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BallisticPropagatorConfigureForMinimumEccentricity Method (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.

Namespace:  AGI.Foundation.Propagators
Assembly:  AGI.Foundation.Models (in AGI.Foundation.Models.dll) Version: 24.1.418.0 (24.1.418.0)
public BallisticPropagatorSolutionType ConfigureForMinimumEccentricity(
	Cartesian targetPositionFixed


Type: AGI.Foundation.CoordinatesCartesian
The target position in the CentralBody's fixed frame.

Return Value

Type: BallisticPropagatorSolutionType
An enumeration which reports whether the calculation successfully met the provided constraint, or contains an alternative solution or best guess.
See Also