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Coordinate systems for differential correctionSystem of state transition partial derivatives for which tracking information normal matrix for lunar orbiter is nearly diagonalized
Document ID
19660027013
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Emerson, E. A.
Lemmon, W. W.
Date Acquired
August 3, 2013
Publication Date
September 1, 1966
Subject Category
Space Sciences
Report/Patent Number
NASA-CR-604
Report Number: NASA-CR-604
Accession Number
66N36303
Funding Number(s)
CONTRACT_GRANT: NAS1-4605-3
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
STATE EQUATION
LUNAR ORBITER
ORBITAL CALCULATION
TRACKING STUDY

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