LambertOrbitSolverSolveMinimumEccentricityTransfer Method (Cartesian, Cartesian)

Solves the constrained Lambert problem given the input. The solver is constrained to return the minimum eccentricity orbit.

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

Syntax

public LambertResult SolveMinimumEccentricityTransfer(
	Cartesian initialPosition,
	Cartesian finalPosition
)

Public Function SolveMinimumEccentricityTransfer ( 
	initialPosition As Cartesian,
	finalPosition As Cartesian
) As LambertResult

public:
LambertResult^ SolveMinimumEccentricityTransfer(
	Cartesian initialPosition, 
	Cartesian finalPosition
)

member SolveMinimumEccentricityTransfer : 
        initialPosition : Cartesian * 
        finalPosition : Cartesian -> LambertResult

initialPosition: Type: AGI.Foundation.CoordinatesCartesian
The first position in the transfer orbit.
finalPosition: Type: AGI.Foundation.CoordinatesCartesian
The final position in the transfer orbit.

Remarks

This method does not include an orbital plane vector used for transfers spanning π in angle subtended.

LambertOrbitSolverAddLanguageSpecificTextSet("LSTB24584F7_0?cpp=::|nu=.");SolveMinimumEccentricityTransfer Method (Cartesian, Cartesian)