2 (sin n ) sin 2 n (1) n +1 1 2 odd n n sin =  = n n 2 even n 0 bn = 2 2 sin n t dt T T T 1 2 4 2 2 cos n t + 2 cos n t =  n T 0 T T 4 n 1 = (2 cos (n ) 1)  cos 2 n 3 n is odd n 2 n = 2,6,10,... =  n n = 4,8,12,... 0 2 T 4 2 sin n T t dt + T 0 ( ) T 2 T 4 159 P15.33 a 0 = average value of f ( t ) = t f ( t ) = A 1  T
an = 2 T A 2 for 0 t T
1 T 2 t dt  t cos n T 0 T t dt T 0 t 2 A 1  cos n T T 2A T 2 t dt = 0 cos n T T T 2 2 2 cos n t+n t sin n t 2A 1 T T T = 2 0  T T 2 n T 0 A = 2 2 cos ( 2n )  cos ( 0 ) + 2n sin ( 2n )  0 2n =0 bn = 2 T T 0 t 2 A 1  sin n T T 2 A T 2 t dt = sin n T 0 T 1 T 2 t dt  t sin n 0 T T t dt T 2 2 2 tn t cos n t sin n 2A 1 T T T = 0 2 T T 2 n T 0 A = 2 2 ( sin ( 2n )  sin ( 0 ) )  ( 2n cos ( 2n )  0 ) 2n A = n f (t ) = A A 2 sin n + 2 n =1 n T t 1510 P15.34 T = 2 s, 0 = 2 = rad/s , a 0 = average value of f ( t ) = 1 , 2
f (t ) = t for 0 t 2
2 2 an = 2 2 0 t cos ( n t ) dt = = cos ( n t ) + ( n t ) sin ( n t ) ( n )
1
2 2 0 cos ( 2n )  cos ( 0 ) + 2n sin ( 2n )  0 n 2 2 =0 2 bn = 2 2 0 t sin ( n t ) dt = = sin ( n t )  ( n t ) cos ( n t ) (n )
1
2 2 0 ( sin ( 2n )  sin ( 0 ) )  ( 2n cos ( 2n )  0 ) n 2 2 = n
f (t ) = 1  n =1 2 2 sin n n T t Use Matlab to check this answer:
% P15.34 pi=3.14159; A=2; T=2; w0=2*pi/T; tf=2*T; dt=tf/200; t=0:dt:tf; a0=A/2; v1=0*t+a0; % input waveform parameters % period % % % % fundamental frequency, rad/s final time time increment time, s % avarage value of input % initialize input as vector Fourier series ... coefficients of the input for n=1:1:51 % for each term in the an=0; % specify series bn=A/pi/n; cn=sqrt(an*an + bn*bn); % convert thetan=atan2(bn,an); v1=v1+cn*cos(n*w0*t+thetan); % add the Fourier series end to magnitude and angle form next term of the input 1511 plot(t, v1,'black') grid xlabel('t, s') ylabel('f(t)') title('P15.34') % plot the Fourier series 1512 Section 154: Symmetry of the Function f(t)
2 = rad/s . 4 2 The coefficients of the Fourier series are: 15.41 T = 4 s o = a0 = average value of vd ( t ) = 0 an = 0 because vd(t) is an odd function of t.
bn = 1 4 0 ( 6  3 t ) sin n 2 t dt 2 4 3 4 = 3 sin n t dt  t sin n t dt 0 2 0 2 2  cos n 2 t 3 1  = 3 2 2 sin n t  n t cos n t 2 2 2 2n n 4 0 2 0 6 = ( 1 + cos ( 2n ) )  n26 2 ( sin ( 2n )  0 )  ( 2 n cos ( 2n ) ) n 12 = n
4 4 ( ) The Fourier series is:
vd ( t ) = n =1 12 sin n t n 2 P15.42
vc ( t ) = vd ( t  1)  6 = 6 + n =1 12 12 sin n ( t  1) = 6 + sin n t  n n 2 2 2 n =1 n 1513 P15.43 2 1000 = rad/s = krad/s .006 3 3 The coefficients of the Fourier series are: 3 2 1 V a0 = average value of va ( t ) = 2 = 6 2 bn = 0 because va(t) is an even function of t. T = 6 ms = 0.006 s o = 2 0.001 1000 an = 2 t dt 0 ( 3  3000 t ) cos n 3 0.006 0.001 1 1000 1000 t dt  ( 2 106 ) t cos n = 2000 cos n 0 0 3 3 1000 sin n 3 = 2000 n 1000 3 t  1000 n 2106 2 9 t dt 0.001 1000 1000 1000 t+n t sin n t cos n 3 3 3 0 3 9 = 2000 sin n 3  0  n 2103 2 cos n 3  1 + n 3 sin n 3  0 n1000 6 18 6 sin n  2 2 cos n  1  sin n = n 3 n 3 n 3 18 =  2 2 cos n  1 n 3 The Fourier series is va ( t ) = 1 18 n 1000 + 2 2 1  cos cos n 2 n =1 n 3 3 t P15.44
1 18 n vb ( t ) = va ( t  2 )  1 = 1 + + 2 2 1  cos cos n ( t  2 ) 2 n =1 n 3 3 1 18 n =  + 2 2 1  cos 2 n =1 n 3 2 1000 tn cos n 3 3 1514 P15.45 Choose t 0 =  T = 2 , 0 = 2 =1 2 average value: a0 = 0 2 T f ( t ) sin n 0 t dt T 0 an = 0 since have odd function 2 2 bn = f (t ) = t  < t < bn = t sin nt dt
 1 sin nt t cos nt = 2  n n  1 b1 = + = 2 1 1 b2 = 1 b3 = 2 3
P15.46 T = 8 s, 0 = 4 rad/s bn = 0 because f ( t ) is an even functon
a0 = average = ( 22 )  21 = 1 4
8 4 T2 f ( t ) cos n 0 t dt T 0 2 4 1 = 0 2 cos n t dt  1 cos n t dt 4 4 8 2 n n = 3 sin 4 sin 2 n a1 = .714, a2 = .955, a3 = .662 an = 1515 P15.47 0 = 2 , T = 2 2A a0 =  A cos t dt = 2
an = 2 2  2 A cos t cos 2n t dt 2 A sin ( 2n 1) t sin ( 2n +1) t 2 = + 2( 2n +1)  2( 2n 1) 2 sin 2n 1) sin ( 2n +1) 2A ( 2+ 2 = 2n +1 2n 1 2A = 2 ( 2n +1) sin ( 2n 1) 2 ( 2n 1) sin ( 2n 1) 2 ( 4n 1) = 4A cos( n ) ( 4n 2 1) = ( 4n 2 1) 4 A( 1) n bn = 0 due to symmetry P15.48 T = 0.4 s, 0 = 2 = 5 rad s T 0 t .1 A cos 0t .1 t < .3 f (t ) = 0 A cos t .3 t .4 0 Choose period  .1 t .3 for integral
a0 = 1 .1 A cos 0t = A T .1 2 .1 an = .1 A cos 0t cos n 0t dt T 1516 a1 = 5 A.1 cos 2 0t dt =
.1 .1 A 2 an = 5 A.1 cos 0t cos n 0t dt = 5 A.1 1 [ cos 5 (1+ n)t + cos 5 (1 n)t ] dt 2 2 A cos (n / 2) n 1 = 1 n 2 bn =0 because the function is even.
.1 P15.49 a0 = 0 because the average value is zero an = 0 because the function is odd bn = 0 for even due to 1 wave symmetry 4 Next: n 8 sin T 4 2 bn = T 4 t sin ( n 0 t ) dt = n 8  4n cos 2 2 2 = n n 2 2  8 n2 2 for n = 1,5,9, ... for n = 3, 7,11, ... Section 15.5: Exponential Form of the Fourier Series P15.51 T = 1 o = 2 = 2 , the coefficients of the complex Fourier series are given by: 1 1 e j t  e  j t  j 2 nt 1 1 Cn = A sin ( t ) e  j 2 nt dt = A dt e 0 1 0 2j A 1  j ( 2 n1) t  j ( 2 n+1) t e dt = e 2 j 0 ( ) 1  j 2 n 1) t  j 2 n +1) t Ae ( e ( 2 A =  = 2 2 j  j ( 2n  1)  j ( 2n + 1) 0 (4n  1) where we have used e j 2 n = 1 and e j = e j . 1517 P15.52 1 1 A  j Cn = t e T T 0 T Recall the formula for integrating by parts:
dv
2  j nt = e T dt . 2 nt dt =
t A T2 0 t e
t2 1 j 2 nt T dt t t2
1 u dv = u v t2  v du . Take u = t and
1 t1 When n 0 , we get 2 t e  j T nt A Cn = 2 T  j 2 n T T 2 nt T dt +
0 1 e 2 0 j n T
T T j 2  j nt  j 2 n AT e e T = + T  j 2 n 2 2 n j T 0  j 2 n AT e e  j 2 n  1 = + T  j 2 n 2 2 n j T A = j 2 n Now for n = 0 we have
C0 = 1 TA A 0 T t dt = 2 T
1 jn ne n =
n0 n = 2 t T Finally,
f (t ) = A A +j 2 2 1518 P15.53
A Cn = T
2  jn t d /2 T dt e d / 2  j n 2 t j n d  jn d T A e A e T e T = =  2 T  j n 2 T j n 2 jn T d / 2 T T d /2 jn d  jn d T e T A e = n 2j A n d = sin n T n d sin Ad T = T n d T P15.54 Cn =
Let = t  td , then t = + td .
Cn = 1 t0 +T ( a f ( t  td ) + b ) e j not dt T t0 1 T 1 = T t t
0 t0 +T td
d ( a f ( ) + b ) e j n ( +t )d
o d t t
0 t0 +T td
d ( a f ( ) + b ) e j n e j n t d
o o d e  j n o td = T t t
0 t0 +T td
d ( a f ( ) + b ) e j n d
o = a e  j n o td ( 1 )T t0 +T td t 0 t d f ( ) e  j n o d + e j n otd
t +T td ( 1 )T t0 +T td t0  t d b e j n o d But t t
0 t0 +T td
d be  j n o e  j no 0 d = b  j n o t t 0 d 0 n 0 so = b = 0 C0 = a C0 + b and C n = a e  j n o td C n n0 1519 P15.55
T = 8 s, 0 = 2 2  2 (1 1) 1 2 = rad/s, C 0 = average value = = T 4 8 4 The coefficients of the exponential Fourier series are calculated as
n n n t t t j j j 1 2 1 1 C n =  1 e 4 dt + 2 e 4 dt +  1 e 4 dt 1 1 8 2 1 1 2 n n n j j j t t t 4 4 4 1 e e e = 1 + 2 + ( 1) n n n 8 j j j 4 2 4 1 4 1 j = 2 n and C n n n n j n4 j j j  j n4  j n2 2 4 e +e e 4 e  e  2 e  n  n  n j t j t j t 1 2 1 1 4 4 =  1 e dt + 2 e dt +  1 e 4 dt 2 1 1 8 1 1 2 n n n j t j t j t 4 4 4 1 e e e = 1 + 2 + ( 1) n n n 8 j j j 4 2 4 1 4 1 = j 2 n n  j n4 j e 2 e n j j n  2 e 4 e 4 n j j n2 +e e 4 = C n The function is represented as f ( t ) = C0 + Cn e j n 0 t + C n e  j n 0 t
n =1 n =1  1520 This result can be checked using MATLAB:
pi = 3.14159; N=100; T = 8; t = linspace(0,2*T,200); c0 = 1/4; w0 = 2*pi/T; % % % % period time average value fundamental frequency for n = 1: N C(n) = j*((exp(+j*n*pi/4)exp(+j*n*pi/2))2*(exp(j*n*pi/4)exp(+j*n*pi/4))+(exp(j*n*pi/2)exp(j*n*pi/4)))/(2*pi*n); end for i=1:length(t) f(i)=c0; for n=1:length(C) f(i)=f(i)+C(n)*exp(j*n*w0*t(i))+C(n)*exp(j*n*w0*t(i)); end end plot(t,f,'black'); xlabel('t, sec'); ylabel('f(t)'); 1521 Alternately, this result can be checked using Mathcad:
N := 15 T := 8 d := T 200 C :=
n 1 n := 1 , 2 .. N := 2 T m := 1 , 2 .. N i := 1 , 2 .. 400 t := d i
i 1 2 2 1 exp( j n t ) dt + 1 2 exp( j n t) dt + 1 exp( j n t ) dt 1 T 1 1 exp( j m t ) dt + 1 2 exp( j m t) dt + T 2 1 exp( j m t ) dt C :=
m 2 1 1 f ( i) := n =1 N C exp j n t +
n i ( ) N C exp 1 j m t
m ( i )
C =
n m=1 C m = f ( i) =
1.643 1.685 1.745 1.807 1.856 1.88 1.872 1.831 1.767 1.693 1.628 1.589 1.589 1.633 1.717 1.825 2 0.357 0.477 0.331 0 0.357 0.477 0.331 0 0.199 0.159 0.051 0 0.04 0.095 0.09 0 0.076 0.068 0.024 f ( i) 0 0.199 0.159 0.051 0 100 200 i 300 400 0.04 0.095 0.09 0 0.076 0.068 0.024 2 1522 P15.56 The function shown at right is related to the given function by v ( t ) = v1 ( t + 1)  6 (Multiply by 1 to flip v1 upsidedown; subtract 6 to fix the average value; replace t by t+1 to shift to the left by 1 s.) From Table 15.51 v1 ( t ) = n = j A ( 1) j n 0 t j 6 ( 1) j n t e = e 2 n n n = n n Therefore v ( t ) = 6 
n = n n j 6 ( 1) j n (t +1) j 6 ( 1) j n j n t 2 e e 2 e 2 = 6  n n n = The coefficients of this series are: j 6 ( 1) j n C0 = 6 and Cn =  e 2 n This result can be checked using Matlab:
n pi = 3.14159; N=100; A = 6; T = 4; t = linspace(0,2*T,200); c0 = 6; w0 = 2*pi/T; % amplitude % period % time % average value % fundamental frequency for n = 1: N C(n) = (j*A*(1)^n/n/pi)*exp(+j*n*pi/2); D(n) = (+j*A*(1)^n/n/pi)*exp(j*n*pi/2); end for i=1:length(t) f(i)=c0; for n=1:length(C) f(i)=f(i)+C(n)*exp(j*n*w0*t(i))+D(n)*exp(j*n*w0*t(i)); end end plot(t,f,'black'); xlabel('t, sec'); ylabel('f(t)'); title('p15.56') 1523 1524 P15.57 Represent the function as 1  e 5 t 0 t 1 f ( t ) = 5 ( t 1) 5 1 t 2 e e (Check: f ( 0 ) = 0,
f (1) = 1  e 5 1, f ( 2 ) = e5  e 5 = 0 ) T = 2 s, 0 = 2 1 = , also C0 = average value = 2 2 The coefficients of the exponential Fourier series are calculated as
Cn =
2 1 1 5 ( t 1) 5 t  j n t 5  j n t 0 (1  e ) e dt + 1 e  e e dt 2 1 1 2  5+ j n t 2 1 ) dt  e 5 e j n t dt = e  j n t dt  e 5 t e  j n t dt + e5 e ( 0 1 1 2 0 1 2 1 2  5+ j n ) t ( 5+ j n ) t 1 e j n t e( e  j n t + e5 e =   e 5 2  j n 0  ( 5 + j n ) 0  ( 5 + j n ) 1  j n 1 ( ) ( )( ) =  5+ j n ) 2  5+ j n ) 1 e  j n  1 e 5 e  j n  1 5 e ( e ( e j n 2  e j n   e 5 +e 2  j n  (5 + j n )  (5 + j n )  j n  j n 2 1 e  j n  1 e 5 e  j n  1 e5 e j 2 n  e j n  e  j n 5 e =  e + 2  j n  (5 + j n )  (5 + j n )  j n n n n n 5 5 1 ( 1)  1 e ( 1)  1 e  ( 1) 5 1  ( 1) =  e + 2  j n  (5 + j n )  (5 + j n )  j n The terms that include the factor e 5 = 0.00674 are small and can be ignored.
n  ( 1)n 1 ( 1)  1 1 C n =  + 2  j n  (5 + j n )  (5 + j n ) 1 1 odd n  = j n 5 + j n 0 even n 5 j n 5 + j n )( ) = ( 0 odd n even n 1525 This result can be checked using Matlab:
pi = 3.14159; N=101; T = 2; t = linspace(0,2*T,200); c0 = 0.5; w0 = 2*pi/T; % period % time % average value % fundamental frequency for n = 1:2:N if n == 2*(n/2) C(n) = 5/((+j*pi*n)*(5+j*pi*n)); D(n) = 5/((j*pi*n)*(5j*pi*n)); else C(n)=0; D(n)=0 end end for i=1:length(t) f(i)=c0; for n=1:length(C) f(i)=f(i)+C(n)*exp(j*n*w0*t(i))+D(n)*exp(j*n*w0*t(i)); end end plot(t,f,'black'); xlabel('t, sec'); ylabel('f(t)'); title('p15.57') 1526 Section 156: The Fourier Spectrum P15.61 Average value = 0 a0 = 0 half  wave symmetry 4 T 2 4A 4A 2 an = T 0  T t cos n T t dt =  2 2 (cos (n ) 1) n f (t ) T bn = 4 0 2  4 A t sin n 2 t dt =  2 A (1 cos ( n ) ) T n T T n Cn = a n + bn 1 1.509 A 2 0 3 0.434 A 4 0 5 0.257 A 6 0 7 0.183 A 2 2 n = tan 1 57.5 0 78.0 0 82.7 0 84.8 bn an 1527 P15.62 Mathcad spreadsheet (p15_6_2.mcd):
N := 100 n := 1 , 2 .. N T := 32 0 := 2 T Calculate the coefficients of the exponential Fourier series:
T T 4 4 C1 := n T 3 T 16 t  3 exp( j n 0 t) dt T 2 4 2 t exp( j n 0 t) dt C2 := sin n T T T 4 16 3 T 4 4 C3 := n T 11 T
n n n 11  16 t exp( j n 0 t) dt T 4 2 t exp( j n 0 t) dt C4 := sin n T T T 3
4 T 16 n n C := C1 + C2 + C3 + C4 Check: Plot the function using it's exponential Fourier series: T 200 d := i := 1 , 2 .. 400 t := d i
i f ( i) := n =1 N C exp j n 0 t +
n ( i) N C exp j n 0 t
n ( i ) n =1 5 f ( i) 0 5 10 20 30 ti 40 50 60 1528 Plot the magnitude spectrum:
1.5 1 Cn 0.5 0 1 2 3 4 5 n 6 7 8 9 10 That's not a very nice plot. Here are the values of the coefficients:
C
n =
1.385 0 0.589 0 0.195 0 0.139 0 0.082 0 0.039 0 0.027 arg C ( n) 180 = 115.853 90 22.197 24.775 113.34 106.837 66.392 78.232 69.062 48.814 109.584 90.415 25.598 78.14 63.432 163.724 0 1.22610 3 0 1529 P15.63 Use Euler's formula to convert the trigonometric series of the input to an exponential series: vi ( t ) = 10 cos t + 10 cos 10 t + 10 cos 100 t V et + et e10 t + e10 t e100 t + e100 t = 10 + 10 + 10 2 2 2 100 t 10 t t 10 t t = 5e + 5 e + 5 e + 5 e + 5 e + 5 e100 t The corresponding Fourier spectrum is: Evaluating the network function at the frequencies of the input: , rad/s
1 10 100 Using superposition: H() 1.923 0.400 0.005 H(), 23 127 174 vo ( t ) = 19.23 cos ( t  23 ) + 4.0 cos (10 t  127 ) + 0.05 cos (100 t  174 ) V Use Euler's formula to convert the trigonometric series of the output to an exponential series:
) ) ) ) +e ( ) e ( +e ( e ( +e ( vo ( t ) = 19.23 + 4.0 + 0.05 V 2 2 2 =19.23e j 174e  j t + 4.0 e j 127 e  j 10 t + 19.23e j 23 e  j t + 19.23e j 23 e j t + 4.0 e  j 127 e j 10 t 19.23e j 174 e j t e j ( t  23 )  j t  23 j 10 t 127  j 10 t 127 j 100 t 174  j 100 t 174 1530 P15.64 T = 1 s, 0 = 2 1 = 2 rad/s, C 0 = T 2 f (t ) = 1 t when 0 t < 1 s The coefficients of the exponential Fourier series are given by
Cn =
1 1 1 1  j 2 nt dt = e  j 2 nt dt  t e  j 2 nt dt 0 (1  t ) e 0 0 1 Evaluate the first integral as 1  j 2 nt e 0 e j 2 nt dt =  j 2 n 1 =
0 e  j 2 n  1 =0  j 2 n To evaluate the second integral, recall the formula for integrating by parts: t t2
1 u dv = u v t2  v du . Take u = t and dv = e  j 2 nt dt . Then
t
1 t2 t1 0 t e 1  j 2 nt t e j 2 nt dt =  j 2 n 1 +
0 1  j 2 nt 1 dt 0 e j 2 n 1 e  j 2 n e  j 2 nt = +  j 2 n ( j 2 n )2 Therefore =
0 e  j 2 n e  j 2 n  1 1 + = j 2 2 n  j 2 n ( j 2 n ) 1 2 Cn = j 2 n n=0 n0 To check these coefficients, represent the function by it's Fourier series: 1 n=  j j 2 nt j  j 2 nt f (t ) = + e e + 2 n=1 2 n 2 n Next, use Matlab to plot the function from its Fourier seris (p15_6_4check.m):
pi = 3.14159; N=20; T = 1; t = linspace(0,2*T,200); % period % time 1531 c0 = 1/2; w0 = 2*pi/T; % average value % fundamental frequency for n = 1: N C(n) = j/(2*pi*n); end for i=1:length(t) f(i)=c0; for n=1:length(C) f(i)=f(i)+C(n)*exp(j*n*w0*t(i))C(n)*exp(j*n*w0*t(i)); end end plot(t,f,'black'); xlabel('t, sec'); ylabel('f(t)'); This plot agrees with the given function, so we are confident that the coefficients are correct. The magnitudes of the coefficients of the exponential Fourier series are: 1 2 Cn = 1 2 n n=0 n0 Finally, use the "stemplot" in Matlab to plot the Fourier spectrum (p15_6_4spectrum.m):
pi = 3.14159; N=20; n = linspace(N,N,2*N+1); Cn = abs(1/(2*pi)./n); % Division by 0 when n=0 causes Cn(N+1)= NaN. 1532 Cn(N+1)=1/2; % Fix Cn(N+1); C0=1/2 % Plot the spectrum using a stem plot stem(n,Cn,'*k'); xlabel('n'); ylabel('Cn'); 1533 Section 15.8: Circuits and Fourier Series P15.81 The network function of the circuit is: 100 Vo ( ) 1 j H ( ) = = = 100 Vi ( ) 10 + 1+ j j 10 Evaluating the network function at the harmonic frequencies: 1 20 20 n = =  tan 1 Hn = 2 1 + j n 20 + j n 20 400 + n 2 2 20 From problem 15.42, the Fourier series of the input voltage is
vc ( t ) = 6 + n =1 12 sin n t  n n 2 2 Using superposition, the Fourier series of the output voltage is vo ( t ) = 6 + n =1 n sin n t  n + tan 1 20 n 400 + n 2 2 2 2 240 P15.82 The network function of the circuit is: R2 H ( ) = j C1 R 2 1 + j C2 R 2 Vo ( ) = = 1 Vi ( ) (1 + j C1R1 )(1 + j C2 R 2 ) R1 + j C1 =
6 (1 + j (10 ) (1000) ) (1 + j (10 ) ( 2000 ))
6 j (106 ) ( 2000 ) = 500 1 + j 1 + j 1000 500 j Evaluating the network function at the harmonic frequencies: 1534 2 1000 3 Hn = 2 3 1 + j n 1 + j n 3 3 From problem 15.44, the Fourier series of the input voltage is jn 1 18 2 n 1000 vb ( t ) =  + 2 2 1  cos tn cos n 2 n =1 n 3 3 3 Using superposition, the Fourier series of the output voltage is 1000 18 H n 3 1 2 1000 n 1000 vb ( t ) =  + 1  cos 3 cos n 3 t  n 3 + H n 3 2 2 2 n =1 n P15.83
H ( ) = Vo ( ) Ho = Vi ( ) 1 + j p When = 0 (dc) 5 =  When = 100 rad/s R ( 2 ) R = 25 k 104 135 = H ( ) = 180  tan 1 ( C R ) tan ( 45 ) = (100 ) C ( 25000 ) C = 0.4 F 25000 104 = 3.032 c4 = ( 5 ) H ( 400 ) = ( 5 ) 1 + j ( 400 ) ( 0.4 106 ) ( 25000 ) 4 = 45 + H ( 400 ) = 45 + 180  tan 1 ( 400 0.4 106 25000 ) = 149 1535 P15.84 When = 0 (dc) When = 25 rad/s 5 = H o ( 2 ) H o = 2.5 V/V 25 45 = H ( ) =  tan 1 tan ( 45 ) = p p
c4 = ( 5 ) H (100 ) = ( 5 ) p = 25 rad/s 2.5 = 3.03 100 1+ j 25 100 4 = 45 + H (100 ) = 45  tan 1 = 31 25 P15.85
H ( ) = R2 Vo ( ) = Vi ( ) R1 + R 2 + j C R1 R 2 When = 0 (dc) R2
R1 + R 2 When = 1000 rad/s = 3.75 2.25 2.25 R1 = R2 = (500) = 300 6 3.75 3.75 R1 R 2 ( 300 )( 500 ) 20.5 = H ( ) =  tan 1 C tan ( 20.5 ) = (1000 ) C R1 + R 2 800 C = 2 F 500 ( 545 ) = 2.076  3.4 c3 3 = 800 + j ( 3000 ) ( 2 106 ) ( 500 )( 300 ) 1536 P15.86 ^ Rather than find the Fourier Series of v(t ) directly, consider the signal v(t ) shown above. These two signals are related by ^ v(t ) = v (t  1)  6 since v(t ) is delayed by 1 ms and shifted down by 6 V. ^ The Fourier series of v (t ) is obtained as follows: T = 4 ms 0 = 2 radians = rad/ms 4 ms 2 ^ ^ a n = 0 because the average value of v (t ) = 0 1 4 ^ ^ bn = 0 ( 63t ) sin n t dt because v (t ) is an odd function. 2 2 3 4 4 = 30 sin n t dt  0 t sin n t dt 2 2 2 4 1 n 3  sin n t  t cos n t 2 n 2 2 2 2 2 0 n 4 2 0 6 12 = ( 1+ cos( 2n ) )  n26 2 ( sin ( 2n )  0 )  ( 2n cos( 2 )  0 ) = n n  cos n t 2 =3
4 ( ) Finally, ^ v (t ) = 12 sin n t n =1 n 2 ^ The Fourier series of v (t ) is obtained from the Fourier series of v (t ) as follows: v(t ) =  6 + 12 12 sin n ( t 1) =  6 + sin n t  n n =1 n 2 2 2 n =1 n where t is in ms. Equivalently, 1537 v(t ) =  6 + where t is in s. 12 1 3 sin n 10 t  n n =1 n 2 2 R s L Next, the transfer function of the circuit is H ( s ) = = . 1 1 2 R + Ls + R s + s+ Cs L LC R j 104 j L The network function of the circuit is H ( ) = = . R 1 2 (108  2 ) + 104 j  + j L LC We see that H(0) = 0 and R
j 20n H ( n 0 ) = H n 103 = = 2 2 2 ( 400  n ) + j 20n 1 e
20 n j 90  tan 1 400  n 2 2 ( 400n )
2 2 2 + 400n 2 2 Finally, v0 ( t ) = 12 n =1 20n sin n 103 t  n + 90  tan 1 2 2 2 400  n 2 n ( 400n )
2 2 2 + 400n 2 2 1538 P15.87 ^ Rather than find the Fourier Series of v(t ) directly, consider the signal v(t ) shown below. ^ These two signals are related by v(t ) = v ( t  2 )  1 ^ Let's calculate the Fourier Series of v (t ), taking advantage of its symmetry. 2 rad = rad ms 6 ms 3 3.2 1 ^ ao = average value of v(t ) = 2 = V 6 2 ^ bn = 0 because v(t ) is an even function T = 6 ms 0 = 2 1 an = 2 0 ( 33t ) cos n t dt 3 6 an = 20 cos n t dt  20 t cos n t dt 3 3 sin n 3 1 = 2 n 2 2 n 3 9 = so ^ v(t ) = 1 18 1 cos n cos n t + 2 2 2 n =1 n 3 3 n 1 18 1 cos + 2 2 2 n =1 n 3 2 cos n t  n 3 3
1539
1 1 cos n t + n t sin n t 3 3 3 0 1 18 6 6 18 sin n  2 2 cos n 1 + sin n =  2 2 cos n 1 3 n 3 n 3 3 n n ^ v ( t ) = v ( t  2 ) 1 =  where t is in ms. Equivalently,
1 18 n v(t ) =  + 2 2 1 cos 2 n =1 n 3 2 3 cos n 10 t  n 3 3 where t is in s. The network function of the circuit is: R2  j C1 R2 1+ j C2 R2 = H ( ) = 1 (1+ j R1C1 )(1+ j R2C2 ) R1 + j C1 Evaluate the network function at the harmonic frequencies of the input to get. 3 H ( n 0 ) = H n 103 = 3 1+ jn 1+ jn 2 3 3 The gain and phase shift are  jn H( n 0 ) H( n 0 ) The output voltage is v0 ( t ) = n 3 = 2 2 2 2 n 4n (9+ n )( 9+ 4n2 2 ) 1+ 1+ 9 9 2 = 90  tan 1 n + tan 1 n 3 3 =
2 2 n n 181cos 3 n =1 2 2 3  90  tan 1 n  tan 1 n cos n 10 t  n 3 3 3 3 2 2 2 2 2 2 n ( 9+ n )( 9 + 4n ) At t = 4 ms =0.004 s
n 2 4 1 1 2 181 cos cos n  n  90  tan n  tan n 3 3 3 3 3 = 2 2 2 2 2 2 n =1 n ( 9 + n )( 9 + 4n ) v0 (.004 ) 1540 Section 15.9 The Fourier Transform P15.91 Let g ( t ) = e  at u ( t )  e at u ( t ) . Notice that f ( t ) = lim g ( t ) . Next
a 0 G ( ) = e e
0  at  j t dt  e e
 0 at  j t e ( a + j )t e( a  j ) t dt =   ( a + j ) 0 ( a  j )  2 j 1 1 = 0  0 = 2  a +2  ( a + j ) ( a  j ) 0 Finally F ( ) = lim G ( ) = lim
a 0 a 0 2 j 2 = 2 2 a + j P15.92
F ( ) = Ae u ( t ) e
 at   j t dt = Ae e
0  at  j t Ae  ( a + j ) t A A = 0 = dt =  ( a + j ) 0  ( a + j ) a + j P15.93 First notice that 2 AT T 2 T  AT 2 T Sa Then, from line 6 of Table 15.102: F { f1( t )} =  = Sa 2 2 4 4 4 AT 2 2 T d From line 7 of Table 15.102: F { f ( t )} = F f1( t ) = j F { f1( t )} =  j Sa 4 dt 4 2 T 2 sin AT 4 = 4 A sin 2 T This can be written as: F { f ( t )} =  j 2 4 j 4 T 4 1541 P15.94 First notice that: F 1  Therefore F {10 cos 50t} = F {5 e j 50t } + F {5 e  j 50t } = 10 (  50) + 10 ( + 50) . Therefore F e  j0t = 2 (  0 ) . Next, 10 cos 50t = 5 e j 50t + 5 e  j 50t . { } {( 1 1  j t = (  ) e d = e 0 )} 2 0 2   j t 0 P15.95
F ( ) = 2 e
1 2  j t 2e  j t dt =  j 2 =
1 2  j 2  j ( e  e ) = j2 ( ( cos 2  j sin 2 )  ( cos  j sin ) ) j = 2j ( cos  cos 2 ) + ( sin  sin 2 ) 2 P15.96
F ( ) = B
0 A  j t A e  j t A e  j B 1 t e dt = j B  1)  2  j t  1) = 2 ( 2 ( B B (  j ) 0 B  =
A  Be  j B e j B 1 + 2  2 B j B P15.97
F ( ) = e
2 2  j t dt  e
1 1  j t e  j t dt =  j e j t   j 2 2 1 =
1 1 ( e j 2  e j 2 )  j1 ( e j  e j ) j 2 = P15.121 ( sin 2  sin ) is ( t ) = 40 signum ( t ) 2 80 I s ( ) = 40 = j j I ( ) 1 = H ( ) = I s ( ) 4 + j
I ( ) = H ( ) I s ( ) = 1 80 20 20 =  4 + j j j 4 + j i ( t ) = 10 signum ( t )  20 e 4t u ( t ) 1542 P15.122 is ( t ) = 100 cos 3t A I s ( ) = 100 (  3) + ( + 3) I ( ) 1 H ( ) = = I s ( ) 4 + j (  3 ) + ( + 3 ) I ( ) = 100 4 + j e  j 3t 100 (  3) + ( + 3) j t e j 3t + i (t ) = e d = 50 2  4 + j 4  j3 4 + j3 = 10 e  j ( 3t 36.9 ) +e j ( 3t 36.9 ) = 10 cos ( 3t  36.9 ) P15.123 v ( t ) = 10 cos 2t V ( ) = 10 ( + 2 ) + (  2 ) 1 Y ( ) = 2 + j I ( ) = Y ( ) V ( ) = 10 ( + 2 ) + (  2 ) 2 + j i (t ) = 10 2 ( + 2 ) + (  2 ) j t e  j 2t e j 2t + e d = 5  2 + j 2  j2 2 + j2 = 5 e  j ( 2 t  45 ) +e j ( 2 t  45) = 5 cos ( 2t  45 ) A 1543 P15.124 v ( t ) = e t u ( t ) + u ( t )
F {e u ( t )} = e u ( t ) e
t t  j t  dt = e e
 0 t  j t e( ) dt = 1  j
1 j t 0 =
 1 1  j F {u ( t )} = ( ) + 1 j V ( ) = 1 1 + ( ) + j 1  j 1 1 1 1 1 2 + j 2 j , H ( ) = = = 1 1 1 2 + j 3 + j 1+ + 2 j 2 + j 1 1 1  1 1 1 3 ( ) 12 4 Vo ( ) = 1  j + ( ) + j = 3 + j + 1  j + j + 3 + j 3 + j ( ) 1 ( )  j t 1 F 1 =  3 + j e d = 6 3 + j 2 vo ( t ) =  1 3t 1 1 1 e u ( t ) + et u ( t ) + signum ( t ) + 12 4 3 6 P15.125
vs ( t ) = 15e5t u ( t ) V V ( ) = Ws = 5t 2 5t 2  0 15 5 + j J (15e u ( t ) ) dt = (15e ) dt = 22.5 1 1 j C H ( ) = = RC 1 1 R+ + j j C RC C =10 F. Try R =10 k. Then 10 15 Vo ( ) = 10 + j 5 + j Wo = 1 0 10 15 1 d = 10 + j 5 + j 2 0 300 300 d = 15 J  2 2 25 + 100 + 2 1544 P15.126
H ( ) = 4 4 + j 8 8  j Vs ( ) = F {8u ( t )  8u ( t  1)} = 8 ( ) +  8 ( ) + e j j 8 Vs ( ) = (1  e j ) since ( ) e j = ( ) j Vo ( ) = 4 8 (1  e j ) = j8  4 +8j  j8  4 +8j e j 4 + j j Next use 1 1 = + ( )  ( ) to write j j 1 8 1 8  j Vo ( ) = 8 + ( )  ( )  + ( )  ( )   8 e 4 + j j 4 + j j 1 8 1 8  j = 8 + ( )  + ( )   8 e 4 + j j 4 + j j vo ( t ) = 8u ( t )  8e 4t u ( t )  8u ( t  1)  8e = 8(1  e 4t )u ( t )  8(1  e
4( t 1) ( 4( t 1) u ( t  1) ) )u ( t  1) V 1545 PSpice Problems
SP 151
Vin R1 .tran .four .probe .end 1 1 0 0 pulse 1 (25 5 0 0 0 4 5) 0.01 5 0.2 v(1) FOURIER COMPONENTS OF TRANSIENT RESPONSE V(1) DC COMPONENT = HARMONIC NO 1 2 3 4 5 6 7 8 9 8.960000E+00 FOURIER COMPONENT 7.419E+00 6.030E+00 4.061E+00 1.935E+00 8.000E02 1.182E+00 1.704E+00 1.537E+00 8.954E01 NORMALIZED COMPONENT 1.000E+00 8.127E01 5.473E01 2.609E01 1.078E02 1.593E01 2.297E01 2.072E01 1.207E01 PHASE (DEG) 1.253E+02 1.606E+02 1.642E+02 1.289E+02 9.360E+01 1.217E+02 1.570E+02 1.678E+02 1.325E+02 NORMALIZED PHASE(DEG) 0.000E+00 3.528E+01 2.894E+02 2.542E+02 2.189E+02 3.600E+00 3.168E+01 2.930E+02 2.578E+02 FREQUENCY (HZ) 2.000E01 4.000E01 6.000E01 8.000E01 1.000E+00 1.200E+00 1.400E+00 1.600E+00 1.800E+00 SP 152
Vin R1 .tran .four .probe .end 1 1 0 0 0.1 1 1 v(1) pulse (1 1 0.5 1 0 0 1) 1 FOURIER COMPONENTS OF TRANSIENT RESPONSE V(1) DC COMPONENT = HARMONIC NO 1 2 3 4 5 6 7 8 9 FREQUENCY (HZ) 1.000E+00 2.000E+00 3.000E+00 4.000E+00 5.000E+00 6.000E+00 7.000E+00 8.000E+00 9.000E+00 1.299437E02 FOURIER COMPONENT 6.364E01 3.180E01 2.117E01 1.585E01 1.264E01 1.051E01 8.972E02 7.817E02 6.916E02 NORMALIZED COMPONENT 1.000E+00 4.996E01 3.326E01 2.490E01 1.987E01 1.651E01 1.410E01 1.228E01 1.087E01 PHASE (DEG) 1.777E+02 4.679E+00 1.730E+02 9.366E+00 1.683E+02 1.407E+01 1.636E+02 1.880E+01 1.588E+02 NORMALIZED PHASE (DEG) 0.000E+00 1.823E+02 4.682E+00 1.870E+02 9.376E+00 1.917E+02 1.409E+01 1.965E+02 1.883E+01 Verification Problems 1546 VP 151
t f (t ) = 2 + cos a0 = 2 , a1 = 1 and all other coefficients are zero. 2 The computer printout is correct. VP 152
Table 15.42 shows that the average value of a full wave rectified sinewave is 2A 2(400) where A is the amplitude of the sinewave. In this case a0 = = 255. Unfortunately the report says, "halfwave rectified." The report is not correct. Design Problems
DP 151
For sinusoidal analysis, shift horizontal axis to average, which is 6 V. Now we have an odd function so an = 0 T = s , 0 = 2 / = 2 rad/s 22 T / 2 f (t ) sin n 0t dt T 0 Need third harmonic : 4 4 /2 /2 b3 = 0 sin 6t dt =  cos 6t 0 = 0.424 6 T v1 ( t ) = 0.424sin ( 6t ) =0.424 cos(6t 90) V V1 ( ) = 0.42490 bn = Zc = j j = for third harmonic C 6C 16 16 
0 transfer function is H (3 0 ) = V2 ( ) = H ( 3 0 ) V1 ( ) = j 6C ( H(3 ) H (3 0 ) ) (0.42490 ) Choose V2 ( ) = 1.36 so H ( 3 0 ) = 3.2 This requires C = 1 16 = 3.264.9 F. Then H ( 3 0 ) = 205 16 j 34 third harmonic of v2 ( t ) = 1.36sin(6t + 64.9 ) V 1547 DP 152 Refer to Table 15.42. 2A N 4A 1  v (t ) = cos(2n0t ) s n = 1 4n 2  1 In our case: 360 N 640 1 v (t ) =  cos(2n377t ) s n = 1 4n 2  1 Let vs (t ) = vs0 + vsn (t ) and v0 (t ) = vo0 + von (t )
n =1 n =1 N N We require ripple 0.04 dc output max von (t )
n =1 ( N ) 0.04 v o0 vo1 (t ) 0.04 vo0 but vo0 = vs0 because the inductor acts like a short at dc. R Next, using the network function of the circuit gives Von = Vsn . R + j 0 n L For n=1:
Vo1 =
R 1 640 1 640 so V01 = Vs1 = Vs1 , but Vs1 = R + j 0 L 1+ j 377 L 1+ j 377 L 3 (3) We require Vo1 0.04 vo0 and vo0 = vs0 =
Solving for L yields L > 1.54 mH 360 . Then 1 1+ (377) 2 L 2 640 360 0.04 3 1548 DP 153 From Table 15.51, the Fourier series can represent the input to the circuit as:
vs ( t ) = 1 + j j 0 t j j 0 t 1 + e + e e j n 0 t 2 4 4 even n = 2 (1  n ) The transfer function of the circuit is calculated as Vo1 = So 1 LC Zp R Vs1 where Z p = Z L +Z p 1+ j RC Vo = = 1 1 Vs + ( j ) 2 + ( j ) RC LC The gain at dc, = 0 , is 1 so 1 v =v =
o0 s0 For n = 1 Vo1 = 1 1 1 vo0 = vs0 = 20 20 20 1/ LC =
2 4 + 1 + RC LC 2 1 20 We are given =800 and R =75 k. Choosing L =0.1 mH yields C =0.1 F 1549 Chapter 16: Filter Circuits
Exercises
Ex. 16.31 Tn ( s ) = 1 s +1 s T ( s ) = Tn = 1250 1 1250 = s s +1250 +1 1250 Problems
Section 16.3: Filters P16.31 Equation 163.2 and Table 163.2 provide a thirdorder Butterworth lowpass filter having a cutoff frequency equal to 1 rad/s. 1 H n (s) = ( s +1)( s 2 + s +1) Frequency scaling so that c = 2 100=628 rad/s : H L ( s) = 1
2 s s s +1 +1 + 628 628 628 = 6283 247673152 = 2 2 ( s + 628)( s + 628s + 628 ) ( s + 628)( s 2 + 628s + 394384) P16.32 Equation 163.2 and Table 163.2 provide a thirdorder Butterworth lowpass filter having a cutoff frequency equal to 1 rad/s and a dc gain equal to 1. H n (s) = 1 ( s + 1)( s 2 + s + 1) Multiplying by 5 to change the dc gain to 5 and frequency scaling to change the cutoff frequency to c = 100 rad/s: H L ( s) = 5 s +1 100 s 2 s +1 + 100 100 = 51003 5000000 = 2 2 ( s +100)( s +100s +100 ) ( s +100)( s 2 +100 s +10000) 161 P16.33 Use Table 163.2 to obtain the transfer function of a thirdorder Butterworth highpass filter having a cutoff frequency equal to 1 rad/s and a dc gain equal to 5.
5 s3 H n ( s) = ( s +1) ( s 2 + s +1) Frequency scaling to change the cutoff frequency to c = 100 rad/s s 5 5s 3 5s 3 100 = = H H ( s) = 2 ( s +100)( s 2 +100 s +1002 ) ( s +100)( s 2 +100s +10000) s s s +1 +1 + 100 100 100 3 P16.34 Use Table 163.2 to obtain the transfer function of a fourthorder Butterworth highpass filter having a cutoff frequency equal to 1 rad/s and a dc gain equal to 5. H n (s) = 5s 4 ( s 2 +0.765s +1) ( s 2 +1.848s +1) Frequency scaling can be used to adjust the cutoff frequency 500 hertz = 3142 rad/s: s 5 3142 HH (s) = 2 s 2 s s s + 0.765 +1 +1.848 +1 3142 3142 3142 3142 = 5s 4 ( s 2 + 2403.6s +31422 ) ( s 2 +5806.4s +31422 )
4 162 P16.35 First, obtain the transfer function of a secondorder Butterworth lowpass filter having a dc gain equal to 2 and a cutoff frequency equal to 2000 rad/s: HL (s) = 2 s s +1.414 +1 2000 2000 2 = 8000000 s + 2828s + 4000000
2 Next, obtain the transfer function of a secondorder Butterworth highpass filter having a passband gain equal to 2 and a cutoff frequency equal to 100 rad/s: HH (s) s 2 2s 2 100 = = 2 2 s +141.4 s +10000 s s +1.414 +1 100 100 2 Finally, the transfer function of the bandpass filter is HB (s) = HL (s) H
P16.36 s H( ) = 16000000s 2 ( s 2 +141.4s +10000 ) ( s 2 + 2828s + 4000000 ) 250 s 250000 s 2 1 HB (s) = 4 = 2 2 250 s2 + s + 2502 ( s + 250 s + 62500 ) 1
2 P16.37 First, obtain the transfer function of a secondorder Butterworth highpass filter having a dc gain equal to 2 and a cutoff frequency equal to 2000 rad/s: s 2 2 s2 2000 HL (s) = = 2 2 s + 2828 s + 4000000 s s +1.414 +1 2000 2000 Next, obtain the transfer function of a secondorder Butterworth lowpass filter having a passband gain equal to 2 and a cutoff frequency equal to 100 rad/s: 2 163 HH (s) = 2 s s +1.414 +1 100 100 2 = 20000 s +141.4 s +10000
2 Finally, the transfer function of the bandstop filter is
HN (s) = HL (s) + HH (s) = 2s 2 ( s 2 +141.4 s +10000 )+ 20000( s 2 + 2828s + 4000000 ) (s 2 +141.4s +10000 )( s 2 + 2828s + 4000000 ) 2s 4 + 282.8s 3 + 40000s 2 + 56560000s +81010 = 2 ( s +141.4s +10000 )( s 2 + 2828s + 4000000 ) P16.38 250 2 s 4( s 2 + 62500 ) 1 HN (s) = 4  4 = 2 2 2 250 2 s + s + 250 ( s + 250 s + 62500 ) 1 P16.39 2 2502 42504 HL (s) = 4 = 250 s2 + s + 2502 s 2 + 250 s + 62500 1 2 ( ) 2 P16.310 s2 4s 4 HH (s) = 4 = 2 2 250 s2 + s + 2502 ( s + 250 s + 62500 ) 1 2 164 Section 16.4: SecondOrder Filters P16.41 The transfer function is s V0 ( s ) RC = T (s) = Vs ( s ) s 2 + s + 1 RC LC so
2 K = 1 , 0 = 1 1 C and = 0 Q = RC 0 = R LC RC Q L
L = 1000 C Pick C =1 F. Then L = 1 C
2 0 = 1 H and R = Q P16.42 The transfer function is 1 I 0 ( s) LC T (s) = = s 1 I s (s) s2 + + RC LC so
2 K = 1 , 0 = 1 1 C = 0 Q = RC 0 = R and LC RC Q L
L = 3535 C Pick C = 1 F then L = 1 C
2 0 = 25 H and R = Q 165 P16.43 The transfer function is 1 R1 R C 2 T (s) = 1 1 R s2 + 2+ s + 2 2 R C R1 R C  Pick C = 0.01 F , then 1 = 0 = 2000 R = 50000 = 50 k RC 0 R R 1 = = 8333 = 8.33 k 2 + R1 = Q RC R1 Q2 P16.44 Pick C = 0.02 F. Then R1 = 40 k, R2 = 400 k and R 3 =3.252 k. P16.45 Pick C1 = C2 = C = 1 F . Then
106 = 0 R1 R2 and 1 = 0 Q= R1C Q
In this case R 2 = R1 R1 R2 R2 = R1 Q2 106 and R1 = = 1000 = 1 k 1000 166 P16.46 The node equations are V0 ( s ) = R2 R2 + 1 C 2s Va ( s ) V0 ( s ) Va ( s )  C1s (Va ( s ) Vi ( s ) ) = 0 R1 The transfer function is:
V (s) = T (s) = 0 Vi ( s ) s 2 + s2 1 s + R 2 C 2 R1 R 2 C 1 C 2
R2 R1 R1Q 2 = R 2 . Pick C1 = C2 = C = 1 F. Then 1 1 = and = 0 Q= 0 R 2C Q C R1 R 2 In this case R1 = R 2 = R and 1 = 0 R = 1000 . CR 167 P16.47 1 V ( s) LC = = T (s) = 0 R 1 Vi ( s ) L s + R + 1 s2 + s+ Cs L LC 1 Cs When R = 25 , L = 102 H and C = 4 106 F, then the transfer function is
T (s) = 25106 s 2 + 2500 s + 25106 so old = 25106 = 5000
and kf = The scaled circuit is new 250 = = 0.05 old 5000 P16.48 The transfer function of this circuit is 168 T (s) = 1+ R 2 C 2 s V0 ( s ) = = 1 Vi ( s ) 1 1 1 R1 + + s 2 + s+ C 1s R1 C 1 R 2 C 2 R1 R 2 C 1 C 2 R2 1 s R1 C 2 100 F 500 F = 0.1 F and = 0.5 F. 1000 1000 Before scaling ( R1 = 20 , C 1 =100 F, R 2 = 10 and C2 = 500 F ) Pick km = 1000 so that the scaled capacitances will be T (s) = 100s s + 700s+105
2 After scaling ( R1 = 20000 = 20 k, C 1 = 0.1 F, R 2 =10000 = 10 k, C 2 = 0.5 F ) T (s) = 100s s + 700 s +105
2 P16.49 This is the frequency response of a bandpass filter, so
K s2 + 0
Q T (s) = s
2 0
Q s + 0 From peak of the frequency response 0 = 2 p 10 106 = 62.8 106 rad/s and k=10 dB = 3.16
Next 0
Q = BW = (10.1106  9.9 106 ) 2 = (0.2 106 )2 = 1.26 106 rad/s So the transfer function is
T (s) = 3.16(1.26)106 s (3.98)106 s = 2 s 2 + (1.26)106 s + 62.82.1012 s + (1.26)106 s + 3.944.1015 169 P16.410 (a) H ( ) = Z V0 ( ) =  2 Vs ( ) Z1 where Z 1 = R1  j C1 1 j C 2 and Z 2 = 1 R2 + j C 2 R2
1 1 , 2 = R1 C 1 R2 C 2 H ( ) =  j R 2C 1 j 1+ 1 j 1+ 2 where 1 = (b) (c) 1 = 1 1 , 2 = R1 C 1 R2 C 2 H ( ) =  j R 2C 1 j 1+0 ) 0+ 1 ( = R 2C 1 R2 = 1 R 2C 1 = R1 1 P16.411 Voltage division: 1 Cs V0 ( s ) = V ( s ) , V1 ( s ) = (1 + s R C )V0 ( s ) 1 1 R+ Cs V1  Vs V V + 1 0 + (V1 V0 ) n C s = 0 mR R Combining these equations gives: 1 sC 2 V V0 +s C+ + s n R C2 = s m mR m R KCL: 1610 Therefore
H ( ) = V0 ( ) 1 = = Vs ( ) 1+ s ( m +1) R C + n m R 2 C 2 s 2 1 1 +j 0 Q 0 2 where 0 = mn 1 and Q = m +1 m n RC P16.412 R2 1 1 s  C 2s R 2 C 2 s +1 R1 C 2 V0 ( s ) H (s) = = = = R1 C 1 s +1 1 VS ( s ) 1 1 1 R1 + s 2 + + s+ C s R1 C 1 R 2 C 2 R1 R 2 C 1 C 2 C1 s 1 R2 where 0 =
BW= 1 = 70.7 k rad sec = 2 (11.25 kHz ) R1 R 2 C 1 C 2 0
Q = 1 1 + = 150 k rad s =2 ( 23.9 kHz ) R1 C 1 R 2 C 2 1611 P16.413 C 1 s (Va Vs ) + Va V0 1 = 0 s  R1 R2 C 2 V0 ( s) = H ( s)= 1 Va Vs ( s) s 2 + 1 s +  C 2 s V0 = 0 R1 C 1 R1 R 2 C 1 C 2 R2 Comparing this transfer function to the standard form of the transfer function of a second order bandpass filter gives: 0 =
BW = Q= 1 = 104 rad sec R1 R 2 C 1 C 2 1 = 103 rad/sec R1 C 1 = 10 0
BW 1612 P16.414 Node equations: a C sVc ( s ) + Vc ( s ) Vs ( s ) V ( s ) V0 ( s ) + c =0 R R V ( s ) Vc ( s ) C s (Vs ( s ) V0 ( s ) ) + s =0 a R Solving these equations yields the transfer function: 1 2 1 s 2 + + a s+ 2 a RC V0 ( s ) (RC) = H (s) = 1 Vs ( s ) 2 1 s 2 + s+ 2 a RC (RC) We require 105 =
1 . Pick C = 0.01 F then R = 1000 . Next at s = j 0 RC 2 +a a2 a H ( 0 ) = = 1+ 2 2 a The specifications require a2 201 = H ( 0 ) = 1 + a = 20 2 1613 P16.415 Node equations:
Va Va V0 + =0 R2 R1 Va Vb =0 R V V C s (Vb V0 ) + b s = 0 R C sVa + Solving the node equation yields: R1 1 1+ 2 2 R2 R C V0 ( s ) = Vs ( s ) R 1 1 s 2 + 2 1 s+ 2 2 R2 R C RC 0 = 1 1 = = 41.67 k rad sec 3 RC (1.210 ) ( 20109 ) 1614 Section 16.5: HighOrder Filters P16.51 This filter is designed as a cascade connection of a Sallenkey lowpass filter designed as described in Table 16.42 and a firstorder lowpass filter designed as described in Table 16.52. SallenKey LowPass Filter: MathCad Spreadsheet (p16_5_1_sklp.mcd)
c The transfer function is of the form T(s) = . s^2 + bs + a Enter the transfer function coefficitents: Determine the Filter Specifications: a := 628 0 := a
2 b := 628 0 b
6 4 3 Q := 0 = 628 Q = 0.707 Pick a convenient value for the capacitance: Calculate resistance values: Calculate the dc gain. R := 1 C 0 C := 0.1 10 A := 3  1 Q R = 1.592 10 R ( A  1) = 9.331 10 A = 1.586 1615 FirstOrder LowPass Filter: MathCad Spreadsheet (p16_5_1_1stlp.mcd)
k The transfer function is of the form T(s) = . s+p Enter the transfer function coefficitents: Pick a convenient value for the capacitance: Calculate resistance values: R2 := 1 C p R1 := p := 628 k := 0.5p
6 4 C := 0.1 10 1 C k R1 = 3.185 10 R2 = 1.592 10 4 P16.52 This filter is designed as a cascade connection of a Sallenkey highpass filter, designed as described in Table 16.42, and a firstorder highpass filter, designed as described in Table 16.52. The passband gain of the Sallen key stage is 2 and the passband gain of the firstorder stage is 2.5 So the overall passband gain is 2 2.5 = 5
SallenKey HighPass Filter: 1616 MathCad Spreadsheet (p16_5_2_skhp.mcd)
A s^2 The transfer function is of the form T(s) = . s^2 + bs + a Enter the transfer function coefficitents: Determine the Filter Specifications: a := 10000 0 := a Q := 0 b
6 5 5 b := 100 0 = 100 Q=1 Pick a convenient value for the capacitance: Calculate resistance values: Calculate the passband gain. R := 1 C 0 C := 0.1 10 A := 3  1 Q R = 1 10 R ( A  1) = 1 10 A=2 FirstOrder HighPass Filter: MathCad Spreadsheet (p16_5_2_1sthp.mcd)
ks The transfer function is of the form T(s) = . s+p Enter the transfer function coefficitents: Pick a convenient value for the capacitance: Calculate resistance values: R1 := 1 C p p := 100 k := 2.5
6 5 C := 0.1 10 R2 := k R1 R1 = 1 10 R2 = 2.5 10 5 1617 P16.53 This filter is designed as a cascade connection of a Sallenkey lowpass filter, a Sallenkey highpass filter and an inverting amplifier. SallenKey LowPass Filter: MathCad Spreadsheet (p16_5_3_sklp.mcd)
c The transfer function is of the form T(s) = . s^2 + bs + a Enter the transfer function coefficitents: Determine the Filter Specifications: a := 4000000 0 := a Q := 0 b
6 3 3 b := 2828 0 = 2 10 Q = 0.707
3 Pick a convenient value for the capacitance: Calculate resistance values: Calculate the dc gain. R := 1 C 0 C := 0.1 10 A := 3  1 Q R = 5 10 R ( A  1) = 2.93 10 A = 1.586 1618 SallenKey HighPass Filter: MathCad Spreadsheet (p16_5_3_skhp.mcd)
c s^2 The transfer function is of the form T(s) = . s^2 + bs + a Enter the transfer function coefficitents: Determine the Filter Specifications: a := 10000 0 := a Q := 0 b
6 5 4 b := 141.4 0 = 100 Q = 0.707 Pick a convenient value for the capacitance: Calculate resistance values: Calculate the passband gain. R := 1 C 0 C := 0.1 10 A := 3  1 Q R = 1 10 R ( A  1) = 5.86 10 A = 1.586 Amplifier: The required passband gain is 1.6106 = 4.00 . An amplifier with a gain equal to 141.42828 4.0 = 1.59 is needed to achieve the specified gain. 2.515 1619 P16.54 This filter is designed as the cascade connection of two identical Sallenkey bandpass filters: SallenKey BandPass Filter: MathCad Spreadsheet (p16_5_4_skbp.mcd)
cs The transfer function is of the form T(s) = . s^2 + bs + a Enter the transfer function coefficitents: Determine the Filter Specifications: a := 62500 0 := a Q := 0 b
6 b := 250 0 = 250 Q=1 Pick a convenient value for the capacitance: Calculate resistance values:
4 4 C := 0.1 10 A := 3  1 Q R := 1 C 0 R = 4 10 2 R = 8 10 R ( A  1) = 4 10 AQ = 2 4 Calculate the passband gain. 1620 P16.55 This filter is designed using this structure: SallenKey LowPass Filter: MathCad Spreadsheet (p16_5_5_sklp.mcd)
c The transfer function is of the form T(s) = . s^2 + bs + a Enter the transfer function coefficitents: Determine the Filter Specifications: a := 10000 0 := a Q := 0 b
6 5 4 b := 141.4 0 = 100 Q = 0.707 Pick a convenient value for the capacitance: Calculate resistance values: Calculate the dc gain. R := 1 C 0 C := 0.1 10 A := 3  1 Q R = 1 10 R ( A  1) = 5.86 10 A = 1.586 1621 SallenKey HighPass Filter: MathCad Spreadsheet (p16_5_5_skhp.mcd)
c s^2 The transfer function is of the form T(s) = . s^2 + bs + a Enter the transfer function coefficitents: Determine the Filter Specifications: a := 4000000 0 := a Q := 0 b
6 3 3 b := 2828 0 = 2 10 Q = 0.707
3 Pick a convenient value for the capacitance: Calculate resistance values: Calculate the passband gain. R := 1 C 0 C := 0.1 10 A := 3  1 Q R = 5 10 R ( A  1) = 2.93 10 A = 1.586 Amplifier: The required gain is 2, but both SallenKey filters have passband gains equal to 1.586. 2 = 1.26 to make the passband gain of the entire filter equal to 2. The amplifier has a gain of 1.586 1622 P16.56 This filter is designed as the cascade connection of two identical Sallenkey notch filters. SallenKey Notch Filter: MathCad Spreadsheet (p16_5_6_skn.mcd)
c(s^2 + a) The transfer function is of the form T(s) = . s^2 + bs + a Enter the transfer function coefficitents: Determine the Filter Specifications: a := 62500 0 := a Q := 0 b
6 b := 250 0 = 250 Q=1
7 Pick a convenient value for the capacitance: Calculate resistance values:
4 C := 0.1 10 A := 2  1 2 Q 2 C = 2 10 R := 1 C 0 = 2 10 2 Calculate the passband gain. R = 4 10 R 4 R ( A  1) = 2 10 A = 1.5 4 Amplifier: The required passband gain is 4. An amplifier having gain equal to 4 = 1.78 (1.5)(1.5) is needed to achieve the required gain. 1623 P16.57 (a) Voltage division gives: H a (s) = Vs ( s )
V2 ( s) V1 ( s ) V1 ( s ) = R1 R1 +
1 Cs = R1 C s
1 + R1 C s (b) Voltage division gives: (c) Voltage division gives: H b (s) = = Ls R2 + L s H c (s) = V2 ( s ) Vs ( s ) = R1  ( R 2 + L s ) 1 + R1  ( R 2 + L s ) Cs
R1 + ( R 2 + L s ) R1 ( R 2 + L s ) Ls R2 + L s Doing some algebra: H c (s) = V2 ( s ) Vs ( s ) = R1 ( R 2 + L s ) 1 + C s R1 + ( R 2 + L s )
2 Ls R2 + L s Ls R2 + L s Ls R2 + L s = = = R1 R 2 C s + R1 L C s 2 R1 R 2 C s + R1 L C s + R1 + R 2 + L s R1 L C s + ( R1 R 2 C + L ) s + R1 + R 2
2 R1 C s ( R 2 + L s ) R1 L C s 2 R1 L C s 2 + ( R1 R 2 C + L ) s + R1 + R 2 (d) H c ( s ) H a ( s ) H b ( s ) because the R 2 , L s voltage divider loads the 1 , R1 voltage Cs divider. 1624 P16.58
H (s) = 100 20 s s s s 1 + 1 + 1 + 1 + 200 20, 000 20 2000 2000 = s s s s 1 + 1 + 1 + 1 + 20 200 2000 20, 000 P16.59 (a) The transfer function of each stage is
1 Cs R2 R2 1 1 R 2  R2 + 1+ R2 C s R1 Cs Cs = = = H i (s) =  R1 R1 R1 1+ R2 C s R2 The specification that the dc gain is 0 db = 1 requires R 2 = R1 . The specification of a break frequency of 1000 rad/s requires Pick C = 0.1 F . Then R 2 = 10 k so R1 = 10 k . (b)
1 = 1000 . R2 C H ( ) = 1 1+ j 1 1+ j 1000 1000 1 1 H (10, 000 ) = = 40.1 dB = 2 1 + 10 101 2 1625 PSpice Problems
SP 161 1626 SP 162 1627 SP 163 1628 SP 164 1629 SP 165 1630 SP 166 1631 SP 167 Vs R1 R2 R3 L1 L2 L3 C1 C2 C3 7 7 7 7 6 1 2 5 3 4 0 6 1 2 5 3 4 0 0 0 ac 1 200 100 50 10m 10m 10m 1u 1u 1u .ac dec 100 100 10k .probe .end SP 168 Vs R1 1 1 0 2 ac 100 1 1632 C1 R2 C2 2 3 3 3 4 4 0.2u 200k 50p 0 4 FGOA Xoa5 3 .subckt FGOA 1 2 4 *nodes listed in order  + o Ri 1 2 500k E 3 0 1 2 100k Ro 4 3 1k .ends FGOA .ac dec 100 1k 100k .probe .end SP 169 Vs L1 Rw C2 L2 Rmr C3 Rt 1 1 2 1 3 4 1 5 0 2 0 3 4 0 5 0 ac 1 2.5m 8 34.82u 0.364m 8 5u 8 .ac dec 100 10 100k .probe .end Bw=4.07k  493 HZ 3600HZ Verification Problems 1633 VP 16.1 0 = 10000 = 100 rad s and
This filter does not satisfy the specifications. 0
Q = 25 Q = 100 = 4 5 25 VP 16.2 0 = 10000 = 100 rad s ,
This filter does satisfy the specifications. 0
Q = 25 Q = 100 75 = 4 and k = = 3 25 25 VP 16.3 0 = 400 = 20 rad s , 0
Q = 25 Q = 20 600 = 0.8 and k = = 1.5 25 400 This filter does satisfy the specifications. VP 16.4 0 = 625 = 25 rad s , 0
Q = 62.5 Q = 25 750 = 0.4 and k = = 1.2 62.5 625 This filter does satisfy the specifications. VP 16.5 0 = 144 = 12 rad/s and
This filter does not satisfy the specifications. 0
Q = 30 Q = 12 = 0.4 30 1634 Design Problems
DP 16.1
V0 ( s ) = 2 2 V1 ( s ) s+ s+ R3 C R R3 C 2 2 (100.103 ) = 0 =  s RC 2 2 and 2 (10.103 ) = BW = 0 = 2 R R3 C R3 C Q
2 2 = 318 k and R = = 1.6 k 3 2 ) (2 1010 ) R3C 2 0 C = 100 pF is specified so R3 = (10010 12 DP 16.2 1635 DP 16.3 Choose 1 = 0.1 , 2 = 2 , 3 = 5 , 4 = 100 rad s . The corresponding Bode magnitude plot is: H (s) = ( ) (1+ s ) (1+ s )
1+ s
2 1 2 2 4 1+ s 3 2 2 Minimum gain is  46.2 dB at f min = 0.505 Hz 1636 Chapter 17 TwoPort and Three Port Networks
Exercises
Ex. 17.41 R1 = R2 = R3 = R a Rc R a + Rb + Rc R b Rc R a + Rb + Rc R a Rb R a + Rb + Rc = = = 25(100) = 10 250 (125)(125) = 12.5 250 100(125) = 50 250 Ex. 17.51 Y12 = Y21 =
Y11 + Y12 = 1 42 Y22 +Y21 = 10.5 1 21 1 3 Y11 =  1 = 21 42 42 1 Y22 =   1 = 1/ 7 21 10.5 ( ) ( ) 1 1 41 21 Y = 1 1  21 7 Z 11 = Z 22 = V1 I1 V2 I2 I2 = 0 = 42 (21+10.5) = 18 42 +31.5 I1 = 0 = 10.5(63) =9 73.5 =6 Z 12 = Z 21 = V1 I2 I1 = 0 Since I = 10.5 42(10.5) I 2 , then V1 = I2 = 6 I2 73.5 73.5 18 Z= 6 6 9 171 Ex. 17.61 I1 1 = V1 6 1 I Y21 = 2 =  = .167 V1 6 Y11 = Y12 = Y22 = I1 = 0.0567 V2 I2 = 0.944 V2 Ex. 17.71
I 2 = 6 i, V2 = (9 + 1) i = 10 i, V1 = 1i h 22 = h12 = I2 6i = = 0.6 S V2 10 i V1 i = = 0.1 V2 10 i V1 = 1 i I1 = i + 10 V1 = i 9 9 44 V I2 = 5 i  1 = i 9 9 V1 = I1 I2 = I1 Therefore h11 = h 21 = ( ) ( ) ( ) i = 0.9 10 i 9 44 i 9 = 4.4 10 i 9 172 Ex. 17.81
1 2 2 1 12 6 4 1 1 5 5 5 15 Y=  = = and Y = S Z = 30 1 1 2 75 50 30 2 3 4 10 5 10 15 Ex. 17.82 2/5  ( 1/10 ) T= 1/ 30  1/10 ) (
Ex. 17.91 1 ( 1/10 ) 4 = 2 /15 1/ 3  ( 1/10 )  10 4 / 3 1 Ta = 0 12 0 1 1 , Tb = 1/6 1 and Tc = 0 1 3 1 21 1 12 1 0 3 12 1 3 3 Ta Tb Tc = Tc = = 0 1 1/ 6 1 1/ 6 1 0 1 1/ 6 3 / 2 Problems
Section 174: TtoT1 Transformations P17.41 173 P17.42 P17.43 I2 =  z21 I1 z22 + R L Ai = I2 z21 = I1 z22 + R L (forward current gain) R in = z A I V1 z11 I1 + z12 I 2 z z = = z11  12 i 1 = z11  12 21 I1 I1 I1 ( z22 + R L ) Av = V2 Ai R L = V1 R in (input resistance) V2 =  I 2 R L = Ai R L I1 and V1 = R in I1 (forward voltage gain) Ap = Ai Av = Ai2 RL R in 174 P17.44 First, simplify the circuit using a Y transformation: R eq = R1  Mesh equations: R = 5  20 = 4 3 30 = 18 I 10 I 2 50 = 10 I  20 I 2 Solving for the required current:
30 10 50  20 100 I= = = 0.385 A 18(20)  (10)10 260 P17.45 175 Section 175: Equations of TwoPort Networks P1751
Z 12 = 6 Z 11  Z 12 = 12 Z 11 = 18 Z 22  Z 21 = 3 Z 22 = 9 Y11 = Y12 = Y 22 = I1 1 = S V1 V =0 14
2 I1 V2 I2 V2 =
V1 = 0 6 I 2 1 =  S = 21 (6+12) V2 21 V2 / 7 1 = S V2 7 =
V1 = 0 1 1 21 14 =  1 1 21 7 P17.52 2 j 4 Z =  j 4  j4 + j2 176 P17.53 Y11 = I1 V1 and Y 21 =
V2 = 0 I2 V1 V2 = 0 V1 = so I1 + I 2 I+I I and 1 2 + 2 = bV1 G1 G1 G2
and I 2 = (b 1) G2 V1 = 3 V1 I1 = (G1  (b 1) G2 ) V1 = 1 V1 Finally Y11 = 1 S and Y21 = 3 S Next
V2 = I1+I 2 G3
I1 V2 I2 V2
V1 = 0 V1 = 0 and V 2 = I 2
G2 Y12 = Y 22 = = G 2 =  1 S = G2 + G3 = 4 S P17.54 Using Fig. 17.52 as shown: Y12 = Y21 = 0.1 S or Y12 = Y21 = 0.1 S
Y11 = 0.2  Y12 = 0.3 S Y22 = 0.05  Y21 = 0.15 S P17.55 Y12 = 10 S = Y 21 Y11 +Y12 =13.33 S Y11 = 23.33 S Y 22 + Y 21 = 20 S Y 22 = 30 S 177 P17.56
Z 11 = Z 21 = V1 I1 V2 I1 = 3 + j 3  j 2 = (3+ j ) I2 = 0 =
I2 = 0  j 2 I1 =  j2 I1 Z 12 = Z 22 = V1 I2 V2 I2 =  j2 I1 = 0 =  j2 I1 = 0 P17.57
Z 11 Z 21 = 4 Z 21  Z 12 = 1 s 4 s +1 Z 11 = 4 + 1 = s s 2 s 2 +1 Z 22 = 2 s + 1 = s s Z 22  Z 21 = 2 s P17.58 Given: s +1 1 Y= s 1 s +1 Try a circuit as shown at the right.
Y12 = 1s s +1 s +1 1 Y11 +Y12 = 1 = s s s Y 22 + Y 21 = ( s + 1)  1 = s Y11 = 178 P17.59 Given: s + 2s + 2 s 2 + s +1 Z= 1 s 2 + s +1 2 Try :
1 s + s +1 s 2 +1 s 2 + s +1 2 From the circuit, we calculate: 1 ( R2 + L s ) L C R1 s 2 + ( R1 R 2 C + L ) s + R1 + R 2 R2 + L s Cs z 11 = R1 + = R1 + = 1 L C s2 + R2 C s + 1 1 + R2 C s + L C s2 + R2 + L s Cs Comparing to the given z 11 yields: R1 = 1 R2 C = 1 R2 = 1 L C R1 = 1 L =1 H R1 R 2 C + L = 2 C =1 F R1 + R 2 = 2 LC =1 Then check z 12 , z 21 and z 22 . The are all okay. If they were not, we would have to try a different circuit structure.. P17.510 It is sufficient to require that the input resistance of each section of the circuit is equal to Ro, that is Then Ro = R (2 R + Ro ) Ro = R 4 R 2 + 4 (2 R 2 ) = R 3 R = ( 3 1) R 3 R + Ro 179 Section 176: Z and Y Parameters P17.61 i= V1 R1 and I 2 =  (b + R1 ) R1 R 2 V1 b + R1 + R 2 I1 =  I 2  i = V1 R1 R 2 Y11 = I1 V1 =
V2 = 0 b + R1 + R 2 R1 R 2 and Y21 = I2 V1 =
V2 = 0 (b + R1 ) R1 R 2 I 2 =  I1 V2 = R 2 I 2 I2 = V2 R2
1 R2 Y22 = I2 V2 =
V1 = 0 and Y12 = I1 V2 =
V1 = 0 1 R2 P17.62 v1 = (1 + 3) i1 = 4 i1 i2 = 0 v 2 = 3 i1 therefore z 11 = 4 and z 21 = 3 v1 = 3 ( i 2 + i 2 ) i1 = 0 v1 = 3 ( i 2 + i 2 ) + 2 i 2 therefore z 12 = 3 (1 + ) and z 21 = 5 + 3 Finally, 4 3(1+ ) Z= 3 5+3 1710 P17.63 Treat the circuit as the parallel connection of two 2port networks:
The admittance matrix of the entire network can be obtained as the sum of the admittance matrices of these two 2port networks 1 0 2 s  s 1+ 2 s  s Y= + = 1+ 2 s 2 1  s 2 s 2 s When i1 ( t ) = u ( t ) : 2 s +1 s 1 1 s  2 2 s +1 V1 ( s ) V1 ( s ) 1 Y = s V ( s ) = Y s = 2 + 6 s +1 V2 ( s ) 0 2 3s 0 1 s 0 so V2 ( s ) = ( S  2) 1 6 1.25 7.25 = S + + 2 3 S (3 S + 6 S +1) S + 1.82 S + 0.184 Taking the inverse Laplace transform v2 (t) = 1 61.25 e 1.82 t + 7.25 e  0.184 t 3 t 0 1711 P17.64
KVL: KCL: 1 ( i1  v 1 ) + 2 v 2 + v 2  v 1 = 0 2
i1  v 1 = 4 v 1 + 2 v 2 i1  5 v 1 v1 2 i1 = 3v1  6 z 11 = = i1 9 2 i1 = 3v1  6 v 2 i1 = 5 v1 + 2 v2 i = 5 i1 + 6 v 2 + 2 v z = v 2 =  1 2 21 1 i1 3 18 KVL: v 2 = 1 v1 + v2
12 1 13 v1 + 5 v1 = v1 2 2 KCL: 13 i 2 = 2 v1 + 5 v1 = 18 v1 2 and 2 i 2 = 2 v 2 + 5 v 2 = 2.769 v1 13 i2 =
1 18 + 5 v1 = 2 v 2 + 5 v1 z 12 = z 22 = 0.361 1712 P17.65
KCL: KVL: Then i1 + i 2 = v1 R1  R 2 i 2  b v1 + 0  v1 = 0 i2 = 
so b +1 v1 R2
i2 v1 and 1 b +1 R 2 + R1 ( b + 1) i1 = + v1 v1 = R1 R 2 R1 R 2 y 11 = i1 v1 = R 2 + R1 ( b + 1) R1 R 2 y 21 = = b +1 and R2 KVL: R 2 i1 + v 2 = 0 i1 =  1 v2 R2 1 v 2 + R3 i 2 KCL: v 2 = R 3 ( i1 + i 2 ) = R 3  R2 Then R3 = R3 i 2 and v 2 1 + R2 y 12 = i1 v2 = 1 R2 y 22 = i2 v2 = 1 1 + R3 R 2 1713 Section 177: Hybrid Transmission Parameters 17.71 B= V1 I2 I1 I2 V1 V2 I1 V2 =
V2 = 0 34 V1 5 = 6.8 since  I 2 = = V1 5 2+ 410 34 10+ 4 = 1.4 since 10 D= =
V2 = 0 I2 =  10 I1 10 + 4 A= =
I2 =0 12 10 = 1.2 since V2 = V1 10 10+ 2 1 = 0.1 S 10 C= =
I2 =0 17.72
so V2 = 0 V1 = ( R i + R1  R 2 ) I 1 therefore h11 =
KVL: V1 I1
V2 = 0 = R i + R1  R 2 = 600 k I2 +
therefore I h 21 = 2 I1 R1 R1 + R 2
= ( A I1 = A Ri Ro Ri Ro I1 + R1 R1 + R 2 ) = 106 V2 = 0 1714 I 1 = 0 vi = 0 so A vi = 0 I2 =
therefore
h 22 = I2 V2
I 1 =0 V2 R o ( R1 + R 2 )
= R o + R1 + R 2 R o ( R1 + R 2 ) = 103 Next, V1 =
therefore
h12 = V1 V2 R1 R1 + R 2
= V2 R1 R1 + R 2 = I 1 =0 1 2 P17.73
Compare :
V 2 = n V1 I 1 =n I 2 to V1 = h11 I 1 + h12V 2 I 2 = h 21 I 1 + h 22V 2 Then h11 = 0, h 22 = 0, h12 = 1 and h 21 = 1 n n P17.74
V1 = ( R1 + R 2  R 3 ) I 1 h11 = R1 + I2 =  R2 R 2 +R 3 I 1 h 21 =  R2 R 2 +R 3 R2 R3 R 2 +R 3 I2 = V1 = V2 R 2 +R 3 R2 R 2 +R 3 h 22 = 1 R 2 +R 3 V 2 h12 = R2 R 2 +R 3 1715 P17.75
I 2 = 0.1 v and v = 950 I 1 so I 2 = 95 I 1 h11 = h 21 = V1 I1 I2 I1
V2 = 0 V2 = 0 = 50 + 950 = 1000 = 95 I1 = 0 v = 0
h12 = h 22 = V1 V2 I2 V2
I1 = 0 I1 = 0 =0 = 104 S Section 178: Relationships between TwoPort Parameters P17.81 Start with I = Y11 V1 + Y12 V2 V1 = h11 I1 + h12 V2 Y parameters: 1 and H parameters: I 2 = h 21 I1 + h 22 V2 I 2 = Y21 V1 + Y22 V2 Solve the Y parameter equations for V1 and I 2 to put them in the same form as the H parameter equations. Y11 V1 = I1 + Y12 V2 Y21 V1 + I 2 = Y22 V2 Y 0 V 1 Y12  I1 11 1 = Y22 V2 Y21 1 I 2 0 1  1 Y12 Y11 = 0 Y22 Y21  Y 11 V Y 0 1 = 11 I 2 Y21 1 Y12 Y11 1 1 Y12  I1 0 Y22 V2 Y 0 H = 11 Y21 1 1 1 0 1 Y12 Y11 = Y22 Y21 0 1 Y 11 Y12Y21 Y22  Y11  1716 P17.82 Z 12 6 Z 22 2 Z  Z 14 14 = First Z = (3)(6)  (2)(2) = 14 . Then Y = . 3  Z 21 Z 11  2 Z Z 14 14 P17.83
Y 1  12 Y Y11 10 1 = First Y = (0.1)(0.5)  (0.4)(0.1) = .01 S . Then H = 11 . 0.1 Y 4 Y21 Y Y11 11 P17.84 Y12 1 Y  Y 2 0.8 11 = First Y = (0.5)(0.6)  (0.4)(0.4) S . Then H = 11 Y 0.8 0.28 Y21 Y Y11 11 Section179: Interconnection of TwoPort Networks P17.91
Y12 = Y21 =  1 S 3 Y22 = 0  Y21 = 1 S 3 Y11 + Y12 = 1 S Y11 = 4
4  1 3 3 Ya =  1 1 3 3 3 S Y12 = Y21 = 1 S Y11 + Y12 = 1 S Y11 = 3 S 2 2 Y21 +Y22 = 1 S Y22 = 4 S 3 3
4 ( 4 + 3 )  4 17 3 6 3 3 2 = Y= 4 5 4 5 3 3 3 3 3 2 Yb = 1 1 4 3 1717 P17.92 Admittance parameters: 10 6 Y = 44 44 6 8 44 44 Transmission parameters: 8 44 6 6 T= 1 10 6 6 20 12 Yp = Y + Y = 44 44 12 16 44 44 108 792 36 36 TC = T T' = 18 144 36 36 P17.93 1 s + s s G1 + G 2 Y = + 1 G 2 s +s s G 2 G 2 +G 3 1718 Verification Problems
VP 171 75 V1 = 50 I 2 = 15 I 2 175+ 75 Z 12 = V1 I2 = 15 I1 = 0 1 1 I1 = + V1 = 0.028 V1 50 125 Y11 =
Y11 24 mS, so the report is not correct. V1 I1 = 28 mS
V2 = 0 VP 172 V1 = (2 + 0.2 s ) I1 Z 11 = 2 + 0.2 s =0.2 ( s +10) Z 21 =0.1 s V2 = (0.1 s) I1 Z 22 = 2 + 0.2 s and Z 12 = 0.1 s Z = (2 + 0.2 s )(2 + 0.2 s )  (0.1 s)(0.1 s) = 0.01(3 s 2 + 80 s + 40) 1719 Z11 Z 21 T= 1 Z 21 Z 2( s +10) Z 21 s = Z 22 0.1 s Z 21 0.1(3 s 2 +80 s + 40) s 2 ( s +10) s This is not the transmission matrix given in the report. Design Problems
DP 171 We will need to find R and R1 by trial and error. A Mathcad spreadsheet will help with the calculations. Given the restrictions R 10 and R1 10 we will start with
R = 10 and R1 = 10 :
R1 := 10 Ra := 14 20 14 + 20 + R R := 10 Rb := 14 R 14 + 20 + R Rin = 14.279 Rc := R 20 14 + 20 + R Rin := R1 + ( Rb + 2) ( Rc + 20) Rb + 2 + Rc + 20 The specifications cannot be satisfied. R and R1 are at their maximum values but
R in needs to be larger. Reducing either R or R1 will reduce R in . 1720 DP 172
Need VA + VB for balance R1 V R1 + R 3 R3 V R1 + R 3 = = R2 V R2 + R4 R4 V R2 + R4 (1) (2)
R1 R 2 = . R3 R 4 Dividing (1) by (2) yields: DP 173 V1 = h11 I1 + h12 V2 I 2 = h 21 I1 + h 22 V2
Next and V2 =  I 2 R L I 2 = h 21 I1  h 22 R L I 2 I2 1 = h 21 1 + h 22 R L I1 We require 1 79 = 80 1 + h 22 R L Ai = IL I 1 =  2 =  h 21 1 + h 22 R L I1 I1 R L = 1.013 k 1 k RL 79 1 + =1 80 80 103 Next
V2 = h 21 I1 + h 22 V2 V2 (h 22 + 1/ RL ) =  h 21 I1 RL Substituting this expression into the second hybrid equation gives: I2 =  V1 = h11 I1 + h12 (h 21 ) I1 (h 22 + 1 ) RL The input resistance is given by
R in h11  h12 R L h 21 (since h 22 << 1 Finally RL ) R in = 45  (5 104 )(103 )(80) = 5 < 10 1721 DP 174
Z 11 = 2 + 4(12) 8(8) = 5 and Z 22 = =4 4 + 12 8+8 V 4 V2 = 8 I1 = 2 I1 Z 21 = 2 I1 4 + 12 Similarly Z 12 = 2 =2
I2 =0 Thvenin: Z T = Z 22 = 4 so for maximum power transfer, use R L =4 Vs 2 PRL = = 89.3 W Vs = 37.8 V 4
2 1722 DP 175 The circuit consists of 4 cascaded stages. Represent each stage by a transmission matrix using: 1 Z ( s ) T= 0 1 1 T= Y ( s ) 0 1 1 1 C s Ta = 1 0 1 L1 s 1 Tb = L1 C 2 s + 1 0 1 1 T = C3 s L2 C 3 s + 1 0 1 1 Td = 1 RL 0 1 L1 C 1 s C3 s 1 + 2 L1 C 2 C 1 s + C 1 s R L L 2 C 3 s + R L T = Ta Tb Tc Td = C3 s RL L2 C 3 s + RL L1 C 2 C 1 s + C 1 s 1 L1 C 1 s
2 1723 ...
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