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    Robust Dynamic Sliding Mode Control of a Rotating Thin-Walled Composite Blade

    Source: Journal of Aerospace Engineering:;2011:;Volume ( 024 ):;issue: 003
    Author:
    Sungsoo Na
    ,
    Bokhee Lee
    ,
    Jeonghwan Choo
    ,
    Piergiovanni Marzocca
    DOI: 10.1061/(ASCE)AS.1943-5525.0000076
    Publisher: American Society of Civil Engineers
    Abstract: This paper presents a robust control methodology for the dynamic response control of a rotating blade exposed to external excitations and modeling uncertainty. The blade is modeled as a tapered thin-walled beam with fiber-reinforced composite material. The dynamic response characteristics of a rotating composite beam are investigated; namely, ply angle, taper ratio, and various selected rotational speeds. To extend life and improve efficiency, a robust control methodology is implemented and structural tailoring composite properties are used. To this end, considering modeling uncertainties and external disturbance conditions, a sliding mode control is proposed and its performance and robustness are compared with the conventional linear quadratic Gaussian control.
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      Robust Dynamic Sliding Mode Control of a Rotating Thin-Walled Composite Blade

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    contributor authorSungsoo Na
    contributor authorBokhee Lee
    contributor authorJeonghwan Choo
    contributor authorPiergiovanni Marzocca
    date accessioned2017-05-08T21:33:46Z
    date available2017-05-08T21:33:46Z
    date copyrightJuly 2011
    date issued2011
    identifier other%28asce%29as%2E1943-5525%2E0000076.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/56218
    description abstractThis paper presents a robust control methodology for the dynamic response control of a rotating blade exposed to external excitations and modeling uncertainty. The blade is modeled as a tapered thin-walled beam with fiber-reinforced composite material. The dynamic response characteristics of a rotating composite beam are investigated; namely, ply angle, taper ratio, and various selected rotational speeds. To extend life and improve efficiency, a robust control methodology is implemented and structural tailoring composite properties are used. To this end, considering modeling uncertainties and external disturbance conditions, a sliding mode control is proposed and its performance and robustness are compared with the conventional linear quadratic Gaussian control.
    publisherAmerican Society of Civil Engineers
    titleRobust Dynamic Sliding Mode Control of a Rotating Thin-Walled Composite Blade
    typeJournal Paper
    journal volume24
    journal issue3
    journal titleJournal of Aerospace Engineering
    identifier doi10.1061/(ASCE)AS.1943-5525.0000076
    treeJournal of Aerospace Engineering:;2011:;Volume ( 024 ):;issue: 003
    contenttypeFulltext
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