QUESTION 1 (a) Given a block diagram for space satellite system as shown in Figure Q2(a). To get C(s) the desired angle

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QUESTION 1 (a) Given a block diagram for space satellite system as shown in Figure Q2(a). To get C(s) the desired angle

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Question 1 A Given A Block Diagram For Space Satellite System As Shown In Figure Q2 A To Get C S The Desired Angle 1
Question 1 A Given A Block Diagram For Space Satellite System As Shown In Figure Q2 A To Get C S The Desired Angle 1 (30.36 KiB) Viewed 33 times
QUESTION 1 (a) Given a block diagram for space satellite system as shown in Figure Q2(a). To get C(s) the desired angle of orientation, a single transfer function of the system Y(s) R(S) obtained. R(s) H₂(s) H₁(s) G₁(s) H5(s) G₂ (s) H3(s) H4(s) G3(s) Figure Q2(a): Space satellite block diagram .C(s) is
Figure Q2(a): Space satellite block diagram (i) Construct a signal flow graph for the system in Figure Q2(a). C2 [SP1] [4 marks] (ii) Identify the forward path, loop gain, combination of non-touching loop and loop gain that do not touch any respective forward path. C3 [SP2] [6 marks] By using Mason's rule, find the single transfer function Y(s) for the system if G₁ (S) = G₂ (S) = G₂ (s) = 2s and H₁(s) = H₂(s) = H₂ (s) = H4(S) = H5(s) = S. C3 [SP1] [6 marks]
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