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    Dynamic Response Control of Rotating Thin-Walled Composite Blade Exposed to External Excitations

    Source: Journal of Aerospace Engineering:;2014:;Volume ( 027 ):;issue: 005
    Author:
    Seok-Ju Cha
    ,
    Ji-Seok Song
    ,
    Hwan-Hee Lee
    ,
    Sungsoo Na
    ,
    Jae-Hong Shim
    ,
    Piergiovanni Marzocca
    DOI: 10.1061/(ASCE)AS.1943-5525.0000335
    Publisher: American Society of Civil Engineers
    Abstract: A study of the dynamic control of a rotating blade subjected to external excitations is presented. A tapered thin-walled beam of closed cross-section contour with fiber-reinforced composite material is used for present study. Since a rotating blade may be exposed to a severe environment such as high angular velocity, large external load, and so on, robust control methodology is implemented to extend the blade’s life and improve its efficiency. To verify the performance of the state estimator, a sliding mode observer is introduced, and an associated robustness test is conducted in case of model uncertainty. A robust control methodology using sliding mode control in conjunction with a sliding mode observer is implemented, and its performance toward reducing the flapping dynamic responses of a rotating blade under initial conditions and various external loadings such blast load and distributed load is demonstrated. Moreover, its control performance is compared with that of the conventional linear quadratic Gaussian implementation.
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      Dynamic Response Control of Rotating Thin-Walled Composite Blade Exposed to External Excitations

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    http://yetl.yabesh.ir/yetl1/handle/yetl/71729
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    • Journal of Aerospace Engineering

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    contributor authorSeok-Ju Cha
    contributor authorJi-Seok Song
    contributor authorHwan-Hee Lee
    contributor authorSungsoo Na
    contributor authorJae-Hong Shim
    contributor authorPiergiovanni Marzocca
    date accessioned2017-05-08T22:07:12Z
    date available2017-05-08T22:07:12Z
    date copyrightSeptember 2014
    date issued2014
    identifier other29607260.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/71729
    description abstractA study of the dynamic control of a rotating blade subjected to external excitations is presented. A tapered thin-walled beam of closed cross-section contour with fiber-reinforced composite material is used for present study. Since a rotating blade may be exposed to a severe environment such as high angular velocity, large external load, and so on, robust control methodology is implemented to extend the blade’s life and improve its efficiency. To verify the performance of the state estimator, a sliding mode observer is introduced, and an associated robustness test is conducted in case of model uncertainty. A robust control methodology using sliding mode control in conjunction with a sliding mode observer is implemented, and its performance toward reducing the flapping dynamic responses of a rotating blade under initial conditions and various external loadings such blast load and distributed load is demonstrated. Moreover, its control performance is compared with that of the conventional linear quadratic Gaussian implementation.
    publisherAmerican Society of Civil Engineers
    titleDynamic Response Control of Rotating Thin-Walled Composite Blade Exposed to External Excitations
    typeJournal Paper
    journal volume27
    journal issue5
    journal titleJournal of Aerospace Engineering
    identifier doi10.1061/(ASCE)AS.1943-5525.0000335
    treeJournal of Aerospace Engineering:;2014:;Volume ( 027 ):;issue: 005
    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