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Hidden nonlinear oscillations in aircraft stabilization system with restrictions at the actuator control. / Andrievsky, Boris; Kudryashova, Elena V.; Kuznetsov, Nikolay V.; Kuznetsova, Olga A.; Mokaev, Timur N.

ICNPAA 2018 World Congress: 12th International Conference on Mathematical Problems in Engineering, Aerospace and Sciences. ed. / Seenith Sivasundaram. Vol. 2046 American Institute of Physics, 2018. 020004.

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › Research › peer-review

Harvard

Andrievsky, B, Kudryashova, EV, Kuznetsov, NV, Kuznetsova, OA & Mokaev, TN 2018, Hidden nonlinear oscillations in aircraft stabilization system with restrictions at the actuator control. in S Sivasundaram (ed.), ICNPAA 2018 World Congress: 12th International Conference on Mathematical Problems in Engineering, Aerospace and Sciences. vol. 2046, 020004, American Institute of Physics, 12th International Conference on Mathematical Problems in Engineering, Aerospace and Sciences, ICNPAA 2018, Yerevan, Armenia, 3/07/18. https://doi.org/10.1063/1.5081524

APA

Andrievsky, B., Kudryashova, E. V., Kuznetsov, N. V., Kuznetsova, O. A., & Mokaev, T. N. (2018). Hidden nonlinear oscillations in aircraft stabilization system with restrictions at the actuator control. In S. Sivasundaram (Ed.), ICNPAA 2018 World Congress: 12th International Conference on Mathematical Problems in Engineering, Aerospace and Sciences (Vol. 2046). [020004] American Institute of Physics. https://doi.org/10.1063/1.5081524

Vancouver

Andrievsky B, Kudryashova EV, Kuznetsov NV, Kuznetsova OA, Mokaev TN. Hidden nonlinear oscillations in aircraft stabilization system with restrictions at the actuator control. In Sivasundaram S, editor, ICNPAA 2018 World Congress: 12th International Conference on Mathematical Problems in Engineering, Aerospace and Sciences. Vol. 2046. American Institute of Physics. 2018. 020004 https://doi.org/10.1063/1.5081524

Author

Andrievsky, Boris ; Kudryashova, Elena V. ; Kuznetsov, Nikolay V. ; Kuznetsova, Olga A. ; Mokaev, Timur N. / Hidden nonlinear oscillations in aircraft stabilization system with restrictions at the actuator control. ICNPAA 2018 World Congress: 12th International Conference on Mathematical Problems in Engineering, Aerospace and Sciences. editor / Seenith Sivasundaram. Vol. 2046 American Institute of Physics, 2018.

BibTeX

@inproceedings{831967c03e1444dd936fb8209eb254d7,
title = "Hidden nonlinear oscillations in aircraft stabilization system with restrictions at the actuator control",
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.",
author = "Boris Andrievsky and Kudryashova, {Elena V.} and Kuznetsov, {Nikolay V.} and Kuznetsova, {Olga A.} and Mokaev, {Timur N.}",
year = "2018",
month = dec,
day = "4",
doi = "10.1063/1.5081524",
language = "English",
volume = "2046",
editor = "Seenith Sivasundaram",
booktitle = "ICNPAA 2018 World Congress",
publisher = "American Institute of Physics",
address = "United States",
note = "12th International Conference on Mathematical Problems in Engineering, Aerospace and Sciences, ICNPAA 2018 ; Conference date: 03-07-2018 Through 06-07-2018",

}

RIS

TY - GEN

T1 - Hidden nonlinear oscillations in aircraft stabilization system with restrictions at the actuator control

AU - Andrievsky, Boris

AU - Kudryashova, Elena V.

AU - Kuznetsov, Nikolay V.

AU - Kuznetsova, Olga A.

AU - Mokaev, Timur N.

PY - 2018/12/4

Y1 - 2018/12/4

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.

UR - http://www.scopus.com/inward/record.url?scp=85058710217&partnerID=8YFLogxK

U2 - 10.1063/1.5081524

DO - 10.1063/1.5081524

M3 - Conference contribution

AN - SCOPUS:85058710217

VL - 2046

BT - ICNPAA 2018 World Congress

A2 - Sivasundaram, Seenith

PB - American Institute of Physics

T2 - 12th International Conference on Mathematical Problems in Engineering, Aerospace and Sciences, ICNPAA 2018

Y2 - 3 July 2018 through 6 July 2018

ER -

ID: 38483890