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- W1521837462 abstract "In this paper we study the problem of active feedback controller design for a thin airfoil, whose mathematical model is derived from classical Theodorsen's formulation. A finite dimensional controller stabilizing the original infinite dimensional model is obtained using H <sup xmlns:mml=http://www.w3.org/1998/Math/MathML xmlns:xlink=http://www.w3.org/1999/xlink>∞</sup> control techniques. We also consider the gust alleviation problem, and show that it can be formulated as a disturbance attenuation problem in the mixed H <sup xmlns:mml=http://www.w3.org/1998/Math/MathML xmlns:xlink=http://www.w3.org/1999/xlink>2</sup> /H <sup xmlns:mml=http://www.w3.org/1998/Math/MathML xmlns:xlink=http://www.w3.org/1999/xlink>∞</sup> control framework. We use existing results on H <sup xmlns:mml=http://www.w3.org/1998/Math/MathML xmlns:xlink=http://www.w3.org/1999/xlink>∞</sup> and mixed H <sup xmlns:mml=http://www.w3.org/1998/Math/MathML xmlns:xlink=http://www.w3.org/1999/xlink>2</sup> /H <sup xmlns:mml=http://www.w3.org/1998/Math/MathML xmlns:xlink=http://www.w3.org/1999/xlink>∞</sup> control to illustrate our approach with a numerical example." @default.
- W1521837462 created "2016-06-24" @default.
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- W1521837462 date "1993-06-01" @default.
- W1521837462 modified "2023-09-23" @default.
- W1521837462 title "Active Feedback Controller Design for a Thin Airfoil" @default.
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- W1521837462 doi "https://doi.org/10.23919/acc.1993.4792792" @default.
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