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OrbitalElementsTryConvertMeanAnomalyToHyperbolicAnomaly 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 bool TryConvertMeanAnomalyToHyperbolicAnomaly(
	double meanAnomaly,
	double eccentricity,
	out double hyperbolicAnomaly
)

Parameters

meanAnomaly
Type: SystemDouble
The mean anomaly to convert (radians).
eccentricity
Type: SystemDouble
The eccentricity of the orbit.
hyperbolicAnomaly
Type: SystemDouble
On return, the hyperbolic anomaly.

Return Value

Type: Boolean
if the eccentricity is less than or equal to one (indicating that the orbit is not hyperbolic), or if the iterative solution to Kepler's equation did not converge, otherwise .
See Also