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Simple adaptive control for airfoil flutter suppression. / Andrievsky, Boris; Kudryashova, Elena V.; Kuznetsov, Nikolay V.; Kuznetsova, Olga A.; Leonov, Gennady A.

In: Mathematics in Engineering, Science and Aerospace, Vol. 9, No. 1, 01.01.2018, p. 5-20.

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

Harvard

Andrievsky, B, Kudryashova, EV, Kuznetsov, NV, Kuznetsova, OA & Leonov, GA 2018, 'Simple adaptive control for airfoil flutter suppression', Mathematics in Engineering, Science and Aerospace, vol. 9, no. 1, pp. 5-20.

APA

Andrievsky, B., Kudryashova, E. V., Kuznetsov, N. V., Kuznetsova, O. A., & Leonov, G. A. (2018). Simple adaptive control for airfoil flutter suppression. Mathematics in Engineering, Science and Aerospace, 9(1), 5-20.

Vancouver

Andrievsky B, Kudryashova EV, Kuznetsov NV, Kuznetsova OA, Leonov GA. Simple adaptive control for airfoil flutter suppression. Mathematics in Engineering, Science and Aerospace. 2018 Jan 1;9(1):5-20.

Author

Andrievsky, Boris ; Kudryashova, Elena V. ; Kuznetsov, Nikolay V. ; Kuznetsova, Olga A. ; Leonov, Gennady A. / Simple adaptive control for airfoil flutter suppression. In: Mathematics in Engineering, Science and Aerospace. 2018 ; Vol. 9, No. 1. pp. 5-20.

BibTeX

@article{4c5fe105eb9142b698161fb571fb1fc0,
title = "Simple adaptive control for airfoil flutter suppression",
abstract = "In the paper, the Simple Adaptive Control scheme based on the implicit reference model and the passification theorem is designed for active suppressing the airfoil flutter. This approach leads to low-order adaptation algorithms despite that the plant model order may be high. Another merit of such a kind of adaptive controllers is a possibility of using them for solving the stabilization problems, when the reference signal is zero. The simulation results are presented to demonstrate efficiency and robustness of the proposed adaptive controller.",
keywords = "Flutter suppression, Implicit reference model, Passification, Simple adaptive control",
author = "Boris Andrievsky and Kudryashova, {Elena V.} and Kuznetsov, {Nikolay V.} and Kuznetsova, {Olga A.} and Leonov, {Gennady A.}",
year = "2018",
month = jan,
day = "1",
language = "English",
volume = "9",
pages = "5--20",
journal = "Mathematics in Engineering, Science and Aerospace",
issn = "2041-3165",
publisher = "Cambridge Scientific Publishers",
number = "1",

}

RIS

TY - JOUR

T1 - Simple adaptive control for airfoil flutter suppression

AU - Andrievsky, Boris

AU - Kudryashova, Elena V.

AU - Kuznetsov, Nikolay V.

AU - Kuznetsova, Olga A.

AU - Leonov, Gennady A.

PY - 2018/1/1

Y1 - 2018/1/1

N2 - In the paper, the Simple Adaptive Control scheme based on the implicit reference model and the passification theorem is designed for active suppressing the airfoil flutter. This approach leads to low-order adaptation algorithms despite that the plant model order may be high. Another merit of such a kind of adaptive controllers is a possibility of using them for solving the stabilization problems, when the reference signal is zero. The simulation results are presented to demonstrate efficiency and robustness of the proposed adaptive controller.

AB - In the paper, the Simple Adaptive Control scheme based on the implicit reference model and the passification theorem is designed for active suppressing the airfoil flutter. This approach leads to low-order adaptation algorithms despite that the plant model order may be high. Another merit of such a kind of adaptive controllers is a possibility of using them for solving the stabilization problems, when the reference signal is zero. The simulation results are presented to demonstrate efficiency and robustness of the proposed adaptive controller.

KW - Flutter suppression

KW - Implicit reference model

KW - Passification

KW - Simple adaptive control

UR - http://www.scopus.com/inward/record.url?scp=85057961965&partnerID=8YFLogxK

M3 - Article

AN - SCOPUS:85057961965

VL - 9

SP - 5

EP - 20

JO - Mathematics in Engineering, Science and Aerospace

JF - Mathematics in Engineering, Science and Aerospace

SN - 2041-3165

IS - 1

ER -

ID: 38349922