Sliding mode control attitude tracking of rigid spacecraft using adaptive back-stepping method

Yu Chunmei,Xia Yuanqing,Liu Hailiang,Lu Kunfeng

doi:10.1109/chicc.2015.7260146

Sliding mode control attitude tracking of rigid spacecraft using adaptive back-stepping method

Yu Chunmei, Xia Yuanqing + Show 2 more

https://doi.org/10.1109/chicc.2015.7260146

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Publication Date: Jul 1, 2015

Citations: 16

Affiliation: Beijing Institute of Technology, Beijing Aerospace Flight Control Center

#Attitude Tracking Of Rigid Spacecraft #Adaptive Back-stepping Method + Show 8 more

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Abstract

The attitude tracking control problem for a rigid spacecraft system is investigated in this paper. A novel adaptive approach is proposed with the utilization of sliding mode control (SMC) and backstepping technique (BT) to achieve accurate attitude tracking control for spacecraft system in the presence of inertia uncertainties and external disturbances. Finally, simulation results are presented to illustrate effectiveness of the control strategies.

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