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Optimal guidance from hyperbolic to circular orbits.Minimum fuel guidance from hyperbolic into specified circular orbit
Document ID
19690057674
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Edelbaum, T. N.
Date Acquired
August 5, 2013
Publication Date
January 1, 1969
Publication Information
Publisher: PERGAMON PRESS, LTD.,
Subject Category
Navigation
Meeting Information
Meeting: ADVANCED PROBLEMS AND METHODS FOR SPACE FLIGHT OPTIMIZATION
Location: LIEGE
Country: BELGIUM
Start Date: June 19, 1967
End Date: June 22, 1967
Accession Number
69A35663
Funding Number(s)
CONTRACT_GRANT: NAS12-114
Distribution Limits
Public
Copyright
Other

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