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OrbitalElementsConvertMeanAnomalyToTrueAnomaly Method

Converts the mean anomaly to the true 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 ConvertMeanAnomalyToTrueAnomaly(
	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 true anomaly.
Exceptions
ExceptionCondition
ArgumentOutOfRangeExceptionThrown if the eccentricity is negative.
ArithmeticExceptionThrown if the iterative solution to Kepler's equation did not converge for elliptic or hyperbolic orbits.
See Also