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Wang Jing L iu L iangdong Zhang Duzhou ( Beijing Institute of Control Engineering,Beijing10 0 0 80 )
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Abstract: The attitude dynamics and kinematics of small satellite are analysed.The dynamic equation can be linearized by a vectorof dynamic parameters.By this property and in the presence of parameter uncertainty,an adaptive control algorithm is presented,and the algorithm can keep the control system increasingly stable.Simulation results confirm the effectiveness of the algorithm.
Wang Jing L iu L iangdong Zhang Duzhou ( Beijing Institute of Control Engineering,Beijing10 0 0 80 ). Adaptive Attitude Control for Small Satellite[J]. .
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