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Basic response relations for space vehicle attitude control using gyros.Use of single-axis gyros for attitude control of space vehicles
Document ID
19650036351
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Cannon, R. H., Jr.
Date Acquired
August 2, 2013
Publication Date
January 1, 1965
Subject Category
Space Vehicles
Accession Number
65A19055
Distribution Limits
Public
Copyright
Other
Keywords
SATELLITE ATTITUDE CONTROL
GYRO-STABILIZED
MOMENTUM TRANSFER
ATTITUDE CONTROL

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