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OrbitalElementsConvertHyperbolicAnomalyToMeanAnomaly Method

Converts the hyperbolic 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 ConvertHyperbolicAnomalyToMeanAnomaly(
	double hyperbolicAnomaly,
	double eccentricity
)

Parameters

hyperbolicAnomaly
Type: SystemDouble
The hyperbolic 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 less than or equal to one (indicating that the orbit is not hyperbolic), or if it is negative.
See Also