OrbitalElements.ConvertTimeFromPeriapsisToHyperbolicAnomaly Method |
Converts the time from periapsis passage to hyperbolic anomaly. The value returned is signed and monotonic.
Namespace: AGI.Foundation.Coordinates
Assembly: AGI.Foundation.Core (in AGI.Foundation.Core.dll) Version: 25.1.421.0 (25.1.421.0)
Syntaxpublic static double ConvertTimeFromPeriapsisToHyperbolicAnomaly( double timeFromPeriapsis, double radiusOfPeriapsis, double eccentricity, double gravitationalParameter )
Parameters
- timeFromPeriapsis
- Type: System.Double
The time from periapsis passage (time). - radiusOfPeriapsis
- Type: System.Double
The radius of periapsis (distance). - eccentricity
- Type: System.Double
The eccentricity of the orbit. - gravitationalParameter
- Type: System.Double
The gravitational parameter (distance cubed per time squared).
Return Value
Type: DoubleThe hyperbolic anomaly (radians).
Exceptions| Exception | Condition |
|---|---|
| ArgumentOutOfRangeException | Thrown when eccentricity is less than or equal to one (indicating that the orbit is not hyperbolic), or if it is negative, or radiusOfPeriapsis or gravitationalParameter is negative or zero. |
| ArithmeticException | Thrown when the iterative solution to Kepler's equation did not converge. |
See Also