Fault-tolerant anti-windup control for hypersonic vehicles in reentry based on ISMDO

DOI10.1016/j.jfranklin.2017.12.004zbMath1393.93028OpenAlexW2779044703MaRDI QIDQ1661704

Ruiyun Qi, Bin Jiang, Yizhen Meng, Jian-wei Liu

Publication date: 17 August 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.2017.12.004

zbMATH Keywords

strong nonlinearityterminal sliding mode controlextreme large flight scalefault-tolerant anti-windup controlhypersonic vehicle (HSV)improved sliding mode disturbance observer (ISMDO)

Mathematics Subject Classification ID

Sensitivity (robustness) (93B35) Nonlinear systems in control theory (93C10) Estimation and detection in stochastic control theory (93E10) Observability (93B07) Variable structure systems (93B12)

Related Items (9)

Adaptive fault-tolerant attitude control for hypersonic reentry vehicle subject to complex uncertainties ⋮ Improved fault detection and control allocation for hypersonic re‐entry vehicle subject to intermittent fault and disturbance ⋮ Anti-disturbance control for HVs system subject to nonlinear actuator characteristics with extended state observer ⋮ Predefined performance adaptive control of robotic manipulators with dynamic uncertainties and input saturation constraints ⋮ Fault‐tolerant spacecraft attitude control under actuator saturation and without angular velocity ⋮ A sliding mode fault compensation scheme for a coupled rigid-flexible system in PDE-ODE form ⋮ Adaptive diagnosis and compensation for hypersonic flight vehicle with multisensor faults ⋮ Fault-tolerant safe control design of switched and interconnected nonlinear systems ⋮ Constrained fault-tolerant control for hypersonic vehicle subject to actuator failure and with unmeasurable states

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