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: 25.1.421.0 (25.1.421.0)
Syntaxpublic static bool TryConvertMeanAnomalyToEccentricAnomaly(
	double meanAnomaly,
	double eccentricity,
	out double eccentricAnomaly
)
Public Shared Function TryConvertMeanAnomalyToEccentricAnomaly ( 
	meanAnomaly As Double,
	eccentricity As Double,
	<OutAttribute> ByRef eccentricAnomaly As Double
) As Boolean
public:
static bool TryConvertMeanAnomalyToEccentricAnomaly(
	double meanAnomaly, 
	double eccentricity, 
	[OutAttribute] double% eccentricAnomaly
)
static member TryConvertMeanAnomalyToEccentricAnomaly : 
        meanAnomaly : float * 
        eccentricity : float * 
        eccentricAnomaly : float byref -> bool 
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