LPV model reduction methods for aeroelastic structures * *The research leading to these results is part of the FLEXOP project. This project has received funding from the European Unions Horizon 2020 research and innovation programme under grant agreement No 636307.-Reference-Cited by-同舟云学术

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LPV model reduction methods for aeroelastic structures * *The research leading to these results is part of the FLEXOP project. This project has received funding from the European Unions Horizon 2020 research and innovation programme under grant agreement No 636307.

Published:2017-07 Issue:1 Volume:50 Page:6344-6349
ISSN:2405-8963
Container-title:IFAC-PapersOnLine
language:en
Short-container-title:IFAC-PapersOnLine

Author:

Lipták Gy.,Luspay T.,Péni T.,Takarics B.,Vanek B.

Publisher

Elsevier BV

Subject

Control and Systems Engineering

Reference20 articles.

1. Reduced-order LPV model of flexible wind turbines from high fidelity aeroelastic codes;Adegas;In IEEE Conference on Control Applications,2013

2. A doublet-lattice method for calculating lift distributions on oscillating surfaces in subsonic flows;Albano;Journal of Aircraft,1969

3. Approximation of Large-Scale Dynamical Systems. Advances in Design and Control;Antoulas,2005

4. Balas, G., Hjartarson, A., Packard, A., and Seiler, P. (2015). LPVTools: A Toolbox for Modeling, Analysis, and Synthesis of Parameter Varying Control Systems. Musyn, Inc. URL http://www.aem.umn.edu/~SeilerControl/software.shtml.

5. Aeroelasticity;Bisplinghoff,1955

Cited by 1 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Ground Testing of the FLEXOP Demonstrator Aircraft;AIAA Scitech 2020 Forum;2020-01-05

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