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APPLICATION OF AN ''ITERATIVE GUIDANCE MODE'' TO A LUNAR LANDINGOptimization of space-vehicle trajectories by use of iterative guidance mode that minimizes midflight recalculation time for new optimum trajectories
Document ID
19630023430
Acquisition Source
Legacy CDMS
Document Type
Preprint (Draft being sent to journal)
Authors
Horn, H. J.
Date Acquired
August 1, 2013
Publication Date
May 24, 1963
Subject Category
Space Radiation
Report/Patent Number
DGRR PAPER 1504 /63/
Report Number: DGRR PAPER 1504 /63/
Accession Number
63A19489
Distribution Limits
Public
Copyright
Other
Keywords
SPACECRAFT GUIDANCE
TRAJECTORY
SPACECRAFT TRAJECTORY

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