OrbitalElementsTryConvertMeanAnomalyToHyperbolicAnomaly Method |
Tries to convert the mean anomaly to the hyperbolic anomaly.
Namespace:
AGI.Foundation.Coordinates
Assembly:
AGI.Foundation.Core (in AGI.Foundation.Core.dll) Version: 24.2.419.0 (24.2.419.0)
Syntax public static bool TryConvertMeanAnomalyToHyperbolicAnomaly(
double meanAnomaly,
double eccentricity,
out double hyperbolicAnomaly
)
Public Shared Function TryConvertMeanAnomalyToHyperbolicAnomaly (
meanAnomaly As Double,
eccentricity As Double,
<OutAttribute> ByRef hyperbolicAnomaly As Double
) As Boolean
public:
static bool TryConvertMeanAnomalyToHyperbolicAnomaly(
double meanAnomaly,
double eccentricity,
[OutAttribute] double% hyperbolicAnomaly
)
static member TryConvertMeanAnomalyToHyperbolicAnomaly :
meanAnomaly : float *
eccentricity : float *
hyperbolicAnomaly : float byref -> bool
Parameters
- meanAnomaly
- Type: SystemDouble
The mean anomaly to convert (radians). - eccentricity
- Type: SystemDouble
The eccentricity of the orbit. - hyperbolicAnomaly
- Type: SystemDouble
On return,
the hyperbolic anomaly.
Return Value
Type:
Boolean if
eccentricity is less than or equal to one (indicating that the orbit is not hyperbolic),
or if the iterative solution to Kepler's equation did not converge; otherwise
.
See Also