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An approximate method for computing error coefficient matrices for lunar trajectories.Computation of transition matrices or error coefficients in midcourse guidance studies of lunar trajectories
Document ID
19640040311
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Mclean, J. D.
Date Acquired
August 2, 2013
Publication Date
January 1, 1964
Subject Category
Space Radiation
Report/Patent Number
AIAA PAPER 63-400
Report Number: AIAA PAPER 63-400
Accession Number
64A26204
Distribution Limits
Public
Copyright
Other
Keywords
MIDCOURSE GUIDANCE
LUNAR TRAJECTORY
SPACECRAFT TRAJECTORY
ERROR

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