Anti-windup design for input-coupled double integrator systems with application to quadrotor UAV's

DOI10.1016/J.EJCON.2017.07.002zbMath1380.93111OpenAlexW2744103164MaRDI QIDQ682847

Matthew C. Turner, Nkemdilim A. Ofodile

Publication date: 5 February 2018

Published in: European Journal of Control (Search for Journal in Brave)

Full work available at URL: http://hdl.handle.net/2381/40532

zbMATH Keywords

nonlinear controlaerospace applicationsactuator saturationantiwindup (AW) compensator designquadrotor unmanned air vehicles (UAVs)

Mathematics Subject Classification ID

Nonlinear systems in control theory (93C10) Automated systems (robots, etc.) in control theory (93C85) Asymptotic stability in control theory (93D20)

Related Items (3)

Static anti-windup compensator for nonlinear systems with both state and input time-varying delays ⋮ Adaptive neural network finite time control for quadrotor UAV with unknown input saturation ⋮ Distributed anti-windup approach for consensus tracking of second-order multi-agent systems with input saturation

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