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    Active Control of Structures in Nonlinear Response

    Source: Journal of Aerospace Engineering:;1988:;Volume ( 001 ):;issue: 001
    Author:
    Manohar P. Kamat
    DOI: 10.1061/(ASCE)0893-1321(1988)1:1(52)
    Publisher: American Society of Civil Engineers
    Abstract: The need to account for geometric and material nonlinearities in the active control of highly flexible, large, space structures is emphasized herein. The performance index of the control problem is minimized subject to equations of state and costate using a variable metric algorithm. Unlike the conventional techniques for active control, the present algorithm is able to exploit the sparsity and symmetry of the mass and stiffness matrices of the finite element models of structures. The algorithm thus has the potential of being able to control moderately large‐scale, finite element models of highly flexible, large, space structures in a cost‐effective manner. The proposed algorithm is validated in suppressing the nonlinear vibrations of an impulsively loaded, highly flexible beam, and the need for inclusion of nonlinearities is demonstrated.
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      Active Control of Structures in Nonlinear Response

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    contributor authorManohar P. Kamat
    date accessioned2017-05-08T21:15:30Z
    date available2017-05-08T21:15:30Z
    date copyrightJanuary 1988
    date issued1988
    identifier other%28asce%290893-1321%281988%291%3A1%2852%29.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/44628
    description abstractThe need to account for geometric and material nonlinearities in the active control of highly flexible, large, space structures is emphasized herein. The performance index of the control problem is minimized subject to equations of state and costate using a variable metric algorithm. Unlike the conventional techniques for active control, the present algorithm is able to exploit the sparsity and symmetry of the mass and stiffness matrices of the finite element models of structures. The algorithm thus has the potential of being able to control moderately large‐scale, finite element models of highly flexible, large, space structures in a cost‐effective manner. The proposed algorithm is validated in suppressing the nonlinear vibrations of an impulsively loaded, highly flexible beam, and the need for inclusion of nonlinearities is demonstrated.
    publisherAmerican Society of Civil Engineers
    titleActive Control of Structures in Nonlinear Response
    typeJournal Paper
    journal volume1
    journal issue1
    journal titleJournal of Aerospace Engineering
    identifier doi10.1061/(ASCE)0893-1321(1988)1:1(52)
    treeJournal of Aerospace Engineering:;1988:;Volume ( 001 ):;issue: 001
    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