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Low-thrust guidance study Final reportComputer algorithm to determine minimum-time optimal control for continuous low-thrust propulsion systems operating in inverse-square gravity field
Document ID
19660025729
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Fimple, W. R. (United Aircraft Corp. East Hartford, CT, United States)
Van Dine, C. P. (United Aircraft Corp. East Hartford, CT, United States)
Date Acquired
August 3, 2013
Publication Date
July 1, 1966
Subject Category
Navigation
Report/Patent Number
NASA-CR-77406
E-910350-11
Report Number: NASA-CR-77406
Report Number: E-910350-11
Accession Number
66N35019
Funding Number(s)
CONTRACT_GRANT: NAS8-20119
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
GRAVITATIONAL FIELD
COMPUTER METHOD
LOW THRUST PROPULSION
OPTIMAL CONTROL
GUIDANCE AND CONTROL

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