Gain-scheduled control of PVTOL aircraft dynamics with parameter-dependent disturbance

DOI10.1016/J.JFRANKLIN.2008.05.006zbMath1201.93038OpenAlexW2119007930MaRDI QIDQ602655

Koan-Yuh Chang, Sun-Li Wu, Chih-Hua Hsu, Pang-Chia Chen

Publication date: 5 November 2010

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

Full work available at URL: https://doi.org/10.1016/j.jfranklin.2008.05.006

zbMATH Keywords

disturbance attenuationLMILPV systemPVTOL aircraft

Mathematics Subject Classification ID

Nonlinear systems in control theory (93C10) Application models in control theory (93C95) (H^infty)-control (93B36) Linear systems in control theory (93C05)

Related Items (6)

LPV modeling and synthesis for DC propulsion of electric scooters ⋮ \(H_\infty\) filter design for nonlinear parameter-varying systems with quantized measurements ⋮ Stabilization of the planar vertical take‐off and landing using nonlinear feedback control ⋮ Robust feedback set stabilization of logic networks with state-dependent uncertain switching and control constraints ⋮ Priority altitude PVTOL aircraft control via immersion and invariance ⋮ The design of smooth switching control with application to V/STOL aircraft dynamics under input and output constraints

Uses Software

• LMI toolbox

Cites Work

• Unnamed Item
• Nonlinear control design for slightly non-minimum phase systems: Application to V/STOL aircraft
• Self-scheduled \({\mathcal H}_ \infty\) control of linear parameter-varying systems: A design example
• Output tracking of a non-linear non-minimum phase PVTOL aircraft based on non-linear state feedback control
• Translational Motion Control of Vertical Takeoff Aircraft Using Nonlinear Dynamic Inversion
• Linear Matrix Inequalities in System and Control Theory
• Global Stabilization of the PVTOL: Real-Time Application to A Mini-Aircraft
• Affine parameter-dependent Lyapunov functions and real parametric uncertainty
• Analysis of gain scheduled control for nonlinear plants
• A prediction‐based nonlinear controller for stabilization of a non‐minimum phase PVTOL aircraft
• Research on gain scheduling

This page was built for publication: Gain-scheduled control of PVTOL aircraft dynamics with parameter-dependent disturbance