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Nonlinear H control and its application to rigid spacecraft

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1 Author(s)
Wei Kang ; Dept. of Math., Naval Postgraduate Sch., Monterey, CA, USA

The problem of H control of a rigid spacecraft with three control torques and disturbances is addressed. The Hamilton-Jacobi-Isaacs inequality for H feedback design is solved. An H suboptimal feedback is given, and the stability properties of the closed-loop system are studied

Published in:

IEEE Transactions on Automatic Control  (Volume:40 ,  Issue: 7 )