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Get Full Access to Modern Control Systems - 12 Edition - Chapter Chapter 2 - Problem E2.16
Get Full Access to Modern Control Systems - 12 Edition - Chapter Chapter 2 - Problem E2.16

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

ISBN: 9780136024583 453

## Solution for problem E2.16 Chapter Chapter 2

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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