PropagationEulerianAxes Constructor (String, ReferenceFrame, UnitQuaternion, Cartesian, Matrix3By3Symmetric) | 
 
            Initializes a new instance.
            
 
    Namespace: 
   AGI.Foundation.Propagators
    Assembly:
   AGI.Foundation.OrbitPropagation (in AGI.Foundation.OrbitPropagation.dll) Version: 25.1.421.0 (25.1.421.0)
Syntaxpublic PropagationEulerianAxes(
	string id,
	ReferenceFrame propagationFrame,
	UnitQuaternion initialAttitudeQuaternion,
	Cartesian initialAngularVelocity,
	Matrix3By3Symmetric inertiaMatrix
)
Public Sub New ( 
	id As String,
	propagationFrame As ReferenceFrame,
	initialAttitudeQuaternion As UnitQuaternion,
	initialAngularVelocity As Cartesian,
	inertiaMatrix As Matrix3By3Symmetric
)
public:
PropagationEulerianAxes(
	String^ id, 
	ReferenceFrame^ propagationFrame, 
	UnitQuaternion initialAttitudeQuaternion, 
	Cartesian initialAngularVelocity, 
	Matrix3By3Symmetric inertiaMatrix
)
new : 
        id : string * 
        propagationFrame : ReferenceFrame * 
        initialAttitudeQuaternion : UnitQuaternion * 
        initialAngularVelocity : Cartesian * 
        inertiaMatrix : Matrix3By3Symmetric -> PropagationEulerianAxesParameters
- id
 - Type: SystemString
A unique string identifying this attitude in the output. - propagationFrame
 - Type: AGI.Foundation.GeometryReferenceFrame
The inertial frame in which to propagate. - initialAttitudeQuaternion
 - Type: AGI.Foundation.CoordinatesUnitQuaternion
The body-fixed attitude at the starting epoch of propagation with respect to the axes
            of the propagationFrame. - initialAngularVelocity
 - Type: AGI.Foundation.CoordinatesCartesian
The body-fixed angular velocity at the starting epoch of propagation. - inertiaMatrix
 - Type: AGI.Foundation.CoordinatesMatrix3By3Symmetric
The 3x3 body-fixed, positive definite inertia matrix of the rigid body. 
See Also