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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: 20.3.405.0 (20.3.405.0)
Syntax
public LambertResult SolveMinimumEccentricityTransfer(
	Cartesian initialPosition,
	Cartesian finalPosition
)

Parameters

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

Return Value

Type: LambertResult
Remarks
This method does not include an orbital plane vector used for transfers spanning π in angle subtended.
See Also