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OrbitalElementsConvertMeanAnomalyToParabolicAnomaly Method

Converts the mean anomaly to the parabolic anomaly.

Namespace:  AGI.Foundation.Coordinates
Assembly:  AGI.Foundation.Core (in AGI.Foundation.Core.dll) Version: 19.1.398.0 (19.1.398.0)
Syntax
public static double ConvertMeanAnomalyToParabolicAnomaly(
	double meanAnomaly,
	double eccentricity
)

Parameters

meanAnomaly
Type: SystemDouble
The true anomaly to convert (radians).
eccentricity
Type: SystemDouble
The eccentricity of the orbit.

Return Value

Type: Double
The parabolic anomaly.
Exceptions
ExceptionCondition
ArgumentOutOfRangeExceptionThrown if the eccentricity is not equal to one (indicating that the orbit is not parabolic), or if it is negative.
See Also