VehicleInitialState =================== .. py:class:: ansys.stk.core.stkobjects.VehicleInitialState Class defining the initial state of the vehicle. .. py:currentmodule:: VehicleInitialState Overview -------- .. tab-set:: .. tab-item:: Properties .. list-table:: :header-rows: 0 :widths: auto * - :py:attr:`~ansys.stk.core.stkobjects.VehicleInitialState.representation` - Representation. * - :py:attr:`~ansys.stk.core.stkobjects.VehicleInitialState.propagation_frame` - Do not use this property, as it is deprecated. Use Two-body, J2 and J4 propagators to configure propagation frame. The propagation frame. * - :py:attr:`~ansys.stk.core.stkobjects.VehicleInitialState.supported_propagation_frames` - Do not use this property, as it is deprecated. Use Two-body, J2 and J4 propagators to get a list of supported propagation frames. Returns supported propagation frames. * - :py:attr:`~ansys.stk.core.stkobjects.VehicleInitialState.orbit_epoch` - Get the smart epoch component to configure the orbit state epoch. Import detail ------------- .. code-block:: python from ansys.stk.core.stkobjects import VehicleInitialState Property detail --------------- .. py:property:: representation :canonical: ansys.stk.core.stkobjects.VehicleInitialState.representation :type: IOrbitState Representation. .. py:property:: propagation_frame :canonical: ansys.stk.core.stkobjects.VehicleInitialState.propagation_frame :type: VehiclePropagationFrame Do not use this property, as it is deprecated. Use Two-body, J2 and J4 propagators to configure propagation frame. The propagation frame. .. py:property:: supported_propagation_frames :canonical: ansys.stk.core.stkobjects.VehicleInitialState.supported_propagation_frames :type: list Do not use this property, as it is deprecated. Use Two-body, J2 and J4 propagators to get a list of supported propagation frames. Returns supported propagation frames. .. py:property:: orbit_epoch :canonical: ansys.stk.core.stkobjects.VehicleInitialState.orbit_epoch :type: ITimeToolInstantSmartEpoch Get the smart epoch component to configure the orbit state epoch.