Camilo Riano-Rios, Sanny R. Omar, R. Bevilacqua, W. Dixon
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引用次数: 4
Abstract
This paper presents a control algorithm for three axis attitude regulation of a 2U CubeSat by means of gravity gradient and atmospheric torques. The inertia tensor of the spacecraft is modified to keep the spacecraft in a gravity gradient stable configuration. A Lyapunov-based control law acts simultaneously to improve the pitch angle regulation performance using atmospheric torque.
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