Research Article
Autonomous Planning of Multigravity-Assist Trajectories with Deep Space Maneuvers Using a Differential Evolution Approach
Table 10
Zero-DSM model trajectory of Cassini 2 mission using HGDE.
| | Mission parameter | Zero-DSM Model |
| | Departure date | 16-Nov-1997 13:55:12 | | Departure impulse (km/s) | 4.5594 | | Venus swing-by date | 03-Apr-1998 21:55:12 | | Pericenter altitude (km) | 605.19 | | Jupiter swing-by date | 25-Aug-2000 21:55:12 | | Postswing-by impulse (km/s) | | | Pericenter altitude (km) | 1285964 | | Arrival date | 01-Jan-2007 23:45:36 | | Arrival impulse (km/s) | 3.4 | | Time of flight (days) | 138.3, 875, 2320.1 | | Mission duration (days) | 3333.4 |
| | Mission cost (km/s) | 12.315 |
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