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

Author

Listed:
  • Dmitry Shalymov

    (Department of Mathematics and Computer Science, St. Petersburg State University, Universitetskaya nab. 7-9, 199034 Saint Petersburg, Russia
    These authors contributed equally to this work.)

  • Oleg Granichin

    (Mathematics and Mechanics Faculty, St. Petersburg State University, Universitetskaya nab. 7-9, 199034 Saint Petersburg, Russia
    Science Research and Educational Center “Mathematical Robotics and Artificial Intelligence”, St. Petersburg State University, Universitetskaya nab. 7-9, 199034 Saint Petersburg, Russia
    Laboratory “Control of Complex Systems”, Institute for Problems in Mechanical Engineering of Russian Academy of Sciences, V.O. Bolshoj pr. 61, 199178 Saint Petersburg, Russia
    These authors contributed equally to this work.)

  • Yury Ivanskiy

    (Science Research and Educational Center “Mathematical Robotics and Artificial Intelligence”, St. Petersburg State University, Universitetskaya nab. 7-9, 199034 Saint Petersburg, Russia
    Laboratory “Control of Complex Systems”, Institute for Problems in Mechanical Engineering of Russian Academy of Sciences, V.O. Bolshoj pr. 61, 199178 Saint Petersburg, Russia
    Faculty of Economics, St. Petersburg State University, Universitetskaya nab. 7-9, 199034 Saint Petersburg, Russia
    These authors contributed equally to this work.)

  • Zeev Volkovich

    (Software Engineering Department, Ort Braude College, Ort Braude College, Rehov Snunit 51, POB 78, Karmiel 2161002, Israel
    These authors contributed equally to this work.)

Abstract

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

Suggested Citation

  • Dmitry Shalymov & Oleg Granichin & Yury Ivanskiy & Zeev Volkovich, 2022. "Multiagent Control of Airplane Wing Stability with “Feathers” under the Flexural Torsional Flutter," Mathematics, MDPI, vol. 10(2), pages 1-19, January.
    • Handle: RePEc:gam:jmathe:v:10:y:2022:i:2:p:236-:d:723526
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