(a) Given a block diagram for space satellite system as shown in Figure Q2(a). To get the desired angle of orientation,

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(a) Given a block diagram for space satellite system as shown in Figure Q2(a). To get the desired angle of orientation,

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A Given A Block Diagram For Space Satellite System As Shown In Figure Q2 A To Get The Desired Angle Of Orientation 1
A Given A Block Diagram For Space Satellite System As Shown In Figure Q2 A To Get The Desired Angle Of Orientation 1 (65.64 KiB) Viewed 30 times
(a) Given a block diagram for space satellite system as shown in Figure Q2(a). To get the desired angle of orientation, a single transfer function of the system Y(s) = is R(S) obtained. R(s) + H₂ (s) H₂(s) G₁(s) He(s) G₂ (s) H₂ (s) Ha(s) G3(s) Figure Q2(a): Space satellite block diagram (1) Construct a signal flow graph for the system in Figure Q2(a). -C(s) C2 [SP1] [4 marks] (n) Identify the forward path. loop gain, combination of non-touching loop and loop gain that do not touch any respective forward path. C3|SP2116 marks] (m) By using Mason's rule, find the single transfer fianchion Y(s) for the system if G₂ (8) = 6₂(s) = 6₂ (s) = 2s al 1₂ (s) = 1₂(s) = 11,(s) = !1, (s) = !1,(8) = 5. C3 [SPI] [6 marks]
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