Low-Thrust Trajectory Design Using Finite Fourier Series Approximation of Pseudoequinoctial Elements

Table 3

Comparison of the Earth-Mars rendezvous trajectory results with different methods.

No.	(km/s)	(m/s^2)	(N)
PE-FFS	5.7684	1.226	0.15
3D-FFS [31]	5.7294	1.5	0.15
GPOPS [31]	5.7077	—	0.15
Indirect [31]	5.67	—	0.15
Spherical [20]	5.74	—	0.22
PE [20]	5.83	—	0.16
Hodographic [22]	5.77	1.5	—