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OrbitalElementsTryConvertMeanAnomalyToEccentricAnomaly Method

Tries to convert the mean anomaly to the eccentric 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 TryConvertMeanAnomalyToEccentricAnomaly(
	double meanAnomaly,
	double eccentricity,
	out double eccentricAnomaly
)

Parameters

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

Return Value

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