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

Table 7

Comparison of the comet Tempel-1 rendezvous trajectory results by different methods.

No.	(km/s)	(m/s^2)	(N)
PE-FFS	12.65	7.1	0.59
3D-FFS [31]	12.69	7.1	0.59
GPOPS [31]	11.45	—	0.59
Indirect [31]	11.45	—	0.59
Spherical [20]	11.13	—	1.4
PE [20]	13.44	—	1.13
Hodographic [22]	12.68	11.7	—