OrbitalElementsTryConvertParabolicAnomalyToMeanAnomaly 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: 24.2.419.0 (24.2.419.0)
Syntax public 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: SystemDouble
The parabolic 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 not equal to one (indicating that the orbit is not parabolic); otherwise
.
See Also