OrbitalElementsTryConvertTimeFromPeriapsisToTrueAnomaly Method  | 
 
            Tries to convert the time from periapsis passage to true anomaly. 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 TryConvertTimeFromPeriapsisToTrueAnomaly(
	double timeFromPeriapsis,
	double radiusOfPeriapsis,
	double eccentricity,
	double gravitationalParameter,
	out double trueAnomaly
)
Public Shared Function TryConvertTimeFromPeriapsisToTrueAnomaly ( 
	timeFromPeriapsis As Double,
	radiusOfPeriapsis As Double,
	eccentricity As Double,
	gravitationalParameter As Double,
	<OutAttribute> ByRef trueAnomaly As Double
) As Boolean
public:
static bool TryConvertTimeFromPeriapsisToTrueAnomaly(
	double timeFromPeriapsis, 
	double radiusOfPeriapsis, 
	double eccentricity, 
	double gravitationalParameter, 
	[OutAttribute] double% trueAnomaly
)
static member TryConvertTimeFromPeriapsisToTrueAnomaly : 
        timeFromPeriapsis : float * 
        radiusOfPeriapsis : float * 
        eccentricity : float * 
        gravitationalParameter : float * 
        trueAnomaly : float byref -> bool 
Parameters
- timeFromPeriapsis
 - Type: SystemDouble
The time from periapsis passage (time). - radiusOfPeriapsis
 - Type: SystemDouble
The radius of periapsis (distance). - eccentricity
 - Type: SystemDouble
The eccentricity of the orbit. - gravitationalParameter
 - Type: SystemDouble
The gravitational parameter (distance cubed per time squared). - trueAnomaly
 - Type: SystemDouble
            
            On return,
            the true anomaly.
             
Return Value
Type: 
Boolean if 
eccentricity is negative
            or 
radiusOfPeriapsis or 
gravitationalParameter is negative or zero
            or the iterative solution to Kepler's equation did not converge for elliptic or hyperbolic orbits; otherwise 
.
            
See Also