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Flight performance of Skylab attitude and pointing control systemThe Skylab attitude and pointing control system (APCS) requirements are briefly reviewed and the way in which they became altered during the prelaunch phase of development is noted. The actual flight mission (including mission alterations during flight) is described. The serious hardware failures that occurred, beginning during ascent through the atmosphere, also are described. The APCS's ability to overcome these failures and meet mission changes are presented. The large around-the-clock support effort on the ground is discussed. Salient design points and software flexibility that should afford pertinent experience for future spacecraft attitude and pointing control system designs are included.
Document ID
19750016749
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Chubb, W. B.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Kennel, H. F.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Rupp, C. C.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Seltzer, S. M.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
September 3, 2013
Publication Date
June 1, 1975
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
M-136
NASA-TN-D-8003
Report Number: M-136
Report Number: NASA-TN-D-8003
Accession Number
75N24821
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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