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

Table 3

Convergence times for various simulation types for trajectories to Hylonome.

Hylonome	Direct	Single	Double	Triple
Minimum	0:42:00	2:26:00	9:08:00	3:14:00
Maximum	1:35:00	6:06:00	50:18:00	28:12:00
Average	1:07:23	3:43:44	26:41:20	8:21:13
Median	1:08:00	3:41:00	20:38:00	6:33:00
Standard deviation	0:13:45	0:58:46	21:14:27	7:35:12
Total runs	19	12	4	10