Effect of Control Constraints on Active Stabilization of Flutter
نویسندگان
چکیده
The effect of amplitude and rate control constraints in active flutter suppression is analysed for a number of different state feedback control laws considering mathematical model of two degree-of freedom nonlinear aeroelastic airfoil system with trailing and leading edge flaps. The size of region of attraction is used as an additional metric to select a set of acceptable control laws designed by eigenstructure assignment and nonlinear dynamic inversion methods.
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