Research Article
Optimal Trajectory Determination and Mission Design for Asteroid/Deep-Space Exploration via Multibody Gravity Assist Maneuvers
Table 12
Single planet flyby results from Earth to Hidalgo.
| Result | Value |
| from Earth | [−8.211 6.459 1.539] km/s | to | [−12.131 1.683 0.059] km/s | from | [−10.010 2.206 −6.700] km/s | to Target | [0.211 0.105 0.522] km/s |
| Total flyby at | [2.121 0.523 −6.759] km/s | Total flyby | 7.103 km/s | Magnitude at _1 | Maneuver at | 0.001 km/s | Gravity assist benefit | 7.101 km/s |
| Maneuver at Earth | 7.469 km/s | Maneuver at target | 0.573 km/s | Total | 8.043 km/s | Total of orbiter | 0.574 km/s |
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