Research Article

Optimal Trajectory Determination and Mission Design for Asteroid/Deep-Space Exploration via Multibody Gravity Assist Maneuvers

Table 10

Mission to Hidalgo for multiple flyby scenarios.

ā€‰ Direct Single Double Triple

Total 13.889 8.043 11.187 29.255
Orbiter 7.055 0.574 7.485 25.580