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Continuous attitude determination for a spin- stabilized satellite.Computer program for continuous attitude determination for spin stabilized OGO-C satellite after malfunction of attitude control system, calculating angle between high rate data periods
Document ID
19690043998
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Hardy, L. M.
Date Acquired
August 5, 2013
Publication Date
February 1, 1969
Subject Category
Space Vehicles
Accession Number
69A21987
Funding Number(s)
CONTRACT_GRANT: NAS5-9277
Distribution Limits
Public
Copyright
Other

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