Electronics Engineering

Electronics EngineeringControl SystemsMultiple Choice (MCQ)1 Mark
Q10.

imageA satellite attitude control system, as shown below, has a plant with transfer function G(s)=1s2G(s) = \frac{1}{s^2} cascaded with a compensator C(s)=K(s+α)s+4C(s) = \frac{K(s+\alpha)}{s+4}, where KK and α\alpha are positive real constants.

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In order for the closed-loop system to have poles at 1±j3-1 \pm j\sqrt{3}, the value of α\alpha must be _______.

A
0
B
1
C
2
D
3