DocumentCode
618159
Title
Space trajectory design: Analysis of a real-world many-objective optimization problem
Author
Lopez Jaimes, Antonio ; Oyama, Akira ; Fujii, Kenichi
Author_Institution
Inst. of Space & Astronaut. Sci., Japan Aerosp. Exploration Agency, Sagamihara, Japan
fYear
2013
fDate
20-23 June 2013
Firstpage
2809
Lastpage
2816
Abstract
Unlike most of the scalability studies on many-objective optimization problems found in the literature, in this paper we present a scalability study adopting a real-world optimization problem. The problem employed is a trajectory design optimization problem in which the objectives where varied from three to six objectives. Likewise, we evaluate the performance of the Chebyshev preference relation, which is a recently proposed technique designed for dealing with many-objective optimization problems. In this study we find that the hardness of the trajectory optimization problem, as observed in benchmark problems, increases with the addition of objective functions. Additionally, for this problem, the proportion of nondominated solutions in a random population quickly increases with the number of objectives. We also find that the Chebyshev relation has a better scalability than the standard Pareto dominance with respect to the dimension of the objective space.
Keywords
Pareto optimisation; aerospace industry; design engineering; space vehicles; Chebyshev preference relation; Pareto dominance; low-thrust spacecraft design; many-objective optimization problem; scalability study; space trajectory design; trajectory design optimization problem; Chebyshev approximation; Engines; Optimization; Scalability; Space vehicles; Trajectory;
fLanguage
English
Publisher
ieee
Conference_Titel
Evolutionary Computation (CEC), 2013 IEEE Congress on
Conference_Location
Cancun
Print_ISBN
978-1-4799-0453-2
Electronic_ISBN
978-1-4799-0452-5
Type
conf
DOI
10.1109/CEC.2013.6557910
Filename
6557910
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