OrbitalElementsConvertMeanAnomalyToEccentricAnomaly Method |
Converts the mean anomaly to the eccentric anomaly.
Namespace:
AGI.Foundation.Coordinates
Assembly:
AGI.Foundation.Core (in AGI.Foundation.Core.dll) Version: 24.2.419.0 (24.2.419.0)
Syntax public static double ConvertMeanAnomalyToEccentricAnomaly(
double meanAnomaly,
double eccentricity
)
Public Shared Function ConvertMeanAnomalyToEccentricAnomaly (
meanAnomaly As Double,
eccentricity As Double
) As Double
public:
static double ConvertMeanAnomalyToEccentricAnomaly(
double meanAnomaly,
double eccentricity
)
static member ConvertMeanAnomalyToEccentricAnomaly :
meanAnomaly : float *
eccentricity : float -> float
Parameters
- meanAnomaly
- Type: SystemDouble
The true anomaly to convert (radians). - eccentricity
- Type: SystemDouble
The eccentricity of the orbit.
Return Value
Type:
DoubleThe eccentric anomaly.
Exceptions Exception | Condition |
---|
ArgumentOutOfRangeException | Thrown when eccentricity is greater than or equal to one (indicating that the orbit is not closed), or if it is negative. |
ArithmeticException | Thrown when the iterative solution to Kepler's equation did not converge. |
See Also