Consider the satellite control system of Fig. P7.5-6. This system is described in Problem 1.4-1. For this

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Consider the satellite control system of Fig. P7.5-6. This system is described in Problem 1.4-1. For this problem, T = 0.1 s, J = 0.1, Hk = 0.02, and D(z) = 1. From the z-transform table,z (1-2) (I + 2)50'0 S 01 SL-3-

(a) Write the closed-loop system characteristic equation.
(b) Use the Routh–Hurwitz criterion to show that the system is unstable for all K.
(c) Check the results of part (b) using the Jury test.R(s) + r(t) A/D Digital controller D(z) DIA Sensor Hk M(s) Amplifier and thrusters K T(s) Torque Satellite 1

Problem 1.4-1

The satellite of Section 1.4 is connected in the closed-loop control system shown in Fig. P1.4-1. The torque

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Related Book For  answer-question

Digital Control System Analysis And Design

ISBN: 9780132938310

4th Edition

Authors: Charles Phillips, H. Nagle, Aranya Chakrabortty

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