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KeplerianElementsTrueAnomalyToMeanAnomaly Method

Note: This API is now obsolete.

Calculates the mean anomaly given the true anomaly and the eccentricity.

Namespace:  AGI.Foundation.Coordinates
Assembly:  AGI.Foundation.Core (in AGI.Foundation.Core.dll) Version: 19.1.398.0 (19.1.398.0)
Syntax
[ObsoleteAttribute("Use OrbitalElements.TryConvertTrueAnomalyToMeanAnomaly instead.")]
public static double TrueAnomalyToMeanAnomaly(
	double trueAnomaly,
	double eccentricity
)

Parameters

trueAnomaly
Type: SystemDouble
The true anomaly (radians).
eccentricity
Type: SystemDouble
The eccentricity.

Return Value

Type: Double
The mean anomaly (radians).
Exceptions
ExceptionCondition
ArgumentOutOfRangeExceptionThis method assumes a circular or elliptical orbit. So, the eccentricity must be between zero and unity.
See Also