International Journal of Aerospace Engineering / 2017 / Article / Tab 3

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 conditionsInput parameters

1.0313 DU2
0 rad5
6.61 DU5
3.1416 rad15.708 rad
0 DU/TU251
0.9565 rad/TU
0 DU/TU
0.05884 rad/TU