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A linear algorithm for determining relative orbital state using angle dataLinear algorithms for determining spacecraft relative orbital state using angle data with digital computer
Document ID
19710030891
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Schneider, A. M.
Date Acquired
August 6, 2013
Publication Date
November 1, 1970
Subject Category
Space Sciences
Accession Number
71A11588
Funding Number(s)
CONTRACT_GRANT: NGR-05-009-106
Distribution Limits
Public
Copyright
Other

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