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 |
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其他作者: | School of Electrical and Electronic Engineering |
格式: | Article |
語言: | English |
出版: |
2015
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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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