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This paper proposes a novel method for the prevention of the unboundedoscillation of an aircraft wings under the flexural torsion flutter. The paperintroducing the novel multiagent method for control of an aircraft wing,assuming that the wing surface consists of controlled "feathers" (agents).Theoretical evaluation of the approach demonstrates its high ability to preventflexural-torsional vibrations of an aircraft. Since the model expands thepossibilities for damping the wing oscillations, which potentially allows anincrease in aircraft speed without misgiving of flutter. The study exhibitsthat timing is the main limitation of dampening vibrations. A new method forcontrolling an aircraft wing is suggested to increase the maximal flight speedof an aircraft without flutter occurrence via a novel model of thebending-torsional vibrations of an airplane wing with controlled feathers onits surface and new control laws based on the Speed-Gradient methodology.Provided experiments demonstrate the theoretical and advantages of themultiagent approach to "feathers" movement control.

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