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Space Station Common Berthing Mechanism, a multi-body simulation applicationThis paper discusses an application of multi-body dynamic analysis conducted at the Boeing Company in connection with the Space Station (SS) Common Berthing Mechanism (CBM). After introducing the hardware and analytical objectives we will focus on some of the day-to-day computational issues associated with this type of analysis.
Document ID
19940010167
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Searle, Ian (Boeing Defense and Space Group Seattle, WA, United States)
Date Acquired
September 6, 2013
Publication Date
February 15, 1993
Publication Information
Publication: JPL, Proceedings of the Fifth NASA(NSF)DOD Workshop on Aerospace Computational Control
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
94N14640
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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