Properties for the Mission Control Sequence.
![]() | Append the existing ephemeris with another individual segment mode run. |
![]() | Append the existing ephemeris with another individual segment mode run, starting at a specified state. Ephemeris is cleared from time based on clear direction. |
![]() | Append the existing ephemeris with another individual segment mode run, starting at a specified time. Ephemeris is cleared from time based on clear direction. |
![]() | Applies all active profile changes in all target sequences. |
![]() | Begins an individual segment mode run. |
![]() | Clears the draw while calculating graphics. |
![]() | Ends an individual segment mode run. |
![]() | Resets all active profiles in all target sequences. |
![]() | Runs the current MCS. |
![]() | Runs the current MCS and returns an error code. |
![]() | Get the Automatic Sequences. |
![]() | Get the calculation graphs. |
![]() | Get the Mission Control Sequence. |
![]() | Get the Mission Control Sequence options. |
Implemented Interface |
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IAgVePropagator |
Name |
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AgVADriverMCS |
Configure the Astrogrator propagator
[C#] | ||
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Configure the Astrogrator propagator
[Visual Basic .NET] | ||
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|
Set satellite propagator to Astrogator and clear segments
[Python - STK API] | ||
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Run the Astrogator MCS
[Python - STK API] | ||
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Set satellite propagator to Astrogator and clear segments
[MATLAB] | ||
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|
Run the Astrogator MCS
[MATLAB] | ||
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Create a new component through the Component Browser
[MATLAB] | ||
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|