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Coordinate system influence on the regularized trajectory optimization problem.Numerical integration for continuously thrusting spacecraft optimal trajectory, considering rectangular Cartesian and polar cylindrical coordinates characteristics
Document ID
19690060557
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Lewallen, J. M.
Schwausch, O. A.
Tapley, B. D.
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 69-903
Report Number: AIAA PAPER 69-903
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
69A38546
Distribution Limits
Public
Copyright
Other

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