StkExternal propagator interface.
![]() | Propagates the satellite's path using the specified time interval. |
![]() | If overriding the times contained in the external file, specify the time of the first ephemeris point. |
![]() | Ephemeris file format. |
![]() | Name of external file. |
![]() | Limit ephemeris for analysis to the Scenario Interval. |
![]() | Message level used to report messages during file loading. |
![]() | Opt whether to override times contained in the external file. |
![]() | Get the start time of ephemeris interval. Uses DateFormat Dimension. |
![]() | Step size. Uses Time Dimension. |
![]() | Get the stop time of ephemeris interval. Uses DateFormat Dimension. |
Implemented Interface |
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IAgVePropagator |
Set ground vehicle to use STK External propagator
[C#] | ||
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Set the satellite to use the STK External propagator
[C#] | ||
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Set ship to use STK External propagator
[C#] | ||
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Create a satellite from an external ephemeris file (.e)
[C#] | ||
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Create a satellite from an external ephemeris file (.e)
[Visual Basic .NET] | ||
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Set ground vehicle to use STK External propagator
[Visual Basic .NET] | ||
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Set the satellite to use the STK External propagator
[Visual Basic .NET] | ||
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Set ship to use STK External propagator
[Visual Basic .NET] | ||
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