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AN APPROXIMATE METHOD FOR COMPUTING ERROR COEFFICIENT MATRICES FOR LUNAR TRAJECTORIESComputation of transition matrices or error coefficients in midcourse guidance studies of lunar trajectories
Document ID
19630025658
Acquisition Source
Legacy CDMS
Document Type
Preprint (Draft being sent to journal)
Authors
Mc Lean, J. D.
Date Acquired
August 1, 2013
Publication Date
August 21, 1963
Subject Category
Space Radiation
Report/Patent Number
AIAA PAPER 63-400
Report Number: AIAA PAPER 63-400
Accession Number
63A21717
Distribution Limits
Public
Copyright
Other
Keywords
LUNAR TRAJECTORY
MIDCOURSE GUIDANCE
SPACECRAFT TRAJECTORY
ERROR

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