VehicleEphemerisCCSDSv2ExportTool#

class ansys.stk.core.stkobjects.VehicleEphemerisCCSDSv2ExportTool#: The Ephemeris/Attitude Export Tool for CCSDSv2 Ephemeris type.

Overview#

Methods

export

Export the ephemeris file.

Properties

`originator`	A string that specifies an identifier of the organization producing the data file.
`object_identifier`	A string defining the Object ID - to be specified as the international spacecraft designator, also known as an NSSDC identifier.
`object_name`	A name for the Object. By recommendation of the CCSDS standard, the name from the SPACEWARN Bulletin should be used.
`central_body_name`	Get or set the central body of the satellite.
`reference_frame`	Get or set the reference frame of the ephemeris.
`date_format`	Get or set the desired date format.
`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.
`time_precision`	If selected, STK uses the Step Size specified in the vehicle’s Basic properties. If not selected, specify a Step Size. Dimensionless.
`step_size`	If the Use Ephemeris Steps option is not selected, enter a Step Size to be used for the vehicle.
`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.
`reference_frames_supported`	Return an array of valid choices.
`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.
`time_system`	Get or set the time system of the ephemeris.
`include_acceleration`	Include acceleration data in the exported file.
`include_covariance`	Include covariance data in the exported file. If covariance data is not available, this property becomes read-only.
`has_covariance_data`	Return true if the object has covariance data.
`file_format`	Get or set the file format that will be generated by the export tool.

Import detail#

from ansys.stk.core.stkobjects import VehicleEphemerisCCSDSv2ExportTool

Property detail#

property VehicleEphemerisCCSDSv2ExportTool.originator: str#: A string that specifies an identifier of the organization producing the data file.

property VehicleEphemerisCCSDSv2ExportTool.object_identifier: str#: A string defining the Object ID - to be specified as the international spacecraft designator, also known as an NSSDC identifier.

property VehicleEphemerisCCSDSv2ExportTool.object_name: str#: A name for the Object. By recommendation of the CCSDS standard, the name from the SPACEWARN Bulletin should be used.

property VehicleEphemerisCCSDSv2ExportTool.central_body_name: str#: Get or set the central body of the satellite.

property VehicleEphemerisCCSDSv2ExportTool.reference_frame: CCSDSReferenceFrame#: Get or set the reference frame of the ephemeris.

property VehicleEphemerisCCSDSv2ExportTool.date_format: CCSDSDateFormat#: Get or set the desired date format.

property VehicleEphemerisCCSDSv2ExportTool.ephemeris_format: 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.

property VehicleEphemerisCCSDSv2ExportTool.time_precision: int#: If selected, STK uses the Step Size specified in the vehicle’s Basic properties. If not selected, specify a Step Size. Dimensionless.

property VehicleEphemerisCCSDSv2ExportTool.step_size: ExportToolStepSize#: If the Use Ephemeris Steps option is not selected, enter a Step Size to be used for the vehicle.

property VehicleEphemerisCCSDSv2ExportTool.time_period: 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.

property VehicleEphemerisCCSDSv2ExportTool.reference_frames_supported: list#: Return an array of valid choices.

property VehicleEphemerisCCSDSv2ExportTool.use_satellite_center_and_frame: bool#: Use the satellite center and frame. Setting the property to ‘True’ will cause CentralBody and ReferenceFrame properties become read-only.

property VehicleEphemerisCCSDSv2ExportTool.time_system: CCSDSTimeSystem#: Get or set the time system of the ephemeris.

property VehicleEphemerisCCSDSv2ExportTool.include_acceleration: bool#: Include acceleration data in the exported file.

property VehicleEphemerisCCSDSv2ExportTool.include_covariance: bool#: Include covariance data in the exported file. If covariance data is not available, this property becomes read-only.

property VehicleEphemerisCCSDSv2ExportTool.has_covariance_data: bool#: Return true if the object has covariance data.

property VehicleEphemerisCCSDSv2ExportTool.file_format: EphemExportToolFileFormat#: Get or set the file format that will be generated by the export tool.

Method detail#

VehicleEphemerisCCSDSv2ExportTool.export(self, file_name: str) → None#

Export the ephemeris file.

Parameters:: file_name : str
Returns:: None