For the satellite control system of Problem 7.5-6, the frequency response for G(z) was calculated by computer

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For the satellite control system of Problem 7.5-6, the frequency response for G(z) was calculated by computer and is given in Table P7.7-3.

(a) Sketch the Nyquist diagram for the open-loop function G(z)H , with H = 0.02 ⇒ − 34.0 dB .

(b) Use the results in part (a) to determine the range of K for stability.TABLE P7.7-3 Frequency Response for Problem 7.7-3 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1.0 2.0 3.0 4.0 5.0 6.0 7.0 8.0 9.0 10.0 20.0 30.0 40.0 5.829 6.733 7.610 8.457 9.273 15.708 19.656 22.143 0.29001 -10.75 0.21622

Problem 7.5-6Consider the satellite control system of Fig. P7.5-6. This system is described in Problem 1.4-1. For thisR(s) r(t) A/D Digital controller D(z) DIA M(s) Sensor  Hk Amplifier and thrusters K T(S) Torque Satellite 1

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Digital Control System Analysis And Design

ISBN: 9780132938310

4th Edition

Authors: Charles Phillips, H. Nagle, Aranya Chakrabortty

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