The STK Ephemeris type for the Export Ephemeris/Attitude Tool.
Export | Exports the ephemeris file. |
CentralBodyName | Gets or sets the central body of the coordinate system in which to express the ephemeris. |
CoordinateSystem | Gets or sets the coordinate system in which to express the ephemeris. Some frames are allowed for use only when the CentralBodyName is Earth. If Earth or the Sun is the central body, the Inertial coordinate system is not an available option - use ICRF instead. |
CovarianceType | Choose to export position covariance (3x3), position/velocity covariance (6x6), or no covariance information. CovarianceType is valid only if the vehicle has ephemeris with covariance. |
IncludeInterp | Include or ignore interpolation boundaries. |
StepSize | If the Use Ephemeris Steps option is not selected, enter a Step Size to be used for the vehicle. |
TimePeriod | Sets 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. |
UseVehicleCentralBody | Uses vehicle's central body. |
VersionFormat | Provides the option to generate files compatible with prior versions of STK. |
Export a vehicle STK ephemeris to an external file
[C#] | ||
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Export a vehicle STK ephemeris to an external file
[Visual Basic .NET] | ||
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