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THE EXPLOITATION OF INERTIAL COUPLING IN PASSIVE GRAVITYGRADIENT STABILIZED SATELLITESParameters selected by analysis of passive damping techniques to facilitate optimum performance for an inertially coupled gravity gradient stabilized satellite
Document ID
19630025540
Acquisition Source
Legacy CDMS
Document Type
Preprint (Draft being sent to journal)
Authors
Merrick, V. K.
Tinling, B. E.
Date Acquired
August 1, 2013
Publication Date
August 14, 1963
Subject Category
Space Sciences
Report/Patent Number
AIAA PAPER 63-342
Report Number: AIAA PAPER 63-342
Accession Number
63A21599
Distribution Limits
Public
Copyright
Other
Keywords
INERTIAL GUIDANCE
SPACECRAFT STABILITY
GRAVITY GRADIENT SATELLITE

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