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Parallel Monotonic Basin Hopping for Low Thrust Trajectory OptimizationMonotonic Basin Hopping has been shown to be an effective method of solving low thrust trajectory optimization problems. This paper outlines an extension to the common serial implementation by parallelizing it over any number of available compute cores. The Parallel Monotonic Basin Hopping algorithm described herein is shown to be an effective way to more quickly locate feasible solutions, and improve locally optimal solutions in an automated way without requiring a feasible initial guess. The increased speed achieved through parallelization enables the algorithm to be applied to more complex problems that would otherwise be impractical for a serial implementation. Low thrust cislunar transfers and a hybrid Mars example case demonstrate the effectiveness of the algorithm. Finally, a preliminary scaling study quantifies the expected decrease in solve time compared to a serial implementation.
Document ID
20180004586
Acquisition Source
Glenn Research Center
Document Type
Presentation
Authors
McCarty, Steven L.
(NASA Glenn Research Center Cleveland, OH, United States)
McGuire, Melissa L.
(NASA Glenn Research Center Cleveland, OH, United States)
Date Acquired
August 21, 2018
Publication Date
January 10, 2018
Subject Category
Astrodynamics
Report/Patent Number
GRC-E-DAA-TN51148
Meeting Information
Meeting: AIAA SciTech Forum, AAS/AIAA Space Flight Mechanics Meeting
Location: Kissimmee, FL
Country: United States
Start Date: January 8, 2018
End Date: January 12, 2018
Sponsors: American Inst. of Aeronautics and Astronautics, American Astronautical Society
Funding Number(s)
WBS: WBS 837933.02.12.03
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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