Multiple Gravity Assist Spacecraft Trajectories Design Based on BFS and EP_DE Algorithm

Table 7

Feature vector matrix in GTOC1.

(a)

First component	Second component	Third component	Fourth component	Fifth component	Sixth component	Seventh component	Eighth component
−0.3850	−0.2518	−0.2510	0.1105	−0.3493	0.1704	0.2427	0.7093
−0.0492	0.3120	0.3859	−0.6696	−0.3199	0.4230	−0.1061	0.1021
−0.2776	0.6459	−0.5983	−0.1580	0.2905	0.0622	0.1809	−0.0423
0.4842	0.4185	−0.1284	0.3069	−0.6616	−0.0948	0.1762	−0.0452
−0.4723	0.3972	0.5264	0.2188	−0.0206	−0.5224	0.0346	0.1403
0.3660	0.0344	−0.1872	−0.3740	0.0992	−0.5419	−0.3616	0.5057
0.3856	0.0454	0.2862	−0.0729	0.3909	0.0490	0.7312	0.2686
0.1794	0.2930	0.1400	0.4767	0.3008	0.4585	−0.4466	0.3675

(b)

First component	Second component	Third component	Fourth component	Fifth component	Sixth component	Seventh component	Eighth component
−0.1287	0.0755	−0.5779	0.4540	−0.1094	0.2181	−0.1042	−0.6060
−0.0511	−0.0347	0.1628	−0.4753	−0.6551	0.5042	0.1035	−0.2230
−0.0646	−0.1284	−0.0644	−0.1991	0.5942	0.3844	0.6374	−0.1686
0.0696	0.0040	0.0960	−0.2124	0.4270	0.4605	−0.7376	−0.0494
−0.1124	0.0311	−0.1876	−0.6225	0.1176	−0.5663	−0.1099	−0.4659
−0.0825	−0.1345	0.7530	0.3088	0.0690	−0.1201	0.0018	−0.5418
0.7923	0.5644	0.0581	−0.0158	0.0225	0.0072	0.1200	−0.1873
0.5697	−0.7994	−0.1437	0.0071	−0.0664	−0.0574	−0.0402	−0.0799