Adaptive fault-tolerance control based finite-time backstepping for hypersonic flight vehicle with full state constrains

DOI10.1016/J.INS.2019.08.012zbMath1461.93266OpenAlexW2965599985WikidataQ127408404 ScholiaQ127408404MaRDI QIDQ1999005

Ding Zhai, Xuening Tang, Xiao-Jian Li

Publication date: 18 March 2021

Published in: Information Sciences (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/j.ins.2019.08.012

zbMATH Keywords

fuzzy logic systemhypersonic flight vehicledynamic surface controlbarrier Lyapunov functionfinite-time backsteppingfull state constrains

Mathematics Subject Classification ID

Fuzzy control/observation systems (93C42) Adaptive control/observation systems (93C40) Finite-time stability (93D40)

Related Items (14)

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Cites Work

• A novel nonlinear resilient control for a quadrotor UAV via backstepping control and nonlinear disturbance observer
• Sliding mode fuzzy control for nonlinear stochastic systems subject to pole assignment and variance constraint
• Barrier Lyapunov functions for the control of output-constrained nonlinear systems
• Adaptive output feedback fault-tolerant control design for hypersonic flight vehicles
• Output feedback adaptive sensor failure compensation for a class of parametric strict feedback systems
• Continuous finite-time control for robotic manipulators with terminal sliding mode
• Adaptive state feedback and tracking control of systems with actuator failures
• Dynamic Surface Control of Constrained Hypersonic Flight Models with Parameter Estimation and Actuator Compensation

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