Attitude fault tolerant control and active vibration suppression of flexible satellite during orbit control

被引：0
|
作者：
Yang, Jing [1 ]
Hou, Jian-Wen [2 ]
Shi, Xiao-Ping [1 ]
机构：
[1] Control and Simulation Center, Harbin Institute of Technology, Harbin,150080, China
[2] Shanghai Academy of Spaceflight Technology, Shanghai,201109, China
来源：
Shanghai Jiaotong Daxue Xuebao/Journal of Shanghai Jiaotong University | 2015年 / 49卷 / 09期
关键词：
Active vibration suppression - Actuator fault - Adaptive control algorithms - Adaptive sliding mode control - Fault tolerant control - Flexible satellites - Stability and robustness - Vibration suppression;
D O I：
10.16183/j.cnki.jsjtu.2015.09.018
中图分类号：
学科分类号：
摘要：
9
引用
收藏
页码：1373 / 1379
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