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A new method for computing the state transition matrixState transition matrix computation method with efficient algorithm for orbit prediction in n-body gravitational field
Document ID
19700042381
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Weiss, E. H.
Date Acquired
August 5, 2013
Publication Date
June 1, 1969
Subject Category
Mathematics
Accession Number
70A18497
Funding Number(s)
CONTRACT_GRANT: NAS5-9762
Distribution Limits
Public
Copyright
Other

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