Quadratic stabilization of a nonlinear aeroelastic system using a novel Neural-Network-based controller
Author:
Publisher
Springer Science and Business Media LLC
Subject
General Engineering,General Materials Science
Link
http://link.springer.com/content/pdf/10.1007/s11431-011-4346-8.pdf
Reference21 articles.
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2. Ko J, Strganac W T, Kurdila A J. Adaptive feedback linearization for the control of a typical wing section with structural nonlinearity. Nonlinear Dyn, 1999, 18: 289–301
3. Singh S N, Wang L. Output feedback form and adaptive control of a nonlinear aeroelastic system. J Guidance, Contl Dyn, 2002, 4: 725–732
4. Xing W, Singh S N. Adaptive output feedback control of a nonlinear aeroelastic structure. J Guidance Contl Dyn, 2000, 6: 1109–1116
5. Behal A, Marzocca P, Dawson D M, et al. Nonlinear adaptive model free control of an aeroelastic 2-D lifting surface. AIAA Guidance, Navigation, and Control Conference and Exhibition, AIAA-2004-5227, 2004
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