Inverse Optimality Results forthe Attitude Motion of a Rigid Spacecraft
نویسنده
چکیده
We present an approach for constructing optimal feedback control laws for optimal regulation of a rotating rigid spacecraft. We employ the inverse optimal control approach which circumvents the task of solving a Hamilton-Jacobi equation and results in a controller optimal with respect to a meaningful cost functional. The design reported in the paper is the rst optimal control design for attitude regulation of the complete, nonlinear system, which includes a penalty on the angular velocity , orientation and the control torque.
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تاریخ انتشار 1997