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Passive stability of a spinning SkylabThe results of an analytical investigation of the rotational dynamics of a spinning Skylab space station are presented. The passive stability of motion of a simplified model consisting of a rigid core body with two attached flexible appendages is investigated. The parameter plane stability technique is applied to the specific Skylab case to determine its transient response to external disturbances.
Document ID
19720012936
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Seltzer, S. M. (NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
September 2, 2013
Publication Date
February 25, 1972
Subject Category
Navigation
Report/Patent Number
NASA-TM-X-64646
Report Number: NASA-TM-X-64646
Accession Number
72N20586
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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