ModifiedKeplerianElements Constructor (Double, Double, Double, Double, Double, Double, Double)

Initialize a set of modified Keplerian elements.

Namespace: AGI.Foundation.Coordinates
Assembly: AGI.Foundation.Core (in AGI.Foundation.Core.dll) Version: 25.1.421.0 (25.1.421.0)

Syntax

C++

Copy

public ModifiedKeplerianElements(
	double radiusOfPeriapsis,
	double inverseSemimajorAxis,
	double inclination,
	double argumentOfPeriapsis,
	double rightAscensionOfAscendingNode,
	double trueAnomaly,
	double gravitationalParameter
)

Public Sub New ( 
	radiusOfPeriapsis As Double,
	inverseSemimajorAxis As Double,
	inclination As Double,
	argumentOfPeriapsis As Double,
	rightAscensionOfAscendingNode As Double,
	trueAnomaly As Double,
	gravitationalParameter As Double
)

public:
ModifiedKeplerianElements(
	double radiusOfPeriapsis, 
	double inverseSemimajorAxis, 
	double inclination, 
	double argumentOfPeriapsis, 
	double rightAscensionOfAscendingNode, 
	double trueAnomaly, 
	double gravitationalParameter
)

new : 
        radiusOfPeriapsis : float * 
        inverseSemimajorAxis : float * 
        inclination : float * 
        argumentOfPeriapsis : float * 
        rightAscensionOfAscendingNode : float * 
        trueAnomaly : float * 
        gravitationalParameter : float -> ModifiedKeplerianElements

Parameters

radiusOfPeriapsis: Type: System.Double
Radius of periapsis (distance).
inverseSemimajorAxis: Type: System.Double
The inverse of semimajor axis (distance).
inclination: Type: System.Double
Inclination, in radians.
argumentOfPeriapsis: Type: System.Double
Argument of periapsis, in radians.
rightAscensionOfAscendingNode: Type: System.Double
Right ascension of the ascending node, in radians.
trueAnomaly: Type: System.Double
True anomaly, in radians.
gravitationalParameter: Type: System.Double
The gravitational parameter associated with these elements (distance cubed per time squared).

Exceptions

Exception	Condition
ArgumentOutOfRangeException	Thrown when inclination is less than zero or greater than π.
ArgumentOutOfRangeException	Thrown when the orbit is hyperbolic and the absolute value of trueAnomaly is greater than or equal to arccosine(1 / eccentricity).

Remarks

The classification of the OrbitType is exact, so to be classified as a Circular orbit, the inverse of radiusOfPeriapsis must be exactly equal to inverseSemimajorAxis.

Reference

ModifiedKeplerianElements Class

ModifiedKeplerianElements Overload

AGI.Foundation.Coordinates Namespace