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Given : Canonical Form - Pitch Control System - Extra 330S ( s ) Pilot Input Pedal angles k K s ( s + 2)( s + 4) ( s ) Yaw angle rudder Dynamics...

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Given : Canonical Form – Pitch Control System - Extra 330S Requirement: (a)Determine the closed-loop transfer function (5pts) (b)Determine the characteristic equation (5 pts) (c) Plot the root locus for the system (Use MATLAB) (20pts) (d)What value of K make the system to be marginally stable (Crossing the imaginary axis) (5pts) (e) Determine the closed-loop poles for K=7 (5pts) (f) Determine the step response and determine the overshoot peak time, settling time. (table) (10pts) ( ) s ( ) s Ψ - k Yaw angle rudder Pilot Input Pedal angles ( 2)( 4) K s s s + + Dynamics
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a) Closed loop transfer function: b) Characteristic equation:
Characteristic equation is
c) The root locus from MATLAB is as shown: d) We will use routh Hurwitz criteria S3...

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