OrbitalElements.TryConvertHyperbolicAnomalyToTimeFromPeriapsis Method |
Tries to convert the hyperbolic anomaly to the time of flight from the corresponding periapsis passage in seconds. The value returned is signed and monotonic even for periodic orbits.
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 TryConvertHyperbolicAnomalyToTimeFromPeriapsis( double hyperbolicAnomaly, double radiusOfPeriapsis, double eccentricity, double gravitationalParameter, out double timeFromPeriapsis )
Parameters
- hyperbolicAnomaly
- Type: System.Double
The hyperbolic 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. - timeFromPeriapsis
- Type: System.Double
On return, the time since the last periapsis passage.
Return Value
Type: Booleanfalse if eccentricity is less than or equal to one (indicating that the orbit is not hyperbolic) or radiusOfPeriapsis or gravitationalParameter is negative or zero; otherwise true.
See Also