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This paper proposes a novel method for prevention of the increasingoscillation of an aircraft wing under the flexural torsion flutter. The paperintroduces the novel multi-agent 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. Our model expands thepossibilities for damping the wing oscillations, which potentially allows anincrease in aircraft speed without misgiving of flutter. The study shows thatthe main limitation is the time, during which the system is able to dampvibrations to a safe level and keep them. The relevance of this indicator isimportant because of the rather fast process of increasing wing oscillationsduring flutter. In this paper, we suggest a new method for controlling anaircraft wing, with the use of which it becomes theoretically possible toincrease the maximum flight speed of an aircraft without flutter occurrence. Amathematical model of the bending-torsional vibrations of an airplane wing withcontrolled feathers on its surface is presented. Based on the Speed-Gradientmethod a new control laws are synthesized.

Multi-agent control of airplane wing stability under the flexural torsion flutter