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: 24.3.420.0 (24.3.420.0)
Syntax public 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