StkExternal propagator interface.
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Propagates the satellite's path using the specified time interval. |
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If overriding the times contained in the external file, specify the time of the first ephemeris point. |
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This property is deprecated. Use EphemerisStartEpoch instead. If overriding the times contained in the external file, specify the time of the first ephemeris point. Uses DateFormat Dimension. |
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Ephemeris file format. |
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Name of external file. |
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Opt whether to override times contained in the external file. |
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The start time of ephemeris interval. Uses DateFormat Dimension. |
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Step size. Uses Time Dimension. |
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The stop time of ephemeris interval. Uses DateFormat Dimension. |
Implemented Interface |
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IAgVePropagator |
Create a satellite
from an external ephemeris file (.e)
[C#] | ![]() |
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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)
[Visual Basic .NET] | ![]() |
|
---|---|---|
|
Set ground vehicle to
use STK External propagator
[Visual Basic .NET] | ![]() |
|
---|---|---|
|
Set the satellite to
use the STK External propagator
[Visual Basic .NET] | ![]() |
|
---|---|---|
|
Set ship to use STK
External propagator
[Visual Basic .NET] | ![]() |
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|