Adaptive Suppression of Wing Flutter under Actuator Saturation and Time Sampling

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Adaptive Suppression of Wing Flutter under Actuator Saturation and Time Sampling. / Kuznetsov, Nikolay V.; Andrievsky, Boris ; Zaitceva, Iuliia ; Kudryashova, Elena V.; Kuznetsova, Olga A.

In: IFAC-PapersOnLine, Vol. 55, No. 12, 2022, p. 689-694.

Research output: Contribution to journal › Conference article › peer-review

BibTeX

@article{4df8b91f4703438f9dcf1e98c779b910,

title = "Adaptive Suppression of Wing Flutter under Actuator Saturation and Time Sampling",

abstract = "In the paper, a digital control law for adaptive suppression of the flexural-torsional wing flutter has been developed and analyzed. The control law uses measurements of the wing twist angle ({"}angle of attack{"}) and its time derivative. The implicit reference model (IRM) method was used for the synthesis of the so-called {"}simple adaptive controller{"} (SAC). A new modification of the adaptive control on the condition of unmodeled servo drive dynamics, time sampling, and boundedness of the control action (the controlling surface deflection) has been developed and studied under parameter variations. The admissible ranges for the values of the mentioned factors are numerically found. The analysis of hidden oscillations in a closed-loop adaptive system caused by the saturation of the control action is carried out. The simulation results demonstrate the robustness of the proposed simple adaptive controller in a wide range of system parameters in the presence of unmodeled system dynamics.",

keywords = "hidden oscillations, implicit reference model, passification, sampling control, simple adaptive control, wing flutter",

author = "Kuznetsov, {Nikolay V.} and Boris Andrievsky and Iuliia Zaitceva and Kudryashova, {Elena V.} and Kuznetsova, {Olga A.}",

note = "Publisher Copyright: {\textcopyright} 2022 Elsevier B.V.. All rights reserved.; 14th IFAC Workshop on Adaptive and Learning Control Systems, ALCOS 2022 ; Conference date: 29-06-2022 Through 01-07-2022",

year = "2022",

doi = "10.1016/j.ifacol.2022.07.392",

language = "English",

volume = "55",

pages = "689--694",

journal = "IFAC-PapersOnLine",

issn = "2405-8971",

publisher = "Elsevier",

number = "12",

}

RIS

TY - JOUR

T1 - Adaptive Suppression of Wing Flutter under Actuator Saturation and Time Sampling

AU - Kuznetsov, Nikolay V.

AU - Andrievsky, Boris

AU - Zaitceva, Iuliia

AU - Kudryashova, Elena V.

AU - Kuznetsova, Olga A.

PY - 2022

Y1 - 2022

N2 - In the paper, a digital control law for adaptive suppression of the flexural-torsional wing flutter has been developed and analyzed. The control law uses measurements of the wing twist angle ("angle of attack") and its time derivative. The implicit reference model (IRM) method was used for the synthesis of the so-called "simple adaptive controller" (SAC). A new modification of the adaptive control on the condition of unmodeled servo drive dynamics, time sampling, and boundedness of the control action (the controlling surface deflection) has been developed and studied under parameter variations. The admissible ranges for the values of the mentioned factors are numerically found. The analysis of hidden oscillations in a closed-loop adaptive system caused by the saturation of the control action is carried out. The simulation results demonstrate the robustness of the proposed simple adaptive controller in a wide range of system parameters in the presence of unmodeled system dynamics.

AB - In the paper, a digital control law for adaptive suppression of the flexural-torsional wing flutter has been developed and analyzed. The control law uses measurements of the wing twist angle ("angle of attack") and its time derivative. The implicit reference model (IRM) method was used for the synthesis of the so-called "simple adaptive controller" (SAC). A new modification of the adaptive control on the condition of unmodeled servo drive dynamics, time sampling, and boundedness of the control action (the controlling surface deflection) has been developed and studied under parameter variations. The admissible ranges for the values of the mentioned factors are numerically found. The analysis of hidden oscillations in a closed-loop adaptive system caused by the saturation of the control action is carried out. The simulation results demonstrate the robustness of the proposed simple adaptive controller in a wide range of system parameters in the presence of unmodeled system dynamics.

KW - hidden oscillations

KW - implicit reference model

KW - passification

KW - sampling control

KW - simple adaptive control

KW - wing flutter

UR - http://www.scopus.com/inward/record.url?scp=85137165176&partnerID=8YFLogxK

UR - https://www.mendeley.com/catalogue/3cfb8045-7a50-3b08-a853-bd700a361dbe/

U2 - 10.1016/j.ifacol.2022.07.392

DO - 10.1016/j.ifacol.2022.07.392

M3 - Conference article

AN - SCOPUS:85137165176

VL - 55

SP - 689

EP - 694

JO - IFAC-PapersOnLine

JF - IFAC-PapersOnLine

SN - 2405-8971

IS - 12

T2 - 14th IFAC Workshop on Adaptive and Learning Control Systems, ALCOS 2022

Y2 - 29 June 2022 through 1 July 2022

ER -

ID: 97331852