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The position control system for a spacecraft platform is governed by the following

Modern Control Systems | 12th Edition | ISBN: 9780136024583 | Authors: Richard C. Dorf, Robert H. Bishop ISBN: 9780136024583 453

Solution for problem E2.16 Chapter Chapter 2

Modern Control Systems | 12th Edition

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Modern Control Systems | 12th Edition | ISBN: 9780136024583 | Authors: Richard C. Dorf, Robert H. Bishop

Modern Control Systems | 12th Edition

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Problem E2.16

The position control system for a spacecraft platform is governed by the following equations: d 2 p dp f + 2-p + 4p = B dt2 dt Vi=r- p - = 06 * V2 = lV\. The variables involved are as follows: r(t) = desired platform position p{t) = actual platform position V\{l) = amplifier input voltage v2(t) = amplifier output voltage 0(/) = motor shaft position Sketch a signal-flow diagram or a block diagram of the system, identifying the component parts and determine the system transfer function P(s)/R(s).

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Chapter Chapter 2, Problem E2.16 is Solved
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Textbook: Modern Control Systems
Edition: 12
Author: Richard C. Dorf, Robert H. Bishop
ISBN: 9780136024583

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The position control system for a spacecraft platform is governed by the following