OrbitalElements Class

Provides functions which can be used to perform calculations and conversions relating orbital elements.

Inheritance Hierarchy

SystemObject
AGI.Foundation.CoordinatesOrbitalElements

Namespace: AGI.Foundation.Coordinates
Assembly: AGI.Foundation.Core (in AGI.Foundation.Core.dll) Version: 24.3.420.0 (24.3.420.0)

Syntax

C++

Copy

public static class OrbitalElements

Public NotInheritable Class OrbitalElements

public ref class OrbitalElements abstract sealed

[<AbstractClassAttribute>]
[<SealedAttribute>]
type OrbitalElements =  class end

The OrbitalElements type exposes the following members.

Methods

	Name	Description
	ComputeEccentricity	Calculates the eccentricity of the orbit.
	ComputeMeanMotion	Calculates the mean motion of the orbit.
	ComputePeriod	Calculates the period of the orbit.
	ComputeRadiusOfApoapsis	Calculates the radius of apoapsis of the orbit.
	ComputeRadiusOfPeriapsis	Calculates the radius of periapsis of the orbit.
	ComputeSemilatusRectum	Calculates the semilatus rectum of the orbit.
	ComputeSemimajorAxis	Calculates the semimajor axis of the orbit.
	ComputeTimeOfFlight	Calculates the time of flight between two true anomalies.
	ConvertEccentricAnomalyToMeanAnomaly	Tries to convert the eccentric anomaly to the mean anomaly.
	ConvertEccentricAnomalyToTimeFromPeriapsis	Converts the eccentric anomaly to the time of flight from the corresponding periapsis passage in seconds. The value returned is signed and monotonic even for periodic orbits.
	ConvertEccentricAnomalyToTrueAnomaly	Converts the eccentric anomaly to the true anomaly.
	ConvertHyperbolicAnomalyToMeanAnomaly	Converts the hyperbolic anomaly to the mean anomaly.
	ConvertHyperbolicAnomalyToTimeFromPeriapsis	Converts 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.
	ConvertHyperbolicAnomalyToTrueAnomaly	Converts the hyperbolic anomaly to the true anomaly.
	ConvertMeanAnomalyToEccentricAnomaly	Converts the mean anomaly to the eccentric anomaly.
	ConvertMeanAnomalyToHyperbolicAnomaly	Tries to convert the mean anomaly to the hyperbolic anomaly.
	ConvertMeanAnomalyToParabolicAnomaly	Converts the mean anomaly to the parabolic anomaly.
	ConvertMeanAnomalyToTimeFromPeriapsis	Converts the mean anomaly to the time of flight from the corresponding periapsis passage in seconds. The value returned is signed and monotonic even for periodic orbits.
	ConvertMeanAnomalyToTimeSincePreviousPeriapsis	Converts the mean anomaly to the time of flight since the previous periapsis passage in seconds. The value returned is positive and, for closed orbits, periodic.
	ConvertMeanAnomalyToTimeUntilNextPeriapsis	Converts the mean anomaly to the time of flight until the next periapsis passage in seconds. The value returned is positive and, for closed orbits, periodic.
	ConvertMeanAnomalyToTrueAnomaly	Converts the mean anomaly to the true anomaly.
	ConvertParabolicAnomalyToMeanAnomaly	Converts the parabolic anomaly to the mean anomaly.
	ConvertParabolicAnomalyToTimeFromPeriapsis	Converts the parabolic anomaly to the time of flight from the corresponding periapsis passage in seconds. The value returned is signed and monotonic even for periodic orbits.
	ConvertParabolicAnomalyToTrueAnomaly	Converts the parabolic anomaly to the true anomaly.
	ConvertTimeFromPeriapsisToEccentricAnomaly	Converts the time from periapsis passage to eccentric anomaly. The value returned is signed and monotonic even for periodic orbits.
	ConvertTimeFromPeriapsisToHyperbolicAnomaly	Converts the time from periapsis passage to hyperbolic anomaly. The value returned is signed and monotonic.
	ConvertTimeFromPeriapsisToMeanAnomaly	Converts the time from periapsis passage to mean anomaly. The value returned is signed and monotonic even for periodic orbits.
	ConvertTimeFromPeriapsisToParabolicAnomaly	Converts the time from periapsis passage to parabolic anomaly. The value returned is signed and monotonic.
	ConvertTimeFromPeriapsisToTrueAnomaly	Converts the time from periapsis passage to true anomaly. The value returned is signed and monotonic even for periodic orbits.
	ConvertTrueAnomalyToEccentricAnomaly	Converts the true anomaly to the eccentric anomaly.
	ConvertTrueAnomalyToHyperbolicAnomaly	Converts the true anomaly to the hyperbolic anomaly.
	ConvertTrueAnomalyToMeanAnomaly	Converts the true anomaly to the mean anomaly.
	ConvertTrueAnomalyToParabolicAnomaly	Converts the true anomaly to the parabolic anomaly.
	ConvertTrueAnomalyToTimeFromPeriapsis	Converts the true anomaly to the time of flight from the corresponding periapsis passage in seconds. The value returned is signed and monotonic even for periodic orbits.
	ConvertTrueAnomalyToTimeSincePreviousPeriapsis	Converts the true anomaly to the time of flight since the previous periapsis passage in seconds. The value returned is positive and, for closed orbits, periodic.
	ConvertTrueAnomalyToTimeUntilNextPeriapsis	Converts the true anomaly to the time of flight until the next periapsis passage in seconds. The value returned is positive and, for closed orbits, periodic.
	PerifocalToCartesianMatrix	Calculates the transformation matrix from the perifocal axes to the inertial axes.
	TryComputeEccentricity	Tries to calculate the eccentricity of the orbit.
	TryComputeMeanMotion	Tries to calculate the mean motion of the orbit.
	TryComputePeriod	Tries to calculate the period of the orbit.
	TryComputeRadiusOfApoapsis	Tries to calculate the radius of apoapsis of the orbit.
	TryComputeRadiusOfPeriapsis	Tries to calculate the radius of periapsis of the orbit.
	TryComputeSemilatusRectum	Tries to calculate the semilatus rectum of the orbit.
	TryComputeSemimajorAxis	Tries to calculate the semimajor axis of the orbit.
	TryComputeTimeOfFlight	Tries to calculate the time of flight between two true anomalies.
	TryConvertEccentricAnomalyToMeanAnomaly	Tries to convert the eccentric anomaly to the mean anomaly.
	TryConvertEccentricAnomalyToTimeFromPeriapsis	Tries to convert the eccentric anomaly to the time of flight from the corresponding periapsis passage in seconds. The value returned is signed and monotonic even for periodic orbits.
	TryConvertEccentricAnomalyToTrueAnomaly	Tries to convert the eccentric anomaly to the true anomaly.
	TryConvertHyperbolicAnomalyToMeanAnomaly	Tries to convert the hyperbolic anomaly to the mean anomaly.
	TryConvertHyperbolicAnomalyToTimeFromPeriapsis	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.
	TryConvertHyperbolicAnomalyToTrueAnomaly	Tries to convert the hyperbolic anomaly to the true anomaly.
	TryConvertMeanAnomalyToEccentricAnomaly	Tries to convert the mean anomaly to the eccentric anomaly.
	TryConvertMeanAnomalyToHyperbolicAnomaly	Tries to convert the mean anomaly to the hyperbolic anomaly.
	TryConvertMeanAnomalyToParabolicAnomaly	Tries to convert the mean anomaly to the parabolic anomaly.
	TryConvertMeanAnomalyToTimeFromPeriapsis	Tries to convert the mean anomaly to the time of flight from the corresponding periapsis passage in seconds. The value returned is signed and monotonic even for periodic orbits.
	TryConvertMeanAnomalyToTimeSincePreviousPeriapsis	Tries to convert the mean anomaly to the time of flight since the previous periapsis passage in seconds. The value returned is positive and, for closed orbits, periodic.
	TryConvertMeanAnomalyToTimeUntilNextPeriapsis	Tries to convert the mean anomaly to the time of flight until the next periapsis passage in seconds. The value returned is positive and, for closed orbits, periodic.
	TryConvertMeanAnomalyToTrueAnomaly	Tries to convert the mean anomaly to the true anomaly.
	TryConvertParabolicAnomalyToMeanAnomaly	Tries to convert the parabolic anomaly to the mean anomaly.
	TryConvertParabolicAnomalyToTimeFromPeriapsis	Tries to convert the parabolic anomaly to the time of flight from the corresponding periapsis passage in seconds. The value returned is signed and monotonic even for periodic orbits.
	TryConvertParabolicAnomalyToTrueAnomaly	Tries to convert the parabolic anomaly to the true anomaly.
	TryConvertTimeFromPeriapsisToEccentricAnomaly	Tries to convert the time from periapsis passage to eccentric anomaly. The value returned is signed and monotonic even for periodic orbits.
	TryConvertTimeFromPeriapsisToHyperbolicAnomaly	Tries to convert the time from periapsis passage to hyperbolic anomaly. The value returned is signed and monotonic.
	TryConvertTimeFromPeriapsisToMeanAnomaly	Tries to convert the time from periapsis passage to mean anomaly. The value returned is signed and monotonic even for periodic orbits.
	TryConvertTimeFromPeriapsisToParabolicAnomaly	Tries to convert the time from periapsis passage to parabolic anomaly. The value returned is signed and monotonic.
	TryConvertTimeFromPeriapsisToTrueAnomaly	Tries to convert the time from periapsis passage to true anomaly. The value returned is signed and monotonic even for periodic orbits.
	TryConvertTrueAnomalyToEccentricAnomaly	Tries to convert the true anomaly to the eccentric anomaly.
	TryConvertTrueAnomalyToHyperbolicAnomaly	Tries to convert the true anomaly to the hyperbolic anomaly.
	TryConvertTrueAnomalyToMeanAnomaly	Tries to convert the true anomaly to the mean anomaly.
	TryConvertTrueAnomalyToParabolicAnomaly	Tries to convert the true anomaly to the parabolic anomaly.
	TryConvertTrueAnomalyToTimeFromPeriapsis	True to convert the true anomaly to the time of flight from the corresponding periapsis passage in seconds. The value returned is signed and monotonic even for periodic orbits.
	TryConvertTrueAnomalyToTimeSincePreviousPeriapsis	Tries to convert the true anomaly to the time of flight since the previous periapsis passage in seconds. The value returned is positive and, for closed orbits, periodic.
	TryConvertTrueAnomalyToTimeUntilNextPeriapsis	Tries to convert the true anomaly to the time of flight until the next periapsis passage in seconds. The value returned is positive and, for closed orbits, periodic.

Top

Reference

AGI.Foundation.Coordinates Namespace