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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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