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. |
FileFormat | Ephemeris file format. |
Filename | Name of external file. |
LimitEphemerisToScenarioInterval | Limit ephemeris for analysis to the Scenario Interval. |
MessageLevel | Message level used to report messages during file loading. |
Override | Opt whether to override times contained in the external file. |
StartTime | Get the start time of ephemeris interval. Uses DateFormat Dimension. |
Step | Step size. Uses Time Dimension. |
StopTime | Get the stop time of ephemeris interval. Uses DateFormat Dimension. |
Implemented Interface |
---|
IAgVePropagator |
Set ground vehicle to use STK External propagator
[C#] | ||
---|---|---|
|
Set the satellite to use the STK External propagator
[C#] | ||
---|---|---|
|
Set ship to use STK External propagator
[C#] | ||
---|---|---|
|
Create a satellite from an external ephemeris file (.e)
[C#] | ||
---|---|---|
|
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] | ||
---|---|---|
|