A novel \(\mathcal{L}_1\) adaptive-hybrid control with guaranteed stability for a class of uncertain nonlinear systems: a case study on SA330 Puma

DOI10.1016/j.jfranklin.2022.07.009zbMath1501.93076OpenAlexW4286267083MaRDI QIDQ2096116

Yanyan Li

Publication date: 16 November 2022

Published in: Journal of the Franklin Institute (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/j.jfranklin.2022.07.009

zbMATH Keywords

helicopter controladaptive-hybrid controlnonlinear non-minimum phase MIMO system

Mathematics Subject Classification ID

Nonlinear systems in control theory (93C10) Control/observation systems with incomplete information (93C41) Multivariable systems, multidimensional control systems (93C35) Adaptive control/observation systems (93C40) Lyapunov and other classical stabilities (Lagrange, Poisson, (L^p, l^p), etc.) in control theory (93D05) Control/observation systems governed by functional relations other than differential equations (such as hybrid and switching systems) (93C30)

Cites Work

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• Stochastic piecewise affine control with application to pitch control of helicopter
• Controllers for reachability specifications for hybrid systems
• Hybrid dynamical systems. Observation and control
• ℒ₁Adaptive Control Theory
• Multiple Lyapunov functions and other analysis tools for switched and hybrid systems
• A novel hybrid model predictive control design with application to a quadrotor helicopter
• Nonlinear sliding sector design for multi‐input systems with application to helicopter control
• Optimal model-free backstepping control for a quadrotor helicopter

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