The position control system for a spacecraft plat- form is governed by the following equations: d²z dz + 2 + 4z = 0 %3D dt2 dt de = 0.6v2 dt vị = r – z v2 = 7v, %3D The variables involved are as follows: r(t) = desired platform position z(t) = actual platform positiom v:(t) = amplifier input voltage v2 (t) = amplifier output voltage %3D O(t) = motor shaft position Sketch a signal- flow diagram of the system, identifying the component parts and their transmittance; then determine the system transfer function Z(s) r(s)

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A: The open loop system is,

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Q: The position control system for a spacecraft plat- form is governed by the following equations: d²z…

A:

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