A novel nonsingular fixed-time sliding mode control for morphing aircraft with actuator faults and saturation
DOI10.1016/j.jfranklin.2024.107062zbMATH Open1543.93275MaRDI QIDQ6593757
Jialun Pu, Yu-Hao Zhang, Xiaowei Wang, Li-Tao Zhang, Naigang Cui
Publication date: 27 August 2024
Published in: Journal of the Franklin Institute (Search for Journal in Brave)
morphing aircraftactuator fault and saturation constraintcontinuous fixed-time adaptive control lawfixed-time anti-saturation compensatornovel nonsingular fixed-time sliding mode surface
Adaptive control/observation systems (93C40) Automated systems (robots, etc.) in control theory (93C85) Variable structure systems (93B12) Finite-time stability (93D40)
Cites Work
- Robust model predictive tracking control of hypersonic vehicles in the presence of actuator constraints and input delays
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- Disturbance rejection control of morphing aircraft based on switched nonlinear systems
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- Adaptive fault-tolerant attitude control for hypersonic reentry vehicle subject to complex uncertainties
- Finite-time fault-tolerant trajectory tracking control of an autonomous surface vehicle
- Adaptive sliding mode control for uncertain Euler-Lagrange systems with input saturation
- Nonlinear Feedback Design for Fixed-Time Stabilization of Linear Control Systems
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