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: 24.3.420.0 (24.3.420.0)
Syntax public 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