International Journal of Aerospace Engineering / 2017 / Article / Tab 1

Research Article

A Shape-Based Method for Continuous Low-Thrust Trajectory Design between Circular Coplanar Orbits

Table 1

Boundary conditions and input parameters for Earth-Mars rendezvous orbit.

Boundary conditionsInput parameters

1 DU1
0 rad6
1.5234 DU6
3.548 rad13.45 TU
0 DU/TU151
1 rad/TU
0 DU/TU
0.5318 rad/TU