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, 𝑡𝑑	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