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Shock and Vibration
Volume 2014, Article ID 597827, 12 pages
http://dx.doi.org/10.1155/2014/597827
Research Article

Control of Limit Cycle Oscillation in a Three Degrees of Freedom Airfoil Section Using Fuzzy Takagi-Sugeno Modeling

1Aeronautical Institute of Technology (ITA), 12 228-900 São José dos Campos, SP, Brazil
2Universidade Estadual Paulista (UNESP), 17 033-360 Bauru, SP, Brazil

Received 14 July 2013; Accepted 10 March 2014; Published 10 June 2014

Academic Editor: Miguel M. Neves

Copyright © 2014 Douglas Domingues Bueno et al. This is an open access article distributed under the Creative Commons Attribution License, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.

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