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Docking of a rigid spacecraft with unrestrained orbiting flexible structureA methodology for producing simulations of the docking of a rigid spacecraft with any unrestrained flexible structure was studied. A detailed algorithm for the simulation of the docking of a rigid body with a nonuniform unrestrained beam was sought. The values acquired during docking by the variables characterizing the motions of the rigid body and the unrestrained beam were sought.
Document ID
19830013989
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Kane, T. R. (Stanford Univ. CA, United States)
Date Acquired
August 11, 2013
Publication Date
April 1, 1983
Publication Information
Publication: NASA. Langley Research Center Structural Dyn. and Control of Large Space Struct., 1982
Subject Category
Astronautics (General)
Accession Number
83N22260
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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IDRelationTitle19830013985Collected WorksStructural Dynamics and Control of Large Space Structures, 198219830013985Collected WorksStructural Dynamics and Control of Large Space Structures, 1982
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