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Auxiliary control of LSSSeven classes of large space structures were identified and idealized into simple geometric shapes which could be easily modelled. Scaling laws were generated which allowed the seven ideal structures to be continuously scaled as to size and mass properties over their respective size ranges. Relevant sources of disturbances were determined and their effects on LSS were compared. These disturbances were applied over the range of scaling parameters to generate control force and torque requirements. Important auxiliary propulsion system (APS) characteristics were identified and an APS characteristic sensitivity matrix was established.
Document ID
19800022953
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Smith, W.
(Boeing Aerospace Co. Seattle, WA, United States)
Date Acquired
August 10, 2013
Publication Date
July 1, 1980
Publication Information
Publication: NASA. Lewis Research Center Large Space Systems(Low-Thrust Propulsion Technol.
Subject Category
Spacecraft Propulsion And Power
Accession Number
80N31459
Funding Number(s)
CONTRACT_GRANT: NAS3-21952
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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