StkExternal propagator interface.
Propagate | Propagates the satellite's path using the specified time interval. |
EphemerisStartEpoch | If overriding the times contained in the external file, specify the time of the first ephemeris point. |
EphemStart | 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. |
FileFormat | Ephemeris file format. |
Filename | Name of external file. |
Override | Opt whether to override times contained in the external file. |
StartTime | The start time of ephemeris interval. Uses DateFormat Dimension. |
Step | Step size. Uses Time Dimension. |
StopTime | 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#] | Copy Code | |
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Set ground vehicle to
use STK External propagator
[C#] | Copy Code | |
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Set the satellite to
use the STK External propagator
[C#] | Copy Code | |
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Set ship to use STK
External propagator
[C#] | Copy Code | |
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Create a satellite
from an external ephemeris file (.e)
[Visual Basic .NET] | Copy Code | |
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|
Set ground vehicle to
use STK External propagator
[Visual Basic .NET] | Copy Code | |
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|
Set the satellite to
use the STK External propagator
[Visual Basic .NET] | Copy Code | |
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|
Set ship to use STK
External propagator
[Visual Basic .NET] | Copy Code | |
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