Active fault tolerant control design approach for the flexible spacecraft with sensor faults
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Publication:682679
DOI10.1016/j.jfranklin.2017.09.023zbMath1380.93090OpenAlexW2765655339MaRDI QIDQ682679
Bing Han, Dezhi Xu, Zhifeng Gao, Jinxing Lin, Guo-Ping Jiang
Publication date: 5 February 2018
Published in: Journal of the Franklin Institute (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1016/j.jfranklin.2017.09.023
flexible spacecraftLipschitz nonlinearitysensor faultsfunctional observeractive fault tolerant controldynamic output feedback-based FTC approach
Sensitivity (robustness) (93B35) Feedback control (93B52) Nonlinear systems in control theory (93C10) Variable mass, rockets (70P05)
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Sensor fault detection based on fuzzy singularly perturbed model, Constrained <scp>multi‐observer‐based fault‐tolerant disturbance‐rejection</scp> control for rigid spacecraft, Adaptive fuzzy fixed-time tracking control for high-order nonlinear delayed systems with mismatched disturbances, Integrated fault tolerant tracking control for rigid spacecraft using fractional order sliding mode technique, Fault-tolerant control for the linearized spacecraft attitude control system with Markovian switching
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