Adaptive Tracking Control of Spacecraft Using Magnetic Actuators

被引:0
|
作者
Guan, Zexin [1 ]
Wang, Zhonghua [1 ]
机构
[1] Univ Jinan, Sch Control Sci & Engn, Jinan, Peoples R China
关键词
ATTITUDE-CONTROL; VELOCITY;
D O I
10.1109/CSO.2009.242
中图分类号
TP39 [计算机的应用];
学科分类号
081203 ; 0835 ;
摘要
The attitude tracking control problem of the spacecraft using magnetic actuators is considered in this paper. We design the adaptive control law, which incorporates a velocity-generating filter from attitude measurement, to ensure the asymptotic convergence of the attitude and angular velocity tracking errors despite unknown spacecraft inertia. Simulation results demonstrate the practical applicability of the proposed approach.
引用
收藏
页码:676 / 679
页数:4
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