International Journal of Aerospace Engineering / 2017 / Article / Tab 4

Research Article

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

Table 4

Simulation results using different initial guesses in the LEO-GEO case.

Before optimizationAfter optimizationOptimization time

OFS method0.5880 DU/TU113.4903 TU0.5803 DU/TU113.5714 TU44.846 s
TFS method0.5900 DU/TU111.1915 TU0.5812 DU/TU111.4286 TU37.880 s
Hohmann0.4974 DU/TU