Four-Impulsive Rendezvous Maneuvers for Spacecrafts in Circular Orbits Using Genetic Algorithms

Table 2

The Keplerian elements of the intermediate orbits for the case where 𝑟_𝑓=2.

Orbit	𝑎	𝐸	𝑤	𝑉𝑐
0	1	0	0	1
1	1.067591	0.247661	4.720904	0.967826586
2	1.553574	0.460257	5.401124	0.802294893
3	1.553574	0.460257	5.401124	0.802294893
4	2	0		0.707106781