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contributor authorJames M. Pitarresi
contributor authorGeorge D. Manolis
date accessioned2017-05-08T21:15:34Z
date available2017-05-08T21:15:34Z
date copyrightJuly 1989
date issued1989
identifier other%28asce%290893-1321%281989%292%3A3%28169%29.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/44663
description abstractThe shape control of structural systems using the temporal finite element method (TFEM) is addressed in this work. In particular, the standard time marching TFEM is used to predict the displacements of each degree of freedom (DOF) at the end of a given time interval. If these displacements do not exceed the limits imposed on the structure for serviceability, safety, etc., then the displacements for the next time step are computed. If, however, any of the displacements exceed their limit, a control velocity is computed and applied at the beginning of the time interval for each DOF exceeding its limit. The magnitude and direction of this velocity are such as to render the displacement at the end of the time interval equal to the limit value. An example of a two-degree-of-freedom system serves to illustrate this methodology.
publisherAmerican Society of Civil Engineers
titleStructural Control by Temporal Finite Elements
typeJournal Paper
journal volume2
journal issue3
journal titleJournal of Aerospace Engineering
identifier doi10.1061/(ASCE)0893-1321(1989)2:3(169)
treeJournal of Aerospace Engineering:;1989:;Volume ( 002 ):;issue: 003
contenttypeFulltext


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