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SIMULATOR STUDY OF A SATELLITE ATTITUDE CONTROL SYSTEM USING INERTIA WHEELS AND A MAGNETAutomatic attitude control system test for satellite using inertia wheels mounted on air bearings
Document ID
19630012013
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Adams, J. J. (NASA Langley Research Center Hampton, VA, United States)
Bergeron, H. P. (NASA Langley Research Center Hampton, VA, United States)
Howell, W. E. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
October 1, 1963
Subject Category
Structural Mechanics
Report/Patent Number
NASA-TN-D-1969
Report Number: NASA-TN-D-1969
Accession Number
63N21893
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
ATTITUDE CONTROL
SATELLITE CONTROL

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