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contributor authorS. S. K. Tadikonda
contributor authorH. T. Chang
date accessioned2017-05-08T23:48:42Z
date available2017-05-08T23:48:42Z
date copyrightOctober, 1995
date issued1995
identifier issn1048-9002
identifier otherJVACEK-28826#452_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/116200
description abstractA flexible branch body in a multibody chain undergoing large overall motions experiences geometric stiffening effects due to its own motions and interbody forces arising from bodies outboard of it. The self-motion effects are modelled through the use of 21 geometric stiffness matrices, in the literature, for an arbitrarily shaped flexible body. In this paper, the effect of interbody forces on the flexible body dynamics is modelled using up to 6 additional geometric stiffness matrices per outboard joint. Simulation results presented indicate that for a flexible body consisting of outboard bodies one may consider only the interbody force effects, without loss of accuracy, and thus significantly reduce the computational burden. This approach is especially suitable for multibody systems such as the Shuttle Remote Manipulator System, where the long boom masses are of similar magnitude, or when the payloads are several orders of magnitude larger than the link masses.
publisherThe American Society of Mechanical Engineers (ASME)
titleOn the Geometric Stiffness Matrices in Flexible Multibody Dynamics
typeJournal Paper
journal volume117
journal issue4
journal titleJournal of Vibration and Acoustics
identifier doi10.1115/1.2874478
journal fristpage452
journal lastpage461
identifier eissn1528-8927
keywordsStiffness
keywordsMultibody dynamics
keywordsForce
keywordsMotion
keywordsChain
keywordsFlexible body dynamics
keywordsBifurcation
keywordsManipulators
keywordsSimulation results AND Multibody systems
treeJournal of Vibration and Acoustics:;1995:;volume( 117 ):;issue: 004
contenttypeFulltext


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