BallisticPropagatorConfigureForMinimumEccentricity Method (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.

Namespace: AGI.Foundation.Propagators
Assembly: AGI.Foundation.Models (in AGI.Foundation.Models.dll) Version: 24.3.420.0 (24.3.420.0)

Syntax

C++

Copy

public BallisticPropagatorSolutionType ConfigureForMinimumEccentricity(
	Cartographic targetPosition
)

Public Function ConfigureForMinimumEccentricity ( 
	targetPosition As Cartographic
) As BallisticPropagatorSolutionType

public:
BallisticPropagatorSolutionType ConfigureForMinimumEccentricity(
	Cartographic targetPosition
)

member ConfigureForMinimumEccentricity : 
        targetPosition : Cartographic -> BallisticPropagatorSolutionType

Parameters

targetPosition: Type: AGI.Foundation.CoordinatesCartographic
The target position, as a Cartographic 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.

Reference

BallisticPropagator Class

ConfigureForMinimumEccentricity Overload

AGI.Foundation.Propagators Namespace

BallisticPropagatorAddLanguageSpecificTextSet("LST2D0809F4_0?cpp=::|nu=.");ConfigureForMinimumEccentricity Method (Cartographic)

Parameters

Return Value

Reference

BallisticPropagatorConfigureForMinimumEccentricity Method (Cartographic)