Dynamics Modeling and Simulation of Deployable Mechanism with Double Clearance

Space deployable mechanisms have been widely employed in aeronautic industry, and the dynamic performance of the space deployable mechanisms become increasingly important. In this paper, the model of space deployable mechanism with double clearances is established by the multi-body program ADAMS. Th...

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Bibliographic Details
Published inKey Engineering Materials Vol. 693; pp. 306 - 313
Main Authors Yan, Shao Ze, Yang, Yun Qiang, Li, Jun Lan, Huang, Hong Zhou
Format Journal Article
LanguageEnglish
Published Zurich Trans Tech Publications Ltd 01.05.2016
Subjects
Aeronautics
Clearances
Computer simulation
Deployable structures
Dynamic tests
Dynamics
Spacecraft
Vibration
Deployable Mechanism
Double Clearance
Dynamic Performance
Contact Force
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Summary:Space deployable mechanisms have been widely employed in aeronautic industry, and the dynamic performance of the space deployable mechanisms become increasingly important. In this paper, the model of space deployable mechanism with double clearances is established by the multi-body program ADAMS. The deployable mechanism with ideal joint, single clearance joint and double clearance joints are simulated to investigate the effects of double clearance on the dynamic performance of the deployable mechanism. The results reveal that the coupler of double joint clearance has significant influence on dynamic performance of deployable mechanism. The results of simulation could help to predict the joint vibration in space deployable mechanisms.
Bibliography:Special topic volume with invited peer reviewed papers only
ObjectType-Article-1
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ISBN:3038357138
9783038357131
ISSN:1013-9826
1662-9795
1662-9795
DOI:10.4028/www.scientific.net/KEM.693.306