Attitude Reorientation of Spacecraft with Attitude Forbidden Zones

被引:4
|
作者
Lu, Xuhui [1 ,2 ]
Jia, Yingmin [1 ,2 ]
机构
[1] Beihang Univ BUAA, Res Div 7, 37 XueYuan Rd, Beijing 100191, Peoples R China
[2] Beihang Univ BUAA, Dept Syst & Control, Beijing 100191, Peoples R China
关键词
attitude stabilization; attitude constraints; backstepping; dynamic scaling;
D O I
10.2991/jrnal.2015.2.1.4
中图分类号
TP24 [机器人技术];
学科分类号
080202 ; 1405 ;
摘要
This paper investigates an attitude reorientation control scheme of spacecraft, considering attitude forbidden zone and external disturbances. A novel potential barrier function is proposed with an attitude constraint term and a dynamical scaling term. Here the dynamical scaling term is synthesized with a backstepping-based control scheme to accommodate both the avoidance of attitude forbidden zones and disturbance attenuation. Simulation results are given to verify the effectiveness of the proposed method.
引用
收藏
页码:13 / 16
页数:4
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