Research Article
Low-Thrust Trajectory Design Using Finite Fourier Series Approximation of Pseudoequinoctial Elements
Table 9
Comparison of results of different methods [
29,
38].
| | Method | Maximum thrust () | Transfer cycle | Transfer time (days) | Trajectory direction | (km/s) | CPU (s) |
| | Three-stage approach [38] | 2.943 | 12 | 6.81 | Prograde | 7.05 | — | | 2D-FFS [29] | 3.237 | 12 | 6.45 | Prograde | 8.14 | 129 |
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