PropagationEulerianAxes Properties | 
The PropagationEulerianAxes type exposes the following members.
| Name | Description | |
|---|---|---|
| AppliedTorques | 
            Gets a list of the torques applied on the IntegrationAxes.
            These torques will be converted to the body-fixed frame before they are evaluated.
              | |
| Dimension | 
            Gets the number of parameters (per Order) within this element.
              (Overrides PropagationStateElementDimension.) | |
| Identification | 
            Gets or sets the string identifying this instance in the overall output.
              (Inherited from PropagationStateElement.) | |
| IncludeHighestDerivativeInOutput | 
            Gets or sets a value indicating whether to include the derivative computed at each step with the output.
            If this is true, the output converted from the raw state will contain the derivative
            associated with the Order of  the differential equation.
              (Inherited from PropagationStateElement.) | |
| InertiaMatrix | 
            Gets or sets the 3x3 inertia matrix of the body on which the torques are applied.
            This must be defined in the same body-fixed frame that the angular velocity is defined.
              | |
| InitialAngularVelocity | 
            Gets or sets the initial angular velocity expressed in body-fixed axes.
              | |
| InitialAttitudeQuaternion | 
            Gets or sets the initial attitude quaternion that rotates from the IntegrationFrame to the body-fixed reference frame.
              | |
| IntegrationAxes | 
            Gets a Axes which is parameterized on the attitude and angular velocity in the state during integration.
            This axes is only valid while the NumericalPropagator is running.
            For more general use, a AxesInterpolator or a RotationalMotionInterpolator should be created from the
            NumericalPropagationStateHistory produced by the propagator.
              | |
| IntegrationFrame | 
            Gets or sets the inertial ReferenceFrame in which the attitude is defined.
            By default, the integration frame is set to the InertialFrame of the Earth.
              | |
| IsFrozen | 
            Gets a value indicating whether this object is frozen.  A frozen object cannot be modified and an
            ObjectFrozenException will be thrown if an attempt is made to do so.
              (Inherited from DefinitionalObject.) | |
| Order | 
            Gets the order of the differential equation corresponding to this element.
              (Overrides PropagationStateElementOrder.) | |
| StateParameter | 
            Gets or sets a parameter which represents the state during propagation.  In general,
            users should never need to explicitly set this property.  It should only be set
            when multiple NumericalPropagator objects are running in the same EvaluatorGroup,
            such as when elements of a state require additional instances of a NumericalPropagator
            inside their implementation in order to produce their values.  In such cases, it may
            be necessary to distinguish between the state of the exterior propagator and the
            state of the interior propagator.  In these cases, it is up to the user to ensure
            that both the state and all of its elements are configured with the same parameter.
            Otherwise, the state will throw an exception when creating its propagator.
              (Overrides PropagationStateElementStateParameter.) |