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An optimal terminal guidance method for continuous powered space vehicles.Error correcting problem in space trajectory of continuous powered space vehicle, discussing optimal terminal guidance
Document ID
19650051198
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Fowler, W. T.
Tapley, B. D.
Date Acquired
August 2, 2013
Publication Date
September 1, 1965
Subject Category
Navigation
Report/Patent Number
AIAA PAPER 65-696
Report Number: AIAA PAPER 65-696
Accession Number
65A33902
Funding Number(s)
CONTRACT_GRANT: NSG-551
Distribution Limits
Public
Copyright
Other
Keywords
OPTIMAL CONTROL
SPACE TRAJECTORY PROGRAM
ERROR CORRECTING DEVICE
TERMINAL GUIDANCE

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