The block diagram of an uncompensated satellite and a compensated satellite launching system is shown in figure 4 and figure 5 respectively. The transfer function G(s) = a(s+d) s(s+c)(s+b) and feedback element transfer function is H(s) = : Do the following: (s+f)

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Q5.
The block diagram of an uncompensated satellite and a compensated satellite launching system is
a(s+d)
shown in figure 4 and figure 5 respectively. The transfer function G(s)
and feedback
s(s+c)(s+b)
e
element transfer function is H(s) =
. Do the following:
(s+f)
a.
Write an m-script of the Compensated basic Satellite launching system as shown in figure 4
and generate the step response graph showing the uncompensated(figure 4) and
compensated (figure 5) system responses both on a single graph. (Values for a=2, b=2, c=5,
d=3, e=6, and f=1).
Transcribed Image Text:Q5. The block diagram of an uncompensated satellite and a compensated satellite launching system is a(s+d) shown in figure 4 and figure 5 respectively. The transfer function G(s) and feedback s(s+c)(s+b) e element transfer function is H(s) = . Do the following: (s+f) a. Write an m-script of the Compensated basic Satellite launching system as shown in figure 4 and generate the step response graph showing the uncompensated(figure 4) and compensated (figure 5) system responses both on a single graph. (Values for a=2, b=2, c=5, d=3, e=6, and f=1).
Satellite
R(s)
G(s)
C(s)
H(s)
Figure 4: Uncompensated basic Satellite launching system
R(s)
Satellite
C(s)
Figure 5: Compensated basic Satellite launching system with unity feedback
Transcribed Image Text:Satellite R(s) G(s) C(s) H(s) Figure 4: Uncompensated basic Satellite launching system R(s) Satellite C(s) Figure 5: Compensated basic Satellite launching system with unity feedback
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