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

Table 6

Term setting of the Tempel-1 rendezvous trajectory.

No.	1	2	3	4	5	6	7	8
	2	4	4	3	3	3	3	3
	3	3	2	2	3	4	4	3
	2	2	2	2	2	2	3	3
	5	5	6	4	4	4	4	5