Research Article
A Shape-Based Method for Continuous Low-Thrust Trajectory Design between Circular Coplanar Orbits
Table 3
Boundary conditions and input parameters for LEO-GEO transfer.
| | Boundary conditions | Input parameters |
| | 1.0313 DU | | 2 | | 0 rad | | 5 | | 6.61 DU | | 5 | | 3.1416 rad | | 15.708 rad | | 0 DU/TU | | 251 | | 0.9565 rad/TU | | | | 0 DU/TU | | | | 0.05884 rad/TU | | |
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