Flutter supression via delayed feedback control

【Author】

Zaihua Wang;Miao Li;

【Abstract】

<正>This paper investigates the delay effect on the stability of the controlled two-dimensional airfoil with delayed feedbacks,arising from the problem of flutter suppression of aircraft wings,where the feedback gain is allowed to be both negative and positive. Based on the stability analysis of the controlled system,it shows that a delayed position feedback with positive gain is superior to

【Keywords】

Flutter supression via delayed feedback control;

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