LambertOrbitSolverSolveMinimumEnergyTransfer Method (Cartesian, Cartesian, Cartesian)

Solves the constrained Lambert problem given the input. The solver is constrained to return the minimum energy solution.

Namespace: AGI.Foundation.Propagators
Assembly: AGI.Foundation.Models (in AGI.Foundation.Models.dll) Version: 24.2.419.0 (24.2.419.0)

Syntax

C++

Copy

public LambertResult SolveMinimumEnergyTransfer(
	Cartesian initialPosition,
	Cartesian finalPosition,
	Cartesian orbitalPlaneVector
)

Public Function SolveMinimumEnergyTransfer ( 
	initialPosition As Cartesian,
	finalPosition As Cartesian,
	orbitalPlaneVector As Cartesian
) As LambertResult

public:
LambertResult^ SolveMinimumEnergyTransfer(
	Cartesian initialPosition, 
	Cartesian finalPosition, 
	Cartesian orbitalPlaneVector
)

member SolveMinimumEnergyTransfer : 
        initialPosition : Cartesian * 
        finalPosition : Cartesian * 
        orbitalPlaneVector : Cartesian -> LambertResult

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.
orbitalPlaneVector: Type: AGI.Foundation.CoordinatesCartesian
A vector that is used in conjunction with the initial position of the spacecraft to define the orbital plane in the case of ambiguity. Typically, the velocity at the initial position if known.

Return Value

Type: LambertResult

Reference

LambertOrbitSolver Class

SolveMinimumEnergyTransfer Overload

AGI.Foundation.Propagators Namespace

LambertOrbitSolverAddLanguageSpecificTextSet("LST9B2D2369_0?cpp=::|nu=.");SolveMinimumEnergyTransfer Method (Cartesian, Cartesian, Cartesian)

Parameters

Return Value

Reference

LambertOrbitSolverSolveMinimumEnergyTransfer Method (Cartesian, Cartesian, Cartesian)