Flexible Satellite Attitude Maneuver via Adaptive Sliding Mode Control and Active Vibration Suppression

被引:25
|
作者
Xu, Shijie [1 ]
Cui, Naigang [2 ]
Fan, Youhua [1 ]
Guan, Yingzi [2 ]
机构
[1] Harbin Inst Technol, Shenzhen Grad Sch, Shenzhen 518055, Peoples R China
[2] Harbin Inst Technol, Sch Astronaut, Harbin 150001, Heilongjiang, Peoples R China
基金
中国国家自然科学基金;
关键词
TRACKING MANEUVERS; SPACECRAFT; DESIGN; BEAMS;
D O I
10.2514/1.J057287
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
[No abstract available]
引用
收藏
页码:4205 / 4212
页数:8
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