Minimum energy oriented global stabilizing control of the PVTOL aircraft

DOI10.1080/00207170601069505zbMath1120.93326OpenAlexW1965873406WikidataQ126268154 ScholiaQ126268154MaRDI QIDQ3447423

G. Poulin, Nicolas Marchand, Ahmed Chemori

Publication date: 19 June 2007

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

Full work available at URL: https://doi.org/10.1080/00207170601069505

zbMATH Keywords

quadratic programmingmicro arial vehiclesreceding horizon model

Mathematics Subject Classification ID

Quadratic programming (90C20) Stabilization of systems by feedback (93D15) Global stability of solutions to ordinary differential equations (34D23) Control/observation systems governed by ordinary differential equations (93C15)

Related Items (3)

Robust Stabilization of Nonlinear PVTOL Aircraft with Parameter Uncertainties ⋮ PVTOL global stabilisation using a nested saturation control ⋮ Priority altitude PVTOL aircraft control via immersion and invariance

Cites Work

• Nonlinear control design for slightly non-minimum phase systems: Application to V/STOL aircraft
• Constrained minimum-time-oriented feedback control for the stabilization of nonholonomic systems in chained form
• A different look at output tracking: Control of a VTOL aircraft
• Global stabilization of multiple integrators with bounded controls
• Optimal feedback control for route tracking with a bounded-curvature vehicle
• On Curves of Minimal Length with a Constraint on Average Curvature, and with Prescribed Initial and Terminal Positions and Tangents
• Global stabilization of a PVTOL aircraft model with bounded inputs
• Non-holonomic control systems: from steering to stabilization with sinusoids
• Global configuration stabilization for the VTOL aircraft with strong input coupling

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