$ 7 5 7 $ 7 7
&|(#|i2|!6(66( pYi
t
p zr!YQ!H!QY!jHiI !HuereyiFC
I Wa ` Wa Q l GQ t C a cQ G
Qtc `Q s Ca CG hw ` WtaQ `c GQtQ Ct `wc Q t C l nC Q t
uhuIH!&F!PXeecjFYCu!PYGWHl4QHutAlHe!u&FuQHFe4HuvH|He v iHu1` r|Qb
pX
G n ` Wt c Ca t I l nC lG n G t
Basic avionics
Avionics is a rather broad subject. The word avionics is short for aviation electronics. But it actually
encompasses much more than electronics. What exactly does avionics entail? How does it work? And
how did it come to be? That is what th
Chapter 2
Problem Solving
Chapter 2- Visual Basic
Schneider
1
Outline and Objective
Program Development Cycle
Programming Tools
Chapter 2- Visual Basic
Schneider
2
Programming Languages:
Machine Language
Assembly Language
High level Language
Chapter 2-
Example on using Tabular method for simplifying Boolean
Functions
Ex. Use the Tabular method to simplify the following function and find PI & EPI
F(A, B, C, D) = (0,1,2,3,5,7,8,10,12,13,15)
Ans:
1) Write & Identify: this step concerns writing the equivale
hFCPP!FCYwvePFCq
G GGQ ` W WI
3wtY`zwitfFPHqifwGH!fdY`F!PFPGXftAYIHwvA!XCHHHfF!aPFCPXft6HwfC
d Cv W Qvd td qCG ad Eaa W Q qCaIC W IQ mC `d Q qC I G Q v w
ifwGH!fdY`cfw_Y`fz6QHwAYIW1id!YQ!fwGH!fdY`W(HFYCPff6FgfgahaYHPFPH!PI
ad Eaa W Wd v v jI Wad Eaa I E W
Lecture 5
Minimal set
Converting to use NAND and NOR
Minimizing functions using Boolean
cubes
Can implement any logic function from
NOT, NOR, and NAND
In fact, can do it with only NORs and
NANDs
NOT is just NAND or NOR with two
identical inputs
X
0
1
Y
0
Determining your orientation
The rst step to knowing where you are, is knowing how youre oriented. How can we measure our
orientation?
1
Indicating your orientation
Before we can determine our orientation, we need to be able to indicate it. For this, we r
Trajectory Calculation
Lab 2 Lecture Notes
Nomenclature
t
time
h altitude
V velocity, positive upwards
F total force, positive upwards
D aerodynamic drag
()
time derivative ( = d( )/dt )
g
m
CD
A
i
air density
gravitational acceleration
mass
drag coecient
EE 281
Embedded Systems Design Laboratory
September 25, 2002
Handout #1
Course Information
Instructor:
Pascal Stang
052 Packard Building (EE281 lab)
Telephone: Home: 408-244-7737
Email: [email protected]
Office hours: Wed/Fri 1:15-2:15, and by appointme
Continuous Time Convolution:
1. Solve the following for y(t)=x(t)*h(t) x(t) = u(t)-u(t-4); h(t) = r(t) 2. Convolve the following:
3. Find the response of a system to an input of x(t)=2u(t-10) if h(t)=sin(2t)u(t). 4. A linear time invariant system has the
MISSION STATEMENT IN INSTITUTIONAL FAMILY
BUSINESS:
A CONTENT ANALYSIS
Turan UHADAR
Vice Governor Governorship of Ordu
Lec. H. brahim ZMEN
Balikesir University, TURKEY
Abstract
Family business has an important place in economic system.
Institutionalizatio
Orbital Mechanics with MATLAB
Lamberts Problem
This document describes four MATLAB scripts that demonstrate how to solve the Earth orbit,
interplanetary, and J 2 -perturbed form of Lamberts problem. Lamberts problem is concerned
with the determination of
LEGAL INFORMATION
Wolfram Mathematica License Agreement
Acceptance
This is a binding Agreement: read all terms; retain a copy.
Carefully read the following terms and conditions before accessing, installing, or using the
Tra jectory Calculation
Lab 2 Lecture Notes
Nomenclature
t
time
h
altitude
V
velo city, positive upwards
F
total force, positive upwards
D aero dynamic drag
T
propulsive thrust
t time step
()
time derivative ( = d( )/dt )
g
m
CD
A
mfuel
ue
i
air density
g
RECEIVER SENSITIVITY / NOISE
RECEIVER SENSITIVITY
Sensitivity in a receiver is normally taken as the minimum input signal (Smin) required to produce a specified output
signal having a specified signal-to-noise (S/N) ratio and is defined as the minimum sig
SIGNALS AND SYSTEMS (IT1201)
Prepared by
N.Sugitha,
Asst.Professor,
Information Technology.
SIGNALS AND SYSTEMS
(IT 1201)
UNIT I
CLASSIFICATION OF SIGNALS AND SYSTEMS
1. Define Signal.
A signal is a function of one or more independent variables which cont
Answers Avionics exam February 2006
1. Avionics - general
a)
WAAS = Wide Area Augmentation System. Network of ground-based reference stations, designed to
augment GPS: provides ground integrity broadcast (satellite status), wide area DGPS corrections
impr
Experiment
7
COUNTERS
Objectives
-To design a ripple counter using JK flip flop.
-To connect a pre-settable counter and observe its operation.
-To create different counter module by decoding outputs and loading preset
inputs.
Basic
Information
A counter i
E W ` Q v C v G v I G v Q Q G jsvI d r Q
AQHHwevFsHFYCdAHwvfXfHhPqPifP&QHwFCffddHE1PFC(Hwv(FUeWP!Q u f1Hwv
C
wv HHfwFC QHwwv H ev!aXYC!FH`HFCPFwveH`YWXH&IYW
`d vG
v C
c W dQU E Gs d W m s
` c ` W WIC vd Qvd d vdGa Wd
Hfds FYCwevPFzoi!wigaXYCYIWviw!PY
Final Exam
Due date Monday December 6th of 2010 at 2pm.
This is the time by which the electronic report submission must be done.
We will meet at 2pm for the nal presentation and project defense.
During this time, your team will give a 20 min presentation
Application Report
SPRA601 - November 1999
Code Composer Studio'sTM Command Window
Jeff Sherman Digital Signal Processing Solutions
ABSTRACT
With the introduction of Code Composer and Code Composer Studio, Texas Instruments (TITM) has provided a Command W
AE 457/641 Navigation and Guidance
Tutorial 7, November 6, 2007
1. At the time of launch, a missile launched at a speed of 900m/s is directly in the path of
a target moving along a straight line at 300m/s. A launch error causes the missile to be
launched
AE 457/641 Navigation and Guidance
Tutorial 1, August 9, 2007
1. Find the constant course required to navigate along a rhumb line from New York (40 47
N, 73 58 W) to Cardi (51 30 N, 3 12 W). Find the rhumb line distance as well as
the shortest distance be
Discrete-Time Convolution: 1. Find the impulse response for each of the following discrete-time systems: a) y[n] + 0.2y[n-1] = x[n]-x[n-1] b) y[n] + 1.2y[n-1] = 2x[n-1] c) y[n] = 0.24(x[n]+x[n-1]+x[n-2]+x[n-3]) d) y[n] = x[n] + 0.5x[n-1] + x[n-2]
2. Perfo
Z-Transforms: 1. Find the z transform of the following signals: a) x[n] = u[n] - u[n-4] b) x[n] = 0.5nu[n] c) x[n] = [1 4 8 2] d) x[n] = [0 1 2 3 4] e) x[n] = 2(0.8)nu[n] 2. Find the inverse Z-transforms of the following signals:
( z 1)( z + 0.8) ( z 0.5)
System Properties: 1. Determine if the following systems are time-invariant, linear, causal, and/or memoryless? dy a) + 6y( t ) = 4 x ( t ) dt dy b) + 4 ty( t ) = 2 x( t ) dt c) y[ n] + 2 y[ n 1] = x[ n + 1] d) e) y(t) = sin(x(t)
dy + y 2 ( t ) = x( t ) d
Laplace Transforms
1. Compute the Laplace Transforms of the following functions:
a)
b)
c)
d)
x( t ) = 4 sin(100t ) u( t )
x( t ) = 4 sin(100t 10) u( t 01)
.
x( t ) = 2 u( t ) + ( t 4) cos(5t ) u( t )
x( t ) = tu( t ) 2( t 2) u( t 2) + ( t 3) u( t 3)
e) x(
XyoTech Engineering Associates
Tactical and Strategic Missile Guidance
Course Synopsis
Whether you work in the tactical world or the strategic world, this 5 day course will help you understand and appreciate
the unique challenges of each. So everyone can