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    A Feedback Linearization Approach for Panel Flutter Suppression With Piezoelectric Actuation

    Source: Journal of Computational and Nonlinear Dynamics:;2011:;volume( 006 ):;issue: 003::page 31006
    Author:
    Oluseyi O. Onawola
    ,
    S. C. Sinha
    DOI: 10.1115/1.4002391
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Panel flutter suppression by exact state transformations and feedback control using piezoelectric actuation is presented. A nonlinear control system is designed for a simply supported rectangular panel with bonded piezoelectric layers based on the von Kármán large-deflection plate theory. The governing nonlinear partial differential equation for the panel is reduced to a set of ordinary differential equations using a two mode approximation. Distributed piezoelectric actuators and sensors connected to processing networks are used as modal actuators and sensors to actively control panel vibrations. The control inputs are given by the electric fields required to drive the actuators based on piezoelectric actuation. Nonlinear feedback control laws are formulated through a transformation of the discretized nonlinear system into an equivalent controllable linear system. The simulated results show that the resulting closed-loop system based on feedback linearized controllers effectively suppress panel flutter limit-cycle motions.
    keyword(s): Flutter (Aerodynamics) , Feedback , Deflection , Control equipment , Actuators , Stress AND Sensors ,
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      A Feedback Linearization Approach for Panel Flutter Suppression With Piezoelectric Actuation

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    http://yetl.yabesh.ir/yetl1/handle/yetl/145536
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    contributor authorOluseyi O. Onawola
    contributor authorS. C. Sinha
    date accessioned2017-05-09T00:42:41Z
    date available2017-05-09T00:42:41Z
    date copyrightJuly, 2011
    date issued2011
    identifier issn1555-1415
    identifier otherJCNDDM-25779#031006_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/145536
    description abstractPanel flutter suppression by exact state transformations and feedback control using piezoelectric actuation is presented. A nonlinear control system is designed for a simply supported rectangular panel with bonded piezoelectric layers based on the von Kármán large-deflection plate theory. The governing nonlinear partial differential equation for the panel is reduced to a set of ordinary differential equations using a two mode approximation. Distributed piezoelectric actuators and sensors connected to processing networks are used as modal actuators and sensors to actively control panel vibrations. The control inputs are given by the electric fields required to drive the actuators based on piezoelectric actuation. Nonlinear feedback control laws are formulated through a transformation of the discretized nonlinear system into an equivalent controllable linear system. The simulated results show that the resulting closed-loop system based on feedback linearized controllers effectively suppress panel flutter limit-cycle motions.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleA Feedback Linearization Approach for Panel Flutter Suppression With Piezoelectric Actuation
    typeJournal Paper
    journal volume6
    journal issue3
    journal titleJournal of Computational and Nonlinear Dynamics
    identifier doi10.1115/1.4002391
    journal fristpage31006
    identifier eissn1555-1423
    keywordsFlutter (Aerodynamics)
    keywordsFeedback
    keywordsDeflection
    keywordsControl equipment
    keywordsActuators
    keywordsStress AND Sensors
    treeJournal of Computational and Nonlinear Dynamics:;2011:;volume( 006 ):;issue: 003
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
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