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Optimum guidance for a low thrust interplanetary vehicle.Optimum guidance in two dimensions of constant acceleration low-thrust vehicle spiraling away from and in toward planet
Document ID
19660030736
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Breakwell, J. V.
Rauch, H. E.
Date Acquired
August 3, 2013
Publication Date
January 1, 1965
Subject Category
Navigation
Accession Number
66A10026
Funding Number(s)
CONTRACT_GRANT: NAS1-3777
Distribution Limits
Public
Copyright
Other
Keywords
OPTIMAL CONTROL
FEEDBACK CONTROL SYSTEM
INTERPLANETARY SPACECRAFT
LOW THRUST PROPULSION
TRAJECTORY OPTIMIZATION

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