Spacecraft Multiple-Impulse Trajectory Optimization Using Differential Evolution Algorithm with Combined Mutation Strategies and Boundary-Handling Schemes

Table 3

Results of same-circle rendezvous model.

Algorithms	Mean (Std)
	FEs = 3 × 10^4	FEs = 5 × 10^4	FEs = 10^5
PSASM	1428.23 (147.17)	1392.07 (134.85)	1375.98 (114.27)
DE_CMS + “whole_rand”	1264.43 (11.59)	1260.73 (7.58)	1256.27 (0)
DE_CMS + “current_rand”	1266.56 (50.38)	1259.49 (6.96)	1262.74 (34.83)
DE_CMS + “reflect_rand”	1259.75 (6.78)	1258.53 (5.28)	1256.27 (0)
DE_CMS + “cut_off”	1269.94 (48.65)	1262.35 (33.58)	1262.74 (34.83)
“DE/rand/1” + DE_CBHS	1283.48 (68.35)	1276.48 (66.27)	1275.67 (58.21)
“DE/rand/2” + DE_CBHS	1278.72 (62.06)	1275.72 (58.48)	1269.20 (48.40)
“DE/current-to-rand/1” + DE_CBHS	1269.58 (47.57)	1268.47 (49.41)	1269.20 (48.40)
“DE/current-to-best/1” + DE_CBHS	1261.45 (8.69)	1258.13 (4.15)	1256.27 (0)
DE_CMSBHS	1257.99 (2.89)	1256.63 (1.16)	1256.27 (0)