Aeroelastic Dynamic Response and Control of an Aeroelastic System with Hysteresis Nonlinearities

A state feedback control law based on the sliding mode control method is derived for the aeroelastic response and flutter suppression of a two-dimensional airfoil section with hysteresis nonlinearity in pitch. An observer is constructed to estimate the unavailable state variables of the system. With...

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Main Authors: Xingzhi Xu, Yakui Gao, Weiguo Zhang
Format: Article
Language:English
Published: Wiley 2015-01-01
Series:Journal of Control Science and Engineering
Online Access:http://dx.doi.org/10.1155/2015/258315
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author Xingzhi Xu
Yakui Gao
Weiguo Zhang
author_facet Xingzhi Xu
Yakui Gao
Weiguo Zhang
author_sort Xingzhi Xu
collection DOAJ
description A state feedback control law based on the sliding mode control method is derived for the aeroelastic response and flutter suppression of a two-dimensional airfoil section with hysteresis nonlinearity in pitch. An observer is constructed to estimate the unavailable state variables of the system. With the control law designed, nonlinear effect of time delay between the control input and actuator is investigated by a numerical approach. The closed-loop system including the observer and nonlinear controller is asymptotically stable. The simulation results show that the observer can give precise estimations for the plunge displacement and the velocities in pitch and plunge and that the controller is effective for flutter suppression. The time delay between the control input and actuator may jeopardize the control performance and cause high-frequency vibrations.
format Article
id doaj-art-a24e9ee4ee554cecbda744cdb12b2411
institution Kabale University
issn 1687-5249
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language English
publishDate 2015-01-01
publisher Wiley
record_format Article
series Journal of Control Science and Engineering
spelling doaj-art-a24e9ee4ee554cecbda744cdb12b24112025-02-03T05:53:02ZengWileyJournal of Control Science and Engineering1687-52491687-52572015-01-01201510.1155/2015/258315258315Aeroelastic Dynamic Response and Control of an Aeroelastic System with Hysteresis NonlinearitiesXingzhi Xu0Yakui Gao1Weiguo Zhang2School of Automation, Northwestern Polytechnical University, Xi’an, Shaanxi 710129, ChinaSchool of Automation, Northwestern Polytechnical University, Xi’an, Shaanxi 710129, ChinaSchool of Automation, Northwestern Polytechnical University, Xi’an, Shaanxi 710129, ChinaA state feedback control law based on the sliding mode control method is derived for the aeroelastic response and flutter suppression of a two-dimensional airfoil section with hysteresis nonlinearity in pitch. An observer is constructed to estimate the unavailable state variables of the system. With the control law designed, nonlinear effect of time delay between the control input and actuator is investigated by a numerical approach. The closed-loop system including the observer and nonlinear controller is asymptotically stable. The simulation results show that the observer can give precise estimations for the plunge displacement and the velocities in pitch and plunge and that the controller is effective for flutter suppression. The time delay between the control input and actuator may jeopardize the control performance and cause high-frequency vibrations.http://dx.doi.org/10.1155/2015/258315
spellingShingle Xingzhi Xu
Yakui Gao
Weiguo Zhang
Aeroelastic Dynamic Response and Control of an Aeroelastic System with Hysteresis Nonlinearities
Journal of Control Science and Engineering
title Aeroelastic Dynamic Response and Control of an Aeroelastic System with Hysteresis Nonlinearities
title_full Aeroelastic Dynamic Response and Control of an Aeroelastic System with Hysteresis Nonlinearities
title_fullStr Aeroelastic Dynamic Response and Control of an Aeroelastic System with Hysteresis Nonlinearities
title_full_unstemmed Aeroelastic Dynamic Response and Control of an Aeroelastic System with Hysteresis Nonlinearities
title_short Aeroelastic Dynamic Response and Control of an Aeroelastic System with Hysteresis Nonlinearities
title_sort aeroelastic dynamic response and control of an aeroelastic system with hysteresis nonlinearities
url http://dx.doi.org/10.1155/2015/258315
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AT yakuigao aeroelasticdynamicresponseandcontrolofanaeroelasticsystemwithhysteresisnonlinearities
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