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Coordinate system influence on the regularized trajectory optimization problemNumerical integration for continuously thrusting spacecraft optimal trajectory, considering rectangular Cartesian and polar cylindrical coordinates characteristics
Document ID
19710038194
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Lewallen, J. M.
Schwausch, O. A.
Tapley, B. D.
Date Acquired
August 6, 2013
Publication Date
January 1, 1971
Subject Category
Space Sciences
Report/Patent Number
AIAA PAPER 69-903
Report Number: AIAA PAPER 69-903
Meeting Information
Meeting: ASTRODYNAMICS CONFERENCE
Location: PRINCETON, NJ
Country: US
Start Date: August 20, 1969
End Date: August 22, 1969
Sponsors: AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS, AMERICAN ASTRONAUTICAL SOCIETY
Accession Number
71A18891
Distribution Limits
Public
Copyright
Other

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