Mathematical Problems in Engineering / 2015 / Article / Tab 3 / Research Article
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 × 104 FEs = 5 × 104 FEs = 105 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)