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Powered flight trajectory optimization for lunar and interplanetary transfer.Steepest descent method of trajectory optimization for computing lunar and interplanetary transfer missions, noting terminal constraints
Document ID
19660058101
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Chuck, W.
Rosenbaum, R.
Willwerth, R. E.
Date Acquired
August 3, 2013
Publication Date
April 1, 1966
Publication Information
Publication: ASTRONAUTICA ACTA
Subject Category
Space Sciences
Accession Number
66A37391
Funding Number(s)
CONTRACT_GRANT: NAS1-2678
Distribution Limits
Public
Copyright
Other
Keywords
LUNAR EXPLORATION
TRAJECTORY OPTIMIZATION
INTERPLANETARY TRANSFER
STEEPEST DESCENT METHOD

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