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Trajectory optimization using regularized variables.Trajectory optimization of space vehicle with continuous thrust based on regularized equations, comparing perturbation method for earth-Jupiter rendezvous transfer
Document ID
19690059184
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Lewallen, J. M.
Szebehely, V.
Tapley, B. D.
Date Acquired
August 5, 2013
Publication Date
June 1, 1969
Subject Category
Space Sciences
Report/Patent Number
AAS PAPER 68-099
Report Number: AAS PAPER 68-099
Meeting Information
Meeting: AMERICAN ASTRONAUTICAL SOCIETY AND AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS, ASTRODYNAMICS SPECIALIST CONFERENCE
Location: JACKSON, WYO.
Start Date: September 3, 1968
End Date: September 5, 1968
Sponsors: AMERICAN ASTRONAUTICAL SOCIETY AND AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS
Accession Number
69A37173
Funding Number(s)
CONTRACT_GRANT: NAS9-6963
CONTRACT_GRANT: NGR-44-012-046
Distribution Limits
Public
Copyright
Other

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