OrbitalElementsTryConvertHyperbolicAnomalyToMeanAnomaly Method  | 
 
            Tries to convert the hyperbolic anomaly to the mean 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 TryConvertHyperbolicAnomalyToMeanAnomaly(
	double hyperbolicAnomaly,
	double eccentricity,
	out double meanAnomaly
)
Public Shared Function TryConvertHyperbolicAnomalyToMeanAnomaly ( 
	hyperbolicAnomaly As Double,
	eccentricity As Double,
	<OutAttribute> ByRef meanAnomaly As Double
) As Boolean
public:
static bool TryConvertHyperbolicAnomalyToMeanAnomaly(
	double hyperbolicAnomaly, 
	double eccentricity, 
	[OutAttribute] double% meanAnomaly
)
static member TryConvertHyperbolicAnomalyToMeanAnomaly : 
        hyperbolicAnomaly : float * 
        eccentricity : float * 
        meanAnomaly : float byref -> bool 
Parameters
- hyperbolicAnomaly
 - Type: SystemDouble
The hyperbolic anomaly to convert (radians). - eccentricity
 - Type: SystemDouble
The eccentricity of the orbit. - meanAnomaly
 - Type: SystemDouble
            
            On return,
            the mean anomaly.
             
Return Value
Type: 
Boolean if 
eccentricity is less than or equal to one (indicating that the orbit is not hyperbolic); otherwise 
.
See Also