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