Multiagent Control of Airplane Wing Stability with “Feathers” under the Flexural Torsional Flutter

This paper proposes a novel method for the unbounded oscillation prevention of an aircraft wing under flexural torsional flutter, innovative multiagent attitude to control with surface consisting managed rotating “feathers” (agents). Theoretical evaluation demonstrates its high aptitude avoid wing’s flexural-torsional vibrations via expansion model’s ability dampen oscillations. It potentially allows increasing aircraft’s speed without misgiving flutter. A new way based on Speed-Gradient methodology is suggested increase maximal possible flight flutter occurrence. Provided experiments demonstrate theoretical advantage approach rotation control.