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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: 24.1.418.0 (24.1.418.0)
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 when eccentricity is less than or equal to one (indicating that the orbit is not hyperbolic), or if it is negative.
See Also