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OrbitalElementsTryComputeTimeOfFlight Method

Tries to calculate the time of flight between two true anomalies.

Namespace:  AGI.Foundation.Coordinates
Assembly:  AGI.Foundation.Core (in AGI.Foundation.Core.dll) Version: 19.1.398.0 (19.1.398.0)
Syntax
public static bool TryComputeTimeOfFlight(
	double initialTrueAnomaly,
	double finalTrueAnomaly,
	double radiusOfPeriapsis,
	double eccentricity,
	double gravitationalParameter,
	out double timeOfFlight
)

Parameters

initialTrueAnomaly
Type: SystemDouble
The initial true anomaly (radians).
finalTrueAnomaly
Type: SystemDouble
The final true anomaly (radians).
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).
timeOfFlight
Type: SystemDouble
On return, the time of flight (time).

Return Value

Type: Boolean
if the time of flight could be calculated with the given elements, otherwise .
See Also