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

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

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Given A Block Diagram For Space Satellite System As Shown In Figure Q2 A To Get C S The Desired Angle Of Orientation 1
Given A Block Diagram For Space Satellite System As Shown In Figure Q2 A To Get C S The Desired Angle Of Orientation 1 (42.87 KiB) Viewed 36 times
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. (1) R(s) + H₂(s) H₁(s) S. G₁(s) G₂(s) H₂(s) H₂(s) G3(s) H5(s) Figure Q2(a): Space satellite block diagram - .C(s) is Construct a signal flow graph for the system in Figure Q2(a). C2 [SP1] [4 marks] 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] (iii) By using Mason's rule, find the single transfer function Y(s) for the system if G₁(s) = G₂ (S) = G₂ (s) = 2s and H₂(s) = H₂(s) = H₂(s) = H₂(s) = H₂(s) =
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