Research Article
Autonomous Planning of Multigravity-Assist Trajectories with Deep Space Maneuvers Using a Differential Evolution Approach
Table 7
Bounds on design variables for JEO mission: MGADSM model.
| | Design variables | Lower bound | Upper bound |
| | No. of DSMs per leg | 0 | 1 | | Flight direction, | Prograde | Retrograde | | Departure date, | 20-Feb-2018 | 24-Feb-2018 | | Arrival date, | 01-Feb-2026 | 28-Feb-2026 | | Time of flight (days)/leg, | 350, 700, 800, 850 | 450, 800, 900, 950 | | Epoch of DSM, | 0.1 | 0.9 | | DSM (km/s), | −10 | 10 |
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