InitialOrbitSolverSolveForAllVelocities Method (Cartesian, Cartesian, Cartesian)

Solves the initial orbit determination problem using the Gibbs method.

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 InitialOrbitSolverResults SolveForAllVelocities(
	Cartesian position1,
	Cartesian position2,
	Cartesian position3
)

Public Function SolveForAllVelocities ( 
	position1 As Cartesian,
	position2 As Cartesian,
	position3 As Cartesian
) As InitialOrbitSolverResults

public:
InitialOrbitSolverResults^ SolveForAllVelocities(
	Cartesian position1, 
	Cartesian position2, 
	Cartesian position3
)

member SolveForAllVelocities : 
        position1 : Cartesian * 
        position2 : Cartesian * 
        position3 : Cartesian -> InitialOrbitSolverResults

Parameters

position1: Type: AGI.Foundation.CoordinatesCartesian
The first position in the orbit.
position2: Type: AGI.Foundation.CoordinatesCartesian
The second position in the orbit.
position3: Type: AGI.Foundation.CoordinatesCartesian
The third position in the orbit.

Return Value

Type: InitialOrbitSolverResults
The results containing the motion of each input position.

Exceptions

Exception	Condition
ArgumentException	Thrown if any of the input positions are Zero or Undefined.

Reference

InitialOrbitSolver Class

SolveForAllVelocities Overload

AGI.Foundation.Propagators Namespace

InitialOrbitSolverAddLanguageSpecificTextSet("LST74A4AF94_0?cpp=::|nu=.");SolveForAllVelocities Method (Cartesian, Cartesian, Cartesian)

Parameters

Return Value

Reference

InitialOrbitSolverSolveForAllVelocities Method (Cartesian, Cartesian, Cartesian)