AircraftMotionElement Properties |
The AircraftMotionElement type exposes the following members.
Name | Description | |
---|---|---|
Identification |
Gets or sets the string identifying this instance in the overall output.
| |
InitialPosition |
Gets or sets the initial position in the fixed frame.
| |
InitialVelocity |
Gets or sets the initial velocity in the fixed frame.
| |
IntegrationPoint |
Gets a Point which is parameterized on the position and velocity in the state
during integration.
This point is only valid while the NumericalPropagator is running.
For more general use, a PointInterpolator should be created from the
NumericalPropagationStateHistory produced by the propagator.
| |
Mass |
Gets or sets the mass used to determine the equations of motion.
Note that the derivatives of mass are not implicitly included in the integration.
Another PropagationStateElement must be added to
the set of integration elements to account for the change in mass over time.
|