Click or drag to resize

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: 20.2.404.0 (20.2.404.0)
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 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