Finite-time fault-tolerant control of nonlinear spacecrafts with randomized actuator fault: fuzzy model approach
The primary objective of this paper is to address the challenge of designing finite-time fault-tolerant control mechanisms for nonlinear flexible spacecraft systems, which are particularly vulnerable to randomized actuator faults. Diverging from traditional methodologies, our research harnesses the...
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格式: | Article |
語言: | English |
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2024
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在線閱讀: | https://hdl.handle.net/10356/181583 |
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