The satellite of Section 1.4 is connected in the closed-loop control system shown in Fig. P1.4-1. The
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The satellite of Section 1.4 is connected in the closed-loop control system shown in Fig. P1.4-1.
The torque is directly proportional to the error signal.
![(a) Derive the transfer function (s)/(s), where e(t) = [0(s)] is the commanded attitude angle. L (b) The](https://dsd5zvtm8ll6.cloudfront.net/images/question_images/1705/3/9/9/70865a6559ce9ed51705399708042.jpg)
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K a s Ts s Ts Es 0s s Js Js K 1500 ...View the full answer
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Related Book For 
Digital Control System Analysis And Design
ISBN: 9780132938310
4th Edition
Authors: Charles Phillips, H. Nagle, Aranya Chakrabortty
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