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

Research output: Contribution to conference › Paper

Abstract

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.

Original language	American English
Pages	5578-5583
Number of pages	6
DOIs	https://doi.org/10.1109/IECON.2012.6389014
State	Published - 1 Dec 2012
Externally published	Yes
Event	IECON Proceedings (Industrial Electronics Conference) - Duration: 21 Dec 2016 → …

Conference

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

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10.1109/IECON.2012.6389014

Cite this

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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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