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Hidden oscillations in an active flutter suppression system and flight of a manned aircraft. / Andrievsky, Boris; Kudryashova, Elena V.; Kuznetsov, Nikolay V.; Kuznetsova, Olga A.; Mokaev, Timur N.

In: Mathematics in Engineering, Science and Aerospace, Vol. 10, No. 3, 01.01.2019, p. 357-371.

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@article{734dc827cfc44e6fa1002a7bb6371bca,
title = "Hidden oscillations in an active flutter suppression system and flight of a manned aircraft",
abstract = "In the paper, the control problem with limitations on the magnitude and rate of the control action in aircraft control systems, is studied. Existence of hidden limit cycle oscillations in the case of actuator position and rate limitations is demonstrated by the examples of piloted aircraft PIO phenomenon and the airfoil flutter suppression system.",
keywords = "Control limitations, Flutter suppression, Hidden oscillations, Limit cycle oscillation, Nonlinear dynamics, PIO",
author = "Boris Andrievsky and Kudryashova, {Elena V.} and Kuznetsov, {Nikolay V.} and Kuznetsova, {Olga A.} and Mokaev, {Timur N.}",
year = "2019",
month = jan,
day = "1",
language = "English",
volume = "10",
pages = "357--371",
journal = "Mathematics in Engineering, Science and Aerospace",
issn = "2041-3165",
publisher = "Cambridge Scientific Publishers",
number = "3",

}

RIS

TY - JOUR

T1 - Hidden oscillations in an active flutter suppression system and flight of a manned aircraft

AU - Andrievsky, Boris

AU - Kudryashova, Elena V.

AU - Kuznetsov, Nikolay V.

AU - Kuznetsova, Olga A.

AU - Mokaev, Timur N.

PY - 2019/1/1

Y1 - 2019/1/1

N2 - In the paper, the control problem with limitations on the magnitude and rate of the control action in aircraft control systems, is studied. Existence of hidden limit cycle oscillations in the case of actuator position and rate limitations is demonstrated by the examples of piloted aircraft PIO phenomenon and the airfoil flutter suppression system.

AB - In the paper, the control problem with limitations on the magnitude and rate of the control action in aircraft control systems, is studied. Existence of hidden limit cycle oscillations in the case of actuator position and rate limitations is demonstrated by the examples of piloted aircraft PIO phenomenon and the airfoil flutter suppression system.

KW - Control limitations

KW - Flutter suppression

KW - Hidden oscillations

KW - Limit cycle oscillation

KW - Nonlinear dynamics

KW - PIO

UR - http://www.scopus.com/inward/record.url?scp=85072598016&partnerID=8YFLogxK

M3 - Article

AN - SCOPUS:85072598016

VL - 10

SP - 357

EP - 371

JO - Mathematics in Engineering, Science and Aerospace

JF - Mathematics in Engineering, Science and Aerospace

SN - 2041-3165

IS - 3

ER -

ID: 50350245