Research Article
Autonomous Planning of Multigravity-Assist Trajectories with Deep Space Maneuvers Using a Differential Evolution Approach
Table 12
MGADSM trajectory of Cassini 2 mission using HGDE.
| | Mission parameter | MGADSM model |
| | Departure date | 03-Nov-1997 15:39:21 | | Departure impulse (km/s) | 3.9141 | | Venus swing-by date | 30-Mar-1998 06:26:22 | | Pericenter altitude (km) | 674.8 | | DSM date | 17-Nov-1998 08:04:14 | | DSM impulse (km/s) | 0.46911 | | Venus swing-by date | 13-Jul-1999 04:43:10 | | Pericenter altitude (km) | 605.2 | | Earth swing-by date | 23-Aug-1999 20:53:59 | | Pericenter altitude (km) | 3588.16 | | Jupiter swing-by date | 06-Apr-2001 01:02:28 | | Pericenter altitude (km) | 4605630.3 | | Arrival date | 21-May-2007 16:47:46 | | Arrival impulse (km/s) | 4.2449 | | Time of flight (days) | 146.6, 469.9, 41.6, 591.1, 2236.6 | | Mission duration (days) | 3486 |
| | Mission cost (km/s) | 8.89 |
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