Specify the planet using a central body and a desired ephemeris source.
[Visual Basic .NET] |
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Public Function SetPositionSourceCentralBody( _ ByVal CentralBody As String, _ ByVal EphemSource As AgEEphemSourceType _ ) As IAgPlPosCentralBody |
[C#] |
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public IAgPlPosCentralBody SetPositionSourceCentralBody( |
[Managed C++] |
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public: IAgPlPosCentralBody^ SetPositionSourceCentralBody( |
[Java] |
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public IAgPlPosCentralBody setPositionSourceCentralBody( |
[Unmanaged C++] |
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public: HRESULT SetPositionSourceCentralBody( |
- CentralBody
- EphemSource
Member Value Description eEphemAnalytic 0 Analytic ephemeris: use an analytic propagator. Available when orbital elements are known for the Central Body about its parent. eEphemDefault 2 Default: use STK's internal definition of the Central Body to generate ephemeris. By default, STK's internal definition uses the DE file if available. eEphemSpice 3 SPICE: use the SPICE toolkit to generate ephemeris. Available only if a SPICE ephemeris file (*.bsp) has been loaded for the selected planet. eEphemJPLDE 4 Default JPL DE file.