Multiphase Trajectory Optimization of a Lunar Return Mission to an LEO Space Station

Table 6

Convergence analysis.

Initial estimated value	Orbit	Convergence	Agreement
Perilune+argument	1000	1000	100.0%
Perilune	1000	875	87.5%
Argument	1000	219	21.9%
None	1000	0	0.00%