A switched control for UAVs

R. Sandoval-Torres; M. Adam-Medina; I. Cervantes; I. A. Diaz-Diaz

doi:10.1109/IECON.2012.6389014

A switched control for UAVs

R. Sandoval-Torres, M. Adam-Medina, I. Cervantes, I. A. Diaz-Diaz

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Resumen

This paper analyzes the stability of a class of linear switched control based on a Piecewise Continuous (PWC) description of the aerial vehicle. Sufficient conditions for the existence of a common Lyapunov equation are stated for an outputdependent control law that makes use of an observer to assign closed-loop performance at each mode. The resulting scheme is able to guarantee asymptotic stability to the desired equilibrium set under arbitrary switching. The results are illustrated via numerical simulations in an airplane model. © 2012 IEEE.

Idioma original	Inglés estadounidense
Páginas	5578-5583
Número de páginas	6
DOI	https://doi.org/10.1109/IECON.2012.6389014
Estado	Publicada - 1 dic. 2012
Publicado de forma externa	Sí
Evento	IECON Proceedings (Industrial Electronics Conference) - Duración: 21 dic. 2016 → …

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Conferencia	IECON Proceedings (Industrial Electronics Conference)
Período	21/12/16 → …

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10.1109/IECON.2012.6389014

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AB - This paper analyzes the stability of a class of linear switched control based on a Piecewise Continuous (PWC) description of the aerial vehicle. Sufficient conditions for the existence of a common Lyapunov equation are stated for an outputdependent control law that makes use of an observer to assign closed-loop performance at each mode. The resulting scheme is able to guarantee asymptotic stability to the desired equilibrium set under arbitrary switching. The results are illustrated via numerical simulations in an airplane model. © 2012 IEEE.

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A switched control for UAVs

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