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Branched trajectory optimization by the projected gradient technique.Branched trajectory optimization for split rocket vehicles using projected gradient or steepest descent method
Document ID
19690061357
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Gera, J.
Date Acquired
August 5, 2013
Publication Date
August 1, 1969
Publication Information
Publisher: AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS,
Subject Category
Space Sciences
Report/Patent Number
AIAA PAPER 69-917
Report Number: AIAA PAPER 69-917
Meeting Information
Meeting: ASTRODYNAMICS CONFERENCE
Location: PRINCETON, NJ
Start Date: August 20, 1969
End Date: August 22, 1969
Sponsors: AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS AND AMERICAN ASTRONAUTICAL SOCIETY
Accession Number
69A39346
Distribution Limits
Public
Copyright
Other

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