Modified adaptive neural dynamic surface control for morphing aircraft with input and output constraints

DOI10.1007/s11071-016-3196-0zbMath1373.93300OpenAlexW2554872022MaRDI QIDQ1673958

Jingping Shi, Qing Zhou, Jingchao Lu, Zhonghua Wu

Publication date: 27 October 2017

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

Full work available at URL: https://doi.org/10.1007/s11071-016-3196-0

zbMATH Keywords

minimal learning parameterbarrier Lyapunov functionsinput and output constraintssliding mode differentiator

Mathematics Subject Classification ID

Lyapunov and storage functions (93D30) Design techniques (robust design, computer-aided design, etc.) (93B51) Adaptive control/observation systems (93C40) Automated systems (robots, etc.) in control theory (93C85)

Related Items (7)

Adaptive finite-time neural control of non-strict feedback systems subject to output constraint, unknown control direction, and input nonlinearities ⋮ Composite learning adaptive dynamic surface control for uncertain nonlinear strict‐feedback systems with fixed‐time parameter estimation under sufficient excitation ⋮ Nonsingular fixed‐time fault‐tolerant attitude control for tailless flying wing aircraft with time‐varying flight envelope constraints ⋮ Robust adaptive neural control of morphing aircraft with prescribed performance ⋮ Constrained adaptive neural control of nonlinear strict-feedback systems with input dead-zone ⋮ Adaptive stabilization for a class of uncertain \(p\)-normal nonlinear systems via a generalized homogeneous domination technique ⋮ Disturbance rejection control of morphing aircraft based on switched nonlinear systems

Cites Work

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