Nonlinear fuzzy fault-tolerant control of hypersonic flight vehicle with parametric uncertainty and actuator fault

DOI10.1007/S11071-018-4127-ZzbMath1398.93247OpenAlexW2793710543MaRDI QIDQ1798216

Fuyang Chen, Juan Niu, Tao, Gang

Publication date: 23 October 2018

Published in: Nonlinear Dynamics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/s11071-018-4127-z

zbMATH Keywords

sliding modefault estimationfault-tolerant controlfuzzy logic systemhypersonic flight vehicle

Mathematics Subject Classification ID

Fuzzy control/observation systems (93C42) Nonlinear systems in control theory (93C10) Automated systems (robots, etc.) in control theory (93C85)

Related Items (7)

Robust model predictive control for hypersonic vehicle with state‐dependent input constraints and parameter uncertainty ⋮ Unknown input observer synthesis for discrete-time T-S fuzzy singular systems with application to actuator fault estimation ⋮ Robust finite-time tracking for uncertain linear systems with actuator faults ⋮ Intelligent trajectory tracking of an aircraft in the presence of internal and external disturbances ⋮ Adaptive neural network finite time control for quadrotor UAV with unknown input saturation ⋮ Performance guaranteed fault-tolerant control of robotic manipulators under actuator faults and motion constraints ⋮ Constrained fault-tolerant control for hypersonic vehicle subject to actuator failure and with unmeasurable states

Cites Work

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• Adaptive sliding mode tracking control for a flexible air-breathing hypersonic vehicle
• Sliding mode observers for fault detection and isolation
• Direct adaptive type-2 fuzzy neural network control for a generic hypersonic flight vehicle
• Robust adaptive neural control of flexible hypersonic flight vehicle with dead-zone input nonlinearity
• Dynamic surface control based on neural network for an air-breathing hypersonic vehicle
• Design of Robust Control Systems for a Hypersonic Aircraft

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