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: 24.2.419.0 (24.2.419.0)
Syntax public 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