Active fault tolerant control design approach for the flexible spacecraft with sensor faults

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

zbMATH Keywords

flexible spacecraftLipschitz nonlinearitysensor faultsfunctional observeractive fault tolerant controldynamic output feedback-based FTC approach

Mathematics Subject Classification ID

Sensitivity (robustness) (93B35) Feedback control (93B52) Nonlinear systems in control theory (93C10) Variable mass, rockets (70P05)

Related Items

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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