Integral-type sliding mode fault-tolerant control for attitude stabilization of spacecraft

Two fault-tolerant control (FTC) schemes for spacecraft attitude stabilization with external disturbances are proposed in this brief. The approach is based on integral-type sliding mode control strategy to compensate for actuator faults without controller reconfiguration. First, a basic integral-typ...

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Main Authors: Zhu, Senqiang, Shen, Qiang, Wang, Danwei, Poh, Eng Kee
其他作者: School of Electrical and Electronic Engineering
格式: Article
語言:English
出版: 2015
在線閱讀:https://hdl.handle.net/10356/79311
http://hdl.handle.net/10220/38578
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機構: Nanyang Technological University
語言: English

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