Application of LPV modeling, design and analysis methods to a re-entry vehicle

A. Marcos, J. Veenman, C.W. Scherer, G. De Zaiacomo, D. Mostaza, M. Kerr, H. Koroglu, S. Bennani

Research output: Chapter in Book/Report/Conference proceedingConference contributionAcademicpeer-review

16 Citations (Scopus)

Abstract

In this paper the application of linear parameter varying (LPV) modeling, design and analysis methods to a re-entry vehicle is presented The selected atmospheric re-entry benchmaik includes full nonlinear motion, a detailed aerodynamic database (from hypersonic to subsonic), relevant actuator and sensor models and physically-meaningful aerodynamic and parametric uncertainty profiles The results show that (i) LPV controller design methods can solve gain-scheduling problems in a very effective manner, (ii) integral quadratic constraint (IQC) analysis methods can be used very efficiently to accurately interpret the nonlinear time domain simulation results, and, (iii) the use of linear fractional transfoi mation (LFT) and LPV modeling representations are key to a successful analysis
Original languageEnglish
Title of host publicationProceedings of the AIAA Guidance, Navigation and Control Conference, AIAA 2010, August 2-5, 2010, Toronto, Canada
Place of PublicationWashington
PublisherAmerican Institute of Aeronautics and Astronautics Inc. (AIAA)
Pages8192-1/18
Publication statusPublished - 2010

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