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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
19670064175
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Merrick, V. K.
Tinling, B. E.
Watson, D. M.
Date Acquired
August 3, 2013
Publication Date
November 1, 1967
Publication Information
Publication: /AIAA/JACC GUIDANCE AND CONTROL CONFERENCE
Subject Category
Space Vehicles
Accession Number
67A42904
Distribution Limits
Public
Copyright
Other
Keywords
PRESSURE EFFECT
SATELLITE ATTITUDE CONTROL
DAMPER
GRAVITY GRADIENT SATELLITE
SOLAR RADIATION

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