GravityGradientTorque Constructor (Point, CentralBody, Double, Matrix3By3Symmetric, Axes)

Initializes the gravity-gradient torque model.

Namespace: AGI.Foundation.Celestial
Assembly: AGI.Foundation.OrbitPropagation (in AGI.Foundation.OrbitPropagation.dll) Version: 24.1.418.0 (24.1.418.0)

Syntax

C++

Copy

public GravityGradientTorque(
	Point bodyCenterOfMass,
	CentralBody centralBody,
	double gravitationalParameter,
	Matrix3By3Symmetric inertiaMatrix,
	Axes bodyAxes
)

Public Sub New ( 
	bodyCenterOfMass As Point,
	centralBody As CentralBody,
	gravitationalParameter As Double,
	inertiaMatrix As Matrix3By3Symmetric,
	bodyAxes As Axes
)

public:
GravityGradientTorque(
	Point^ bodyCenterOfMass, 
	CentralBody^ centralBody, 
	double gravitationalParameter, 
	Matrix3By3Symmetric inertiaMatrix, 
	Axes^ bodyAxes
)

new : 
        bodyCenterOfMass : Point * 
        centralBody : CentralBody * 
        gravitationalParameter : float * 
        inertiaMatrix : Matrix3By3Symmetric * 
        bodyAxes : Axes -> GravityGradientTorque

Parameters

bodyCenterOfMass: Type: AGI.Foundation.GeometryPoint
The center of mass point of the gravity-gradient satellite.
centralBody: Type: AGI.Foundation.CelestialCentralBody
The body which creates the gravity and provides a reference point at its center of mass.
gravitationalParameter: Type: SystemDouble
The gravitational parameter to use when computing gravity, in meters cubed per second squared.
inertiaMatrix: Type: AGI.Foundation.CoordinatesMatrix3By3Symmetric
The 3x3 inertia matrix of the gravity-gradient satellite. This must be defined in the BodyAxes.
bodyAxes: Type: AGI.Foundation.GeometryAxes
The body axes of the gravity-gradient satellite. These should be the IntegrationAxes of the PropagationEulerianAxes associated with the gravity-gradient satellite.

Reference

GravityGradientTorque Class

GravityGradientTorque Overload

AGI.Foundation.Celestial Namespace