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Stabilizing a spinning SkylabThe results are presented of a study of the dynamics of a spinning Skylab space station. The stability of motion of several simplified models with flexible appendages was investigated. A digital simulation model that more accurately portrays the complex Skylab vehicle is described, and simulation results are compared with analytically derived results.
Document ID
19720009938
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Seltzer, S. M. (NASA Marshall Space Flight Center Huntsville, AL, United States)
Patel, J. S. (Teledyne Brown Engineering Huntsville, AL, United States)
Justice, D. W. (NASA Marshall Space Flight Center Huntsville, AL, United States)
Schweitzer, G. E. (NASA Marshall Space Flight Center)
Date Acquired
September 2, 2013
Publication Date
January 3, 1972
Subject Category
Navigation
Report/Patent Number
NASA-TM-X-64635
Report Number: NASA-TM-X-64635
Accession Number
72N17588
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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