Adaptive fast sliding mode fault tolerant control integrated with disturbance observer for spacecraft attitude stabilization system.

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作者： Bin,Guo ^[1] ; Yong,Chen ^[2]

作者单位： School of Automation Engineering, University of Electronic Science and Technology of China, Chengdu, 611731, China; Institute of Electric Vehicle Driving System and Safety Technology, University of Electronic Science and Technology of China, Chengdu, 611731, China. Electronic address: bguodxl@163.com. ^[1] School of Automation Engineering, University of Electronic Science and Technology of China, Chengdu, 611731, China; Institute of Electric Vehicle Driving System and Safety Technology, University of Electronic Science and Technology of China, Chengdu, 611731, China. Electronic address: ychencd@uestc.edu.cn. ^[2]

关键词 Actuator fault Adaptive fast terminal sliding mode Composite observer Fault-tolerant control (FTC)Mismatched disturbance Spacecraft system

DOI 10.1016/j.isatra.2019.04.014

PMID 31047644

发布时间 2019-11-20

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ISA transactions

2019年94卷

1-9页

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Adaptive fast sliding mode fault tolerant control integrated with disturbance observer for spacecraft attitude stabilization system.

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Adaptive fast sliding mode fault tolerant control integrated with disturbance observer for spacecraft attitude stabilization system.

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