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A split-damper inertially coupled passive gravity-gradient attitude control system.Attitude errors of inertially coupled gravity gradient satellite with solar radiation pressure as dominant disturbance, noting slot problems in stabilized package accommodating damper motion
Document ID
19660059571
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Merrick, V. K.
Tinling, B. E.
Watson, D. M.
Date Acquired
August 3, 2013
Publication Date
January 1, 1966
Subject Category
Space Vehicles
Accession Number
66A38861
Distribution Limits
Public
Copyright
Other
Keywords
SATELLITE ATTITUDE CONTROL
PRESSURE EFFECT
SOLAR RADIATION
DAMPER
GRAVITY GRADIENT SATELLITE

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