ModifiedKeplerianElementsComputeParabolicAnomaly Method

Computes the parabolic anomaly based on the current Keplerian position.

Namespace: AGI.Foundation.Coordinates
Assembly: AGI.Foundation.Core (in AGI.Foundation.Core.dll) Version: 24.2.419.0 (24.2.419.0)

Syntax

C++

Copy

public double ComputeParabolicAnomaly()

Public Function ComputeParabolicAnomaly As Double

public:
double ComputeParabolicAnomaly()

member ComputeParabolicAnomaly : unit -> float

Return Value

Type: Double
The current parabolic anomaly (radians).

Exceptions

Exception	Condition
InvalidOperationException	Thrown if the orbit type is not parabolic.

Remarks

The parabolic anomaly is an angular measure defined to be zero at periapsis, unity at the latus rectum point, and goes to infinity as true anomaly approaches Pi.

Reference

ModifiedKeplerianElements Class

AGI.Foundation.Coordinates Namespace

ModifiedKeplerianElementsAddLanguageSpecificTextSet("LST8F296226_0?cpp=::|nu=.");ComputeParabolicAnomaly Method

Return Value

Reference

ModifiedKeplerianElementsComputeParabolicAnomaly Method