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Trajectory optimization by a direct descent process.Space vehicle trajectory optimization using computerized step by step steepest descent to minimum cost, considering cost gradient vs control
Document ID
19690039581
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Fogarty, L. E.
Howe, R. M.
Date Acquired
August 5, 2013
Publication Date
January 1, 1968
Publication Information
Publisher: PERGAMON PRESS, LTD. AND PANSTWOWE WYDAWNICTWO NAUKOWE,
Subject Category
Space Sciences
Meeting Information
Meeting: INTERNATIONAL ASTRONAUTICAL FEDERATION, INTERNATIONAL ASTRONAUTICAL CONGRESS
Location: BELGRADE
Country: YUGOSLAVIA
Start Date: September 24, 1967
End Date: September 30, 1967
Sponsors: INTERNATIONAL ASTRONAUTICAL FEDERATION
Accession Number
69A17570
Funding Number(s)
CONTRACT_GRANT: NASR-54/06/
Distribution Limits
Public
Copyright
Other

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