BallisticPropagatorConfigureForMinimumEccentricity Method |
Overload List| Name | Description | |
|---|---|---|
 | ConfigureForMinimumEccentricity(Cartesian) |
Populates the InitialVelocity and FinalTime values for the trajectory with the minimum orbital
eccentricity. With an initial and final point on the surface of the
central body this will correspond to a trajectory that skims the surface of the body. This trajectory is mainly used
to determine the absolute lower bounds for a reasonable flight duration for a specific initial and final point.
|
| ConfigureForMinimumEccentricity(Cartographic) |
Populates the InitialVelocity and FinalTime values for the trajectory with the minimum orbital
eccentricity. With an initial and final point on the surface of the
central body this will correspond to a trajectory that skims the surface of the body. This trajectory is mainly used
to determine the absolute lower bounds for a reasonable flight duration for a specific initial and final point.
|
See Also