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International Journal of Aerospace Engineering
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International Journal of Aerospace Engineering
/
2018
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Article
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Tab 11
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Research Article
Enhanced Hybrid Differential Evolution for Earth-Moon Low-Energy Transfer Trajectory Optimization
Table 11
Results obtained by the multiple-problem Wilcoxon test for DEMR and other six algorithms on CEC2005.
VS
R
+
R
ā
value
CMA-ES
274
26
0.000375
LBBO
238.5
86.5
0.039554
GL-25
261
64
0.007727
SaDE
183
117
0.338495
=
=
MPEDE
216
84
0.057433
=
SHADE
183
117
0.338495
=
=