Nonlinear Singular H 1 Suboptimal Control for a Rigid Spacecraft with Actuator Dynamics
نویسنده
چکیده
In the present paper we address a nonlinear singular H1 sub-optimal control problem for a rigid spacecraft with actuator dynamics. Using recent results from nonlinear H1 control theory , we nd an explicit feedback solution involving the Euler parameters. Our solution is based on a solution to a corresponding nonlinear regular H1 suboptimal control problem for a rigid spacecraft with three control torques and disturbances .
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