DocumentCode :
550726
Title :
A blending method control of switched LPV systems with slow-varying parameters and its application to an F-16 aircraft model
Author :
He Xu ; Zhao Jun ; Dimirovski, Georgi M.
Author_Institution :
State Key Lab. of Integrated Autom. for Process Ind., Northeastern Univ., Shenyang, China
fYear :
2011
fDate :
22-24 July 2011
Firstpage :
1765
Lastpage :
1770
Abstract :
This paper presents a controller design method using a blending method based on a common Lyapunov function for the induced L2-norm problem for switched linear parameter varying (LPV) systems with slowly-varying parameters. The parameter region is divided into two overlapped subsets, and Lyapunov existence conditions are proposed in terms of linear matrix inequalities (LMIs) for each subset. Based on each Lyapunov function in each subset, the blending method is used to construct a blended Lyapunov function for the whole parameter set. The proposed method is applied to an F-16 aircraft longitudinal model and simulation result demonstrate the effectiveness of the approach.
Keywords :
Lyapunov matrix equations; aircraft control; control system synthesis; linear systems; military aircraft; time-varying systems; F-16 aircraft longitudinal model; blended Lyapunov function; blending method control; controller design method; induced L2-norm problem; linear matrix inequalities; overlapped subsets; slow-varying parameter; switched linear parameter varying system; Aerospace control; Aircraft; Atmospheric modeling; Linear matrix inequalities; Lyapunov methods; Switches; Blending method; F-16 aircraft; Induced ℒ2-norm; Switched LPV systems;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Control Conference (CCC), 2011 30th Chinese
Conference_Location :
Yantai
ISSN :
1934-1768
Print_ISBN :
978-1-4577-0677-6
Electronic_ISBN :
1934-1768
Type :
conf
Filename :
6001065
Link To Document :
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