OrbitalElements.TryConvertTrueAnomalyToTimeUntilNextPeriapsis Method |
Tries to convert the true anomaly to the time of flight until the next periapsis passage in seconds. The value returned is positive and, for closed orbits, periodic.
Namespace: AGI.Foundation.Coordinates
Assembly: AGI.Foundation.Core (in AGI.Foundation.Core.dll) Version: 25.1.421.0 (25.1.421.0)
Syntaxpublic static bool TryConvertTrueAnomalyToTimeUntilNextPeriapsis( double trueAnomaly, double radiusOfPeriapsis, double eccentricity, double gravitationalParameter, out double timeUntilNextPeriapsis )
Parameters
- trueAnomaly
- Type: System.Double
The true anomaly (radians). - radiusOfPeriapsis
- Type: System.Double
The radius of periapsis. - eccentricity
- Type: System.Double
The eccentricity of the orbit. - gravitationalParameter
- Type: System.Double
The gravitational parameter of the central body being orbited. - timeUntilNextPeriapsis
- Type: System.Double
On return, the time until the next periapsis passage.
Return Value
Type: Booleanfalse if eccentricity is negative or radiusOfPeriapsis or gravitationalParameter is negative or zero or if the orbit is open (parabolic or hyperbolic) and trueAnomaly is positive or zero or if trueAnomaly is not within the valid range for the type of orbit; otherwise true.
See Also