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NASA NTRS · 19940031368

Robust control design techniques for active flutter suppression

Abstract

In this paper, an active flutter suppression problem is studied for a thin airfoil in unsteady aerodynamics. The mathematical model of this system is infinite dimensional because of Theodorsen's function which is irrational. Several second order approximations of Theodorsen's function are compared. A finite dimensional model is obtained from such an approximation. We use H infinity control techniques to find a robustly stabilizing controller for active flutter suppression.

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BibTeXRIS

Ozbay, Hitay, Bachmann, Glen R.. 1994-06-01. Robust control design techniques for active flutter suppression. https://ntrs.nasa.gov/citations/19940031368

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