Determination of the stability parameter space of a two dimensional aeroelastic system, a TP model-based approach

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

8 Citations (Scopus)

Abstract

This paper falls in the topic of qLPV state-space model based control design in which LMIs are used to optimize the multi-objective control performance. In this paper we investigate how the convex hull of the polytopic model influences the feasibility of the LMI based control design and the resulting control performances. We examine these influences through the control design of the two dimensional aeroelastic system's example. First we define various TP type polytopic model representations of a wing section whose vertices define different convex hulls. In the second step we investigate how these models lead to different control performances.

Original languageEnglish
Title of host publicationINES 2010 - 14th International Conference on Intelligent Engineering Systems, Proceedings
Pages265-270
Number of pages6
DOIs
Publication statusPublished - Jul 26 2010
Event14th International Conference on Intelligent Engineering Systems, INES 2010 - Las Palmas of Gran Canaria, Spain
Duration: May 5 2010May 7 2010

Publication series

NameINES 2010 - 14th International Conference on Intelligent Engineering Systems, Proceedings

Other

Other14th International Conference on Intelligent Engineering Systems, INES 2010
CountrySpain
CityLas Palmas of Gran Canaria
Period5/5/105/7/10

ASJC Scopus subject areas

  • Artificial Intelligence
  • Information Systems

Cite this

Gróf, P., Baranyi, P., & Korondi, P. (2010). Determination of the stability parameter space of a two dimensional aeroelastic system, a TP model-based approach. In INES 2010 - 14th International Conference on Intelligent Engineering Systems, Proceedings (pp. 265-270). [5483836] (INES 2010 - 14th International Conference on Intelligent Engineering Systems, Proceedings). https://doi.org/10.1109/INES.2010.5483836