VehicleEphemerisCCSDSExportTool =============================== .. py:class:: ansys.stk.core.stkobjects.VehicleEphemerisCCSDSExportTool VehicleEphemerisCCSDSExportTool Class. .. py:currentmodule:: VehicleEphemerisCCSDSExportTool Overview -------- .. tab-set:: .. tab-item:: Methods .. list-table:: :header-rows: 0 :widths: auto * - :py:attr:`~ansys.stk.core.stkobjects.VehicleEphemerisCCSDSExportTool.export` - Export the ephemeris file. .. tab-item:: Properties .. list-table:: :header-rows: 0 :widths: auto * - :py:attr:`~ansys.stk.core.stkobjects.VehicleEphemerisCCSDSExportTool.originator` - A string that specifies an identifier of the organization producing the data file. * - :py:attr:`~ansys.stk.core.stkobjects.VehicleEphemerisCCSDSExportTool.object_identifier` - A string defining the Object ID - to be specified as the international spacecraft designator, also known as an NSSDC identifier. * - :py:attr:`~ansys.stk.core.stkobjects.VehicleEphemerisCCSDSExportTool.object_name` - A name for the Object. By recommendation of the CCSDS standard, the name from the SPACEWARN Bulletin should be used. * - :py:attr:`~ansys.stk.core.stkobjects.VehicleEphemerisCCSDSExportTool.central_body_name` - Get or set the central body of the coordinate system in which to express the ephemeris. * - :py:attr:`~ansys.stk.core.stkobjects.VehicleEphemerisCCSDSExportTool.reference_frame` - Get or set the reference frame in which to express the ephemeris. Some frames are allowed for use only when the CentralBodyName is Earth or Moon. * - :py:attr:`~ansys.stk.core.stkobjects.VehicleEphemerisCCSDSExportTool.date_format` - Get or set the desired date format. * - :py:attr:`~ansys.stk.core.stkobjects.VehicleEphemerisCCSDSExportTool.ephemeris_format` - Get or set the desired format to be used for representing the position and velocity information as either scientific notation or floating point notation. Scientific notation is recommended when possible. * - :py:attr:`~ansys.stk.core.stkobjects.VehicleEphemerisCCSDSExportTool.time_precision` - If selected, STK uses the Step Size specified in the vehicle's Basic properties. If not selected, specify a Step Size. Dimensionless. * - :py:attr:`~ansys.stk.core.stkobjects.VehicleEphemerisCCSDSExportTool.step_size` - If the Use Ephemeris Steps option is not selected, enter a Step Size to be used for the vehicle. * - :py:attr:`~ansys.stk.core.stkobjects.VehicleEphemerisCCSDSExportTool.time_period` - Set the time period. Options are Use Entire Ephemeris - STK creates a data file using the Start and Stop Time specified in the vehicle's Orbit tab or Specify Time Period - STK creates a data file using the Start and Stop Time specified here. * - :py:attr:`~ansys.stk.core.stkobjects.VehicleEphemerisCCSDSExportTool.reference_frames_supported` - Return an array of valid choices. * - :py:attr:`~ansys.stk.core.stkobjects.VehicleEphemerisCCSDSExportTool.use_satellite_center_and_frame` - Use the satellite center and frame. Setting the property to 'True' will cause CentralBody and ReferenceFrame properties become read-only. * - :py:attr:`~ansys.stk.core.stkobjects.VehicleEphemerisCCSDSExportTool.time_system` - Get or set the time system of the ephemeris. Import detail ------------- .. code-block:: python from ansys.stk.core.stkobjects import VehicleEphemerisCCSDSExportTool Property detail --------------- .. py:property:: originator :canonical: ansys.stk.core.stkobjects.VehicleEphemerisCCSDSExportTool.originator :type: str A string that specifies an identifier of the organization producing the data file. .. py:property:: object_identifier :canonical: ansys.stk.core.stkobjects.VehicleEphemerisCCSDSExportTool.object_identifier :type: str A string defining the Object ID - to be specified as the international spacecraft designator, also known as an NSSDC identifier. .. py:property:: object_name :canonical: ansys.stk.core.stkobjects.VehicleEphemerisCCSDSExportTool.object_name :type: str A name for the Object. By recommendation of the CCSDS standard, the name from the SPACEWARN Bulletin should be used. .. py:property:: central_body_name :canonical: ansys.stk.core.stkobjects.VehicleEphemerisCCSDSExportTool.central_body_name :type: str Get or set the central body of the coordinate system in which to express the ephemeris. .. py:property:: reference_frame :canonical: ansys.stk.core.stkobjects.VehicleEphemerisCCSDSExportTool.reference_frame :type: CCSDSReferenceFrame Get or set the reference frame in which to express the ephemeris. Some frames are allowed for use only when the CentralBodyName is Earth or Moon. .. py:property:: date_format :canonical: ansys.stk.core.stkobjects.VehicleEphemerisCCSDSExportTool.date_format :type: CCSDSDateFormat Get or set the desired date format. .. py:property:: ephemeris_format :canonical: ansys.stk.core.stkobjects.VehicleEphemerisCCSDSExportTool.ephemeris_format :type: CCSDSEphemerisFormatType Get or set the desired format to be used for representing the position and velocity information as either scientific notation or floating point notation. Scientific notation is recommended when possible. .. py:property:: time_precision :canonical: ansys.stk.core.stkobjects.VehicleEphemerisCCSDSExportTool.time_precision :type: int If selected, STK uses the Step Size specified in the vehicle's Basic properties. If not selected, specify a Step Size. Dimensionless. .. py:property:: step_size :canonical: ansys.stk.core.stkobjects.VehicleEphemerisCCSDSExportTool.step_size :type: ExportToolStepSize If the Use Ephemeris Steps option is not selected, enter a Step Size to be used for the vehicle. .. py:property:: time_period :canonical: ansys.stk.core.stkobjects.VehicleEphemerisCCSDSExportTool.time_period :type: ExportToolTimePeriod Set the time period. Options are Use Entire Ephemeris - STK creates a data file using the Start and Stop Time specified in the vehicle's Orbit tab or Specify Time Period - STK creates a data file using the Start and Stop Time specified here. .. py:property:: reference_frames_supported :canonical: ansys.stk.core.stkobjects.VehicleEphemerisCCSDSExportTool.reference_frames_supported :type: list Return an array of valid choices. .. py:property:: use_satellite_center_and_frame :canonical: ansys.stk.core.stkobjects.VehicleEphemerisCCSDSExportTool.use_satellite_center_and_frame :type: bool Use the satellite center and frame. Setting the property to 'True' will cause CentralBody and ReferenceFrame properties become read-only. .. py:property:: time_system :canonical: ansys.stk.core.stkobjects.VehicleEphemerisCCSDSExportTool.time_system :type: CCSDSTimeSystem Get or set the time system of the ephemeris. Method detail ------------- .. py:method:: export(self, file_name: str) -> None :canonical: ansys.stk.core.stkobjects.VehicleEphemerisCCSDSExportTool.export Export the ephemeris file. :Parameters: **file_name** : :obj:`~str` :Returns: :obj:`~None`