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

Béla Takarics; Patrícia Gróf; Péter Baranyi; Péter Korondi

doi:10.1109/SISY.2010.5647078

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

Béla Takarics, Patrícia Gróf, Péter Baranyi, Péter Korondi

Research output: Chapter in Book/Report/Conference proceeding › Conference 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 language	English (US)
Title of host publication	SIISY 2010 - 8th IEEE International Symposium on Intelligent Systems and Informatics
Pages	527-533
Number of pages	7
DOIs	https://doi.org/10.1109/SISY.2010.5647078
State	Published - 2010
Externally published	Yes
Event	8th IEEE International Symposium on Intelligent Systems and Informatics, SIISY 2010 - Subotica, Serbia Duration: Sep 10 2010 → Sep 11 2010

Publication series

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

Other

Other	8th IEEE International Symposium on Intelligent Systems and Informatics, SIISY 2010
Country/Territory	Serbia
City	Subotica
Period	9/10/10 → 9/11/10

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10.1109/SISY.2010.5647078

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Takarics, B., Gróf, P., Baranyi, P., & Korondi, P. (2010). Friction compensation of an aeroelastic wing - A TP model transformation based approach. In SIISY 2010 - 8th IEEE International Symposium on Intelligent Systems and Informatics (pp. 527-533). Article 5647078 (SIISY 2010 - 8th IEEE International Symposium on Intelligent Systems and Informatics). https://doi.org/10.1109/SISY.2010.5647078

Friction compensation of an aeroelastic wing - A TP model transformation based approach. / Takarics, Béla; Gróf, Patrícia; Baranyi, Péter et al.
SIISY 2010 - 8th IEEE International Symposium on Intelligent Systems and Informatics. 2010. p. 527-533 5647078 (SIISY 2010 - 8th IEEE International Symposium on Intelligent Systems and Informatics).

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

Takarics, B, Gróf, P, Baranyi, P & Korondi, P 2010, Friction compensation of an aeroelastic wing - A TP model transformation based approach. in SIISY 2010 - 8th IEEE International Symposium on Intelligent Systems and Informatics., 5647078, SIISY 2010 - 8th IEEE International Symposium on Intelligent Systems and Informatics, pp. 527-533, 8th IEEE International Symposium on Intelligent Systems and Informatics, SIISY 2010, Subotica, Serbia, 9/10/10. https://doi.org/10.1109/SISY.2010.5647078

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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.",

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AB - 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.

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

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