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
来源：
AIAA JOURNAL | 2018年 / 56卷 / 10期
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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