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    On the Geometric Stiffness Matrices in Flexible Multibody Dynamics

    Source: Journal of Vibration and Acoustics:;1995:;volume( 117 ):;issue: 004::page 452
    Author:
    S. S. K. Tadikonda
    ,
    H. T. Chang
    DOI: 10.1115/1.2874478
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A 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.
    keyword(s): Stiffness , Multibody dynamics , Force , Motion , Chain , Flexible body dynamics , Bifurcation , Manipulators , Simulation results AND Multibody systems ,
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      On the Geometric Stiffness Matrices in Flexible Multibody Dynamics

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    http://yetl.yabesh.ir/yetl1/handle/yetl/116200
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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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    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
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