System Dynamics
3rd Edition
ISBN: 9780073398068
Author: III William J. Palm
Publisher: MCG
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Chapter 12, Problem 12.3P
It is desired to control the angular displacement 9 of a space vehicle by controlling the applied torque T supplied by thrusters (Figure Pl2.3). The plant model is Design a compensator for this plant. The system must have a settling time no greater than 4 sec and a steady-state error of zero for a step command, and the dominant roots of the closed-loop system must have < > 0.45.
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Please solve the following by hand and without the use of AI. Thank you!
do not solve the last part ofthe question which states “Obtain the steady-state error when the disturbance qd is a unit-stepfunction”.
Can you also please do the simulate the step response in MATLAB for the design and report achieved PO and settling time? Thank you.
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