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State feedback ℋ-suboptimal control of a rigid spacecraft

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2 Author(s)
Dalsmo, M. ; Div. of Eng. Cybern., Norwegian Univ. of Sci. & Technol., Trondheim, Norway ; Egeland, O.

A state feedback ℋ-suboptimal control problem on TSO(3) for a rigid spacecraft with three control torques and disturbances is addressed, the Hamilton-Jacobi inequality associated with a corresponding state feedback ℋ-suboptimal control problem on TS3 is solved globally. The ℋ-suboptimal state feedback on TS3 involves the Euler parameters and solves the original problem on TSO(3) when the initial values of the Euler parameters are appropriately chosen

Published in:

Automatic Control, IEEE Transactions on  (Volume:42 ,  Issue: 8 )

Date of Publication:

Aug 1997

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