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Mathematical modelling of a loading problem in flexible assembly systems

โœ Scribed by R.S. Lashkari; M. Duan


Publisher
Elsevier Science
Year
1994
Tongue
English
Weight
472 KB
Volume
26
Category
Article
ISSN
0360-8352

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Space structures such as the solar panels or antenna, when deployed in space, have large dimensions, low mass to size ratio, large inertias and relatively low structural rigidity. Due to space restrictions, these structures are originally in stowed configurations and are deployed into their full siz