Research Article
Autonomous Planning of Multigravity-Assist Trajectories with Deep Space Maneuvers Using a Differential Evolution Approach
Table 5
Both the zero-DSM and MGADSM solutions for the Earth-Mars mission.
| Mission parameter | Zero-DSM model | MGADSM model |
| Departure date, | 05-Jun-2004 15:50:23 | 01-Jun-2004 00:00:00 | Departure impulse (km/s) | 4.612 | 4.1985 | DSM date | — | 20-Jul-2004 16:56:38 | DSM impulse (km/s) | — | 0.43784 | Venus swing-by date | 20-Nov-2004 11:02:26 | 19-Nov-2004 09:36:00 | Pericenter altitude (km) | 8050 | 7962.5 | Arrival date | 13-May-2005 16:19:11 | 16-May-2005 21:07:12 | Arrival impulse (km/s) | 6.1667 | 6.0906 | Mission duration (days) | 342.02 | 349.88 |
| Mission cost (km/s) | 10.78 | 10.73 |
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