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OrbitalElementsConvertEccentricAnomalyToMeanAnomaly Method

Tries to convert the eccentric anomaly to the mean anomaly.

Namespace:  AGI.Foundation.Coordinates
Assembly:  AGI.Foundation.Core (in AGI.Foundation.Core.dll) Version: 20.2.404.0 (20.2.404.0)
Syntax
public static double ConvertEccentricAnomalyToMeanAnomaly(
	double eccentricAnomaly,
	double eccentricity
)

Parameters

eccentricAnomaly
Type: SystemDouble
The eccentric anomaly to convert (radians).
eccentricity
Type: SystemDouble
The eccentricity of the orbit.

Return Value

Type: Double
The mean anomaly.
Exceptions
ExceptionCondition
ArgumentOutOfRangeExceptionThrown when eccentricity is greater than or equal to one (indicating that the orbit is not closed), or if it is negative.
See Also