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Multiagent Control of Airplane Wing Stability with “Feathers” under the Flexural Torsional Flutter. / Shalymov, Dmitry; Granichin, Oleg; Ivanskiy, Yury; Volkovich, Zeev.

In: Mathematics, Vol. 10, No. 2, 236, 13.01.2022.

Research output: Contribution to journal › Article › peer-review

Harvard

Shalymov, D, Granichin, O, Ivanskiy, Y & Volkovich, Z 2022, 'Multiagent Control of Airplane Wing Stability with “Feathers” under the Flexural Torsional Flutter', Mathematics, vol. 10, no. 2, 236. https://doi.org/10.3390/math10020236

APA

Shalymov, D., Granichin, O., Ivanskiy, Y., & Volkovich, Z. (2022). Multiagent Control of Airplane Wing Stability with “Feathers” under the Flexural Torsional Flutter. Mathematics, 10(2), [236]. https://doi.org/10.3390/math10020236

Vancouver

Shalymov D, Granichin O, Ivanskiy Y, Volkovich Z. Multiagent Control of Airplane Wing Stability with “Feathers” under the Flexural Torsional Flutter. Mathematics. 2022 Jan 13;10(2). 236. https://doi.org/10.3390/math10020236

Author

Shalymov, Dmitry ; Granichin, Oleg ; Ivanskiy, Yury ; Volkovich, Zeev. / Multiagent Control of Airplane Wing Stability with “Feathers” under the Flexural Torsional Flutter. In: Mathematics. 2022 ; Vol. 10, No. 2.

BibTeX

@article{de22ef18764643f0918345b27e2bc7cd,
title = "Multiagent Control of Airplane Wing Stability with “Feathers” under the Flexural Torsional Flutter",
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{\textquoteright}s flexural-torsional vibrations via expansion of the model{\textquoteright}s ability to dampen the wing oscillations. It potentially allows increasing an aircraft{\textquoteright}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.",
keywords = "Flexural-torsional vibrations of an aircraft, Flutter, Multiagent system, Speed-gradient method, Wing with feathers, flutter, speed-gradient method, ADAPTIVE-CONTROL, SUPPRESSION, flexural-torsional vibrations of an aircraft, wing with feathers, multiagent system",
author = "Dmitry Shalymov and Oleg Granichin and Yury Ivanskiy and Zeev Volkovich",
note = "Shalymov, D.; Granichin, O.; Ivanskiy, Y.; Volkovich, Z. Multiagent Control of Airplane Wing Stability with “Feathers” under the Flexural Torsional Flutter. Mathematics 2022, 10, 236. https://doi.org/10.3390/math10020236",
year = "2022",
month = jan,
day = "13",
doi = "10.3390/math10020236",
language = "English",
volume = "10",
journal = "Mathematics",
issn = "2227-7390",
publisher = "MDPI AG",
number = "2",

}

RIS

TY - JOUR

T1 - Multiagent Control of Airplane Wing Stability with “Feathers” under the Flexural Torsional Flutter

AU - Shalymov, Dmitry

AU - Granichin, Oleg

AU - Ivanskiy, Yury

AU - Volkovich, Zeev

N1 - Shalymov, D.; Granichin, O.; Ivanskiy, Y.; Volkovich, Z. Multiagent Control of Airplane Wing Stability with “Feathers” under the Flexural Torsional Flutter. Mathematics 2022, 10, 236. https://doi.org/10.3390/math10020236

PY - 2022/1/13

Y1 - 2022/1/13

N2 - 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.

AB - 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.

KW - Flexural-torsional vibrations of an aircraft

KW - Flutter

KW - Multiagent system

KW - Speed-gradient method

KW - Wing with feathers

KW - flutter

KW - speed-gradient method

KW - ADAPTIVE-CONTROL

KW - SUPPRESSION

KW - flexural-torsional vibrations of an aircraft

KW - wing with feathers

KW - multiagent system

UR - http://www.scopus.com/inward/record.url?scp=85123002070&partnerID=8YFLogxK

UR - https://www.mendeley.com/catalogue/8b0bc4da-8b96-3ea7-ad9d-c2c1a77671d7/

U2 - 10.3390/math10020236

DO - 10.3390/math10020236

M3 - Article

AN - SCOPUS:85123002070

VL - 10

JO - Mathematics

JF - Mathematics

SN - 2227-7390

IS - 2

M1 - 236

ER -

ID: 88750672