The position control system for a spacecraft plat- form is governed by the following equations: d²y dy + 2 + 4y = dt dt2 de = 0.6v2 dt v1 = r – y V2 = 7v1 The variables involved are as follows: r(t) = desired platform position y(t) = actual platform position v,(t) = amplifier input voltage v2(t) = amplifier output voltage 0(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 Y(s) r(s)

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The position control system for a spacecraft plat-
form is governed by the following equations:
d²y
dy
+ 2
+ 4y =
dt
: 이
dt2
do
= 0.6v2
dt
Vị = r – y
V2 = 7v1
The variables involved are as follows:
r(t) = desired platform position
y(t) = actual platform position
v,(t) = amplifier input voltage
v2(t) = amplifier output voltage
0(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
Y(s)
r(s)
Transcribed Image Text:The position control system for a spacecraft plat- form is governed by the following equations: d²y dy + 2 + 4y = dt : 이 dt2 do = 0.6v2 dt Vị = r – y V2 = 7v1 The variables involved are as follows: r(t) = desired platform position y(t) = actual platform position v,(t) = amplifier input voltage v2(t) = amplifier output voltage 0(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 Y(s) r(s)
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