Research Article

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 𝑉 𝑐

01001
11.0675910.2476614.7209040.967826586
21.5535740.4602575.4011240.802294893
31.5535740.4602575.4011240.802294893
4200.707106781