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