Optimal Trajectory Determination and Mission Design for Asteroid/Deep-Space Exploration via Multibody Gravity Assist Maneuvers

Table 4

Convergence times for various simulation types for trajectories to Hidalgo.

Hidalgo	Direct	Single	Double	Triple
Minimum	0:41:00	1:59:00	1:46:00	1:05:00
Maximum	1:34:00	15:48:00	8:33:00	9:08:00
Average	0:59:13	4:32:00	5:47:22	4:37:32
Median	0:50:00	2:42:30	6:13:30	5:30:00
Standard deviation	0:17:31	4:38:25	1:58:57	2:51:15
Total runs	19	11	10	15