Research Article
Optimization of Low-Thrust Limited-Power Trajectories in a Noncentral Gravity Field—Transfers between Orbits with Small Eccentricities
Table 1
Maneuver of modification of all orbital elements.
| | | Maneuver of modification of all orbital elements | | | Initial orbit | Final orbit | Orbital elements |
| 100 | 0.950 | 0.900 | | | | 0.850 | 0.800 | | | | 150 | 0.750 | 0.700 | 1.000 | 1.150 | | 0.650 | 0.600 | 0.0025 | 0.0050 | | 200 | 0.550 | 0.500 | | | | 0.450 | 0.400 | | | | 250 | 0.350 | 0.300 | | | | 0.250 | 0.200 | | | | — | 0.150 | 0.100 | | | |
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