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