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Torque equilibrium attitude control for Skylab reentryAll the available torque equilibrium attitudes (most were useless from the standpoint of lack of electrical power) and the equilibrium seeking method are presented, as well as the actual successful application during the 3 weeks prior to Skylab reentry.
Document ID
19800005912
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Glaese, J. R. (NASA Marshall Space Flight Center Huntsville, AL, United States)
Kennel, H. F. (NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
September 4, 2013
Publication Date
November 1, 1979
Subject Category
Launch Vehicles And Space Vehicles
Report/Patent Number
NASA-TM-78252
Report Number: NASA-TM-78252
Accession Number
80N14169
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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