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Q#1
Control System Design
GATE EC 2024
MCQ
+2 marks
-0.66 marks
A satellite attitude control system, as shown below, has a plant with transfer function
cascaded with a compensator
, where K and
are positive real constants.

In order for the closed-loop system to have poles at
, the value of
must be ________.
0
1
2
3
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