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Passive damping augmentation of flexible beam-like lattice trusses for large space structuresA Timoshenko beam continuum model is developed to determine the transient response of a beam-like latticed large space structure, subjected to a unit impulse. It is demonstrated that an increase in diagonal stiffness, on account of the stiffness of the vertical girder, leads to a rise in the transverse shear rigidity. This results in higher natural frequencies and reduction in peak displacement. In addition, in an asymmetrical truss configuration, coupling between the extensional and shear modes raises the maximum peak displacement compared with that obtained for a symmetrical truss. The model is modified to investigate the introduction of passive damping in the form of several dynamic vibration absorbers. A unique absorber parameter optimization procedure, based on the classical steady-state criteria, is used to tune the absorbers, having a total allocated mass budget of 10%, to the first two frequencies of the latticed structure. It is found that inclusion of transverse shear rigidity as a design parameter in damping augmentation studies reduces settling time for predetermined maximum peak displacements.
Document ID
19960009726
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Cohen, K.
(Technion - Israel Inst. of Tech. Haifa, Israel)
Weller, T.
(Technion - Israel Inst. of Tech. Haifa, Israel)
Date Acquired
August 17, 2013
Publication Date
April 1, 1992
Publication Information
Publication: Proceedings of the Second International Workshop on Civilian Space Applications
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
96N16892
Distribution Limits
Public
Copyright
Other

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