Modeling and LQR Control of a Two-Dimensional Airfoil
In this paper we develop a mathematical model of a two-dimensional aeroelastic airfoil. This model is used to design a flutter suppression controller. Flutter is a vibration in a wing caused by airstream energy being absorbed by the lifting surface. Flutter increases with increasing speed. For simpl...
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| Format: | Others |
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Virginia Tech
2014
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| Online Access: | http://hdl.handle.net/10919/36668 http://scholar.lib.vt.edu/theses/available/etd-4128132049721391/ |