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Global, Multi-Objective Trajectory Optimization With Parametric SpreadingMission design problems are often characterized by multiple, competing trajectory optimization objectives. Recent multi-objective trajectory optimization formulations enable generation of globally-optimal, Pareto solutions via a multi-objective genetic algorithm. A byproduct of these formulations is that clustering in design space can occur in evolving the population towards the Pareto front. This clustering can be a drawback, however, if parametric evaluations of design variables are desired. This effort addresses clustering by incorporating operators that encourage a uniform spread over specified design variables while maintaining Pareto front representation. The algorithm is demonstrated on a Neptune orbiter mission, and enhanced multidimensional visualization strategies are presented.
Document ID
20170007991
Acquisition Source
Goddard Space Flight Center
Document Type
Conference Paper
Authors
Vavrina, Matthew A.
(a.i. solutions, Inc. Lanham, MD, United States)
Englander, Jacob A.
(NASA Goddard Space Flight Center Greenbelt, MD United States)
Phillips, Sean M.
(a.i. solutions, Inc. Lanham, MD, United States)
Hughes, Kyle M.
(NASA Goddard Space Flight Center Greenbelt, MD United States)
Date Acquired
August 24, 2017
Publication Date
August 22, 2017
Subject Category
Astrodynamics
Statistics And Probability
Report/Patent Number
GSFC-E-DAA-TN45282
Report Number: GSFC-E-DAA-TN45282
Meeting Information
Meeting: AAS/AIAA Astrodynamics Specialist Conference 2017
Location: Stevenson, WA
Country: United States
Start Date: August 20, 2017
End Date: August 24, 2017
Sponsors: American Inst. of Aeronautics and Astronautics, American Astronomical Society
Funding Number(s)
CONTRACT_GRANT: NNG12CR31C
CONTRACT_GRANT: nng14vc09c
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
trajectory design
low-thrust
optimization
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