Enhanced Hybrid Differential Evolution for Earth-Moon Low-Energy Transfer Trajectory Optimization

Table 12

Results obtained by the Friedman test for contraction criteria combinations on CEC2005.

Friedman
		1	1.5	2	2.5	3
	1	10.34	11.08	10.12	13.28	12.32
	1.5	11.14	11.74	13.98	12.24	13.90
	2	15.04	14.66	13.08	15.46	16.84
	2.5	11.14	12.78	14.10	14.48	14.66
	3	9.12	12.34	13.90	14.94	13.32