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

Table 4

Setting of the terms for the rendezvous trajectory of asteroid 1989ML.

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