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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: 19.1.398.0 (19.1.398.0)
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 if the eccentricity is greater than or equal to one (indicating that the orbit is not closed), or if it is negative.
See Also