Friction compensation of an aeroelastic wing - A TP model transformation based approach

Bela Takarics, Patrícia Gróf, Péter Baranyi, Péter Korondi

Research output: Chapter in Book/Report/Conference proceedingConference contribution

3 Scopus citations

Abstract

Various approaches to control aeroelastic wing section with structural nonlinearity emerged in the last years. One of the approaches is based on the Tensor Product (TP) model transformation and the feasibility test of linear matrix inequalities (LMIs) under the Parallel Distributed Compensation framework. The main contribution of this paper is that it extends the previously established qLPV model of the aeroelastic wing section with nonlinear friction. It is proven that the extended model can be exactly described after TP type polytopic decomposition. The qLPV model of the aeroelastic wing section with Coulomb friction was transformed to TP type polytopic model form for which LMI based controller was designed. The designed controller is compared to controllers of other authors dealing with the same problem.

Original languageEnglish (US)
Title of host publicationSIISY 2010 - 8th IEEE International Symposium on Intelligent Systems and Informatics
Pages527-533
Number of pages7
DOIs
StatePublished - Dec 30 2010
Event8th IEEE International Symposium on Intelligent Systems and Informatics, SIISY 2010 - Subotica, Serbia
Duration: Sep 10 2010Sep 11 2010

Publication series

NameSIISY 2010 - 8th IEEE International Symposium on Intelligent Systems and Informatics

Other

Other8th IEEE International Symposium on Intelligent Systems and Informatics, SIISY 2010
CountrySerbia
CitySubotica
Period9/10/109/11/10

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