State Feedback H 1 Suboptimal Control of a Rigid Spacecraft
نویسندگان
چکیده
A state feedback H 1 suboptimal control problem on T SO(3) for a rigid spacecraft with three control torques and disturbances is addressed. The Hamilton-Jacobi inequality associated with a corresponding state feedback H 1 suboptimal control problem on T S 3 is solved globally. The H 1 suboptimal state feedback on T S 3 involves the Euler parameters and solves the original problem on T SO(3) when the initial values of the Euler parameters are appropriately chosen.
منابع مشابه
State feedback H 1 control of a Rigid
In the present paper we address a state feedback H 1 suboptimal control problem for a rigid spacecraft with three control torques and disturbances. The state feedback H 1 suboptimal control problem on T SO(3) is transferred to a corresponding state feedback H 1 suboptimal control problem on T S 3 , and the Hamilton-Jacobi inequality associated with this problem is solved. We obtain a state feed...
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