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OrbitalElements.TryConvertMeanAnomalyToEccentricAnomaly 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: 25.1.421.0 (25.1.421.0)
Syntax
public static bool TryConvertMeanAnomalyToEccentricAnomaly(
	double meanAnomaly,
	double eccentricity,
	out double eccentricAnomaly
)

Parameters

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

Return Value

Type: Boolean
false if 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 true.
See Also