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: 24.3.420.0 (24.3.420.0)
Syntax public 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