Satellite attitude fault tolerant control with reaction wheel misalignment and fault

被引：0
作者：
Huo, Xing [1 ,2 ]
Hu, Qing-Lei [1 ]
Xiao, Bing [1 ]
机构：
[1] Department of Control Science and Engineering, Harbin Institute of Technology, Harbin
[2] College of Engineering, Bohai University, Jinzhou
来源：
Kongzhi yu Juece/Control and Decision | 2014年 / 29卷 / 08期
关键词：
Actuator misalignment; Fault tolerant control; Finite time; Partial loss of effectiveness; Satellite;
D O I：
10.13195/j.kzyjc.2013.0807
中图分类号：
学科分类号：
摘要：
An attitude stabilization scheme is presented for a rigid satellite. The partial loss of reaction wheel effectiveness is tolerated, and reaction wheel misalignment is also compensated. The Lyapunov stability analysis shows that the closedloop attitude system is guaranteed to be almost asymptotically stable in finite-time. An illustrative example of a satellite is given, and simulation results show the effectiveness of the derived control law.
引用
收藏
页码：1434 / 1438
页数：4
相关论文
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