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 .
| Orbit | | | | |
| 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 |
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