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Sequential estimation of the state and the observation-error convariance matrixAlgorithm for simultaneous estimate of spacecraft state and covariance matrix with observation error vector
Document ID
19710039185
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Born, G. H.
Tapley, B. D.
Date Acquired
August 6, 2013
Publication Date
February 1, 1971
Subject Category
Mathematics
Accession Number
71A19882
Funding Number(s)
CONTRACT_GRANT: NGR-44-012-008
CONTRACT_GRANT: NAS9-6963
Distribution Limits
Public
Copyright
Other

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