A recurrent neural network (RNN)-based attitude control method for a VSCMG-actuated satellite

Published: 01 Jan 2012, Last Modified: 14 May 2024ACC 2012EveryoneRevisionsBibTeXCC BY-SA 4.0
Abstract: A recurrent neural network (RNN)-based adaptive attitude controller is developed, which achieves attitude tracking in the presence of uncertain actuator inertia in addition to time-varying, uncertain satellite inertia. The satellite control torques are produced by means of a cluster of variable speed control moment gyroscopes (VSCMGs). The adaptive attitude controller results from a RNN structure while simultaneously acting as a composite VSCMG steering law. A null motion strategy is exploited to simultaneously perform the gimbal reconfiguration for singularity avoidance and wheel speed reg-ularization for internal momentum management. In designing the adaptive attitude controller, one of the challenges confronted is that the control input is premultiplied by a non-square, time-varying, nonlinear, uncertain matrix.
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