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OrbitalElementsTryConvertMeanAnomalyToTrueAnomaly Method

Tries to convert the mean anomaly to the true 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 TryConvertMeanAnomalyToTrueAnomaly(
	double meanAnomaly,
	double eccentricity,
	out double trueAnomaly
)

Parameters

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

Return Value

Type: Boolean
if the eccentricity is negative or the iterative solution to Kepler's equation did not converge for elliptic or hyperbolic orbits, otherwise .
See Also