Exact Feedback Linearization and Control of Space Station Using CMG
Based on feedback linearization theory, an approach to attitude control of a space station using control moment gyros (CMGs) is developed. A linearizing transformation is derived to obtain a simple linear representation of the nonlinear pitch axis dynamics. A feedback control law for trajectory tracking is derived. Extension of this approach to linearization of the coupled yaw and roll axis dynamics and control is presented.
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Singh, S. N.,
Bossart, T. C.
Exact Feedback Linearization and Control of Space Station Using CMG.
Institute of Electrical and Electronics Engineers Transactions on Automatic Control, 38(1),