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    Active Vibration Damping of Composite Beam using Smart Sensors and Actuators

    Source: Journal of Aerospace Engineering:;2002:;Volume ( 015 ):;issue: 003
    Author:
    G. Song
    ,
    P. Z. Qiao
    ,
    W. K. Binienda
    ,
    G. P. Zou
    DOI: 10.1061/(ASCE)0893-1321(2002)15:3(97)
    Publisher: American Society of Civil Engineers
    Abstract: This paper discusses active vibration control of an E-glass/epoxy-laminated composite beam using smart sensors and actuators. The smart sensors and actuators used in this study are piezoelectric ceramic patches. The composite beam is in a cantilevered configuration. Both theoretical and numerical (finite-element analysis) studies of the laminated composite beam are conducted to reveal the beam’s fundamental modal frequencies and modal shapes. The results based on the theoretical predication and numerical simulation are then compared with those from experimental modal testing, and a good correlation is obtained. Utilizing results from the model analysis and experimental modal testing, two control algorithms, namely, positive position feedback control and strain rate feedback control, are designed. Both single-mode vibration suppression and multimode vibration suppression are studied. An experimental apparatus has been developed to implement the control algorithms. The apparatus consists of a voltage amplifier and a data acquisition and real-time control system, in addition to the composite beam with bonded piezoelectric ceramic sensors and actuators. Experiments show that the proposed controllers can achieve active vibration damping of the composite beam.
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      Active Vibration Damping of Composite Beam using Smart Sensors and Actuators

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/44969
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    • Journal of Aerospace Engineering

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    contributor authorG. Song
    contributor authorP. Z. Qiao
    contributor authorW. K. Binienda
    contributor authorG. P. Zou
    date accessioned2017-05-08T21:16:07Z
    date available2017-05-08T21:16:07Z
    date copyrightJuly 2002
    date issued2002
    identifier other%28asce%290893-1321%282002%2915%3A3%2897%29.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/44969
    description abstractThis paper discusses active vibration control of an E-glass/epoxy-laminated composite beam using smart sensors and actuators. The smart sensors and actuators used in this study are piezoelectric ceramic patches. The composite beam is in a cantilevered configuration. Both theoretical and numerical (finite-element analysis) studies of the laminated composite beam are conducted to reveal the beam’s fundamental modal frequencies and modal shapes. The results based on the theoretical predication and numerical simulation are then compared with those from experimental modal testing, and a good correlation is obtained. Utilizing results from the model analysis and experimental modal testing, two control algorithms, namely, positive position feedback control and strain rate feedback control, are designed. Both single-mode vibration suppression and multimode vibration suppression are studied. An experimental apparatus has been developed to implement the control algorithms. The apparatus consists of a voltage amplifier and a data acquisition and real-time control system, in addition to the composite beam with bonded piezoelectric ceramic sensors and actuators. Experiments show that the proposed controllers can achieve active vibration damping of the composite beam.
    publisherAmerican Society of Civil Engineers
    titleActive Vibration Damping of Composite Beam using Smart Sensors and Actuators
    typeJournal Paper
    journal volume15
    journal issue3
    journal titleJournal of Aerospace Engineering
    identifier doi10.1061/(ASCE)0893-1321(2002)15:3(97)
    treeJournal of Aerospace Engineering:;2002:;Volume ( 015 ):;issue: 003
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
    yabeshDSpacePersian