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

Author:

Shalymov DmitryORCID,Granichin OlegORCID,Ivanskiy YuryORCID,Volkovich ZeevORCID

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.

Funder

Russian Science Foundation

St Petersburg University

Publisher

MDPI AG

Subject

General Mathematics,Engineering (miscellaneous),Computer Science (miscellaneous)

Reference49 articles.

1. Aerodinamika i Dinamika Poleta Magistralnykh Samoletov [Aerodynamics and Flight Dynamics of Long Haul Aircraft];Byushgens,1995

2. Introduction to Aircraft Aeroelasticity and Loads;Wright,2008

3. An Introduction to the Theory of Aeroelasticity;Fung,2008

4. Aircraft Active Flutter Suppression: State of the Art and Technology Maturation Needs

5. Aeroelasticity;Bisplinghoff,1955

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