An engineering laboratory has presented a plan to operate an Earth-orbiting satellite

Chapter 0, Problem CP9.7

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An engineering laboratory has presented a plan to operate an Earth-orbiting satellite that is to be controlled from a ground station. A block diagram of the proposed system is shown in Figure CP9.7. It takes T seconds for a signal to reach the spacecraft from the ground station and the identical delay for a return signal. The proposed ground-based controller is a proportional-derivative (PD) controller, where Gr(s) = Kr + Kos.

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