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International Journal of Aerospace Engineering
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International Journal of Aerospace Engineering
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2018
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Article
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Tab 8
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Research Article
Enhanced Hybrid Differential Evolution for Earth-Moon Low-Energy Transfer Trajectory Optimization
Table 8
Simple investigation of the success rates for all of the algorithms in three-dimensional space.
Algorithm
SaDE
CMA-ES
GL-25
LBBO
MPEDE
SHADE
DEMR
Success time(s)
25
19
24
16
23
25
25
Success rate
100%
76%
96%
64%
92%
100%
100%