The AircraftMotionIntegrationPoint type exposes the following members.
Gets or sets the CentralBody to be used in converting the propagation state elements.
Gets the ReferenceFrame used to define the state during integration.
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.)
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 in cases where 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.