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OrbitalElementsConvertMeanAnomalyToHyperbolicAnomaly Method

Tries to convert the mean anomaly to the hyperbolic 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 ConvertMeanAnomalyToHyperbolicAnomaly(
	double meanAnomaly,
	double eccentricity
)

Parameters

meanAnomaly
Type: SystemDouble
The true anomaly to convert (radians).
eccentricity
Type: SystemDouble
The eccentricity of the orbit.

Return Value

Type: Double
The hyperbolic 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.
ArithmeticExceptionThrown if the iterative solution to Kepler's equation did not converge.
See Also