Two-body propagator interface.
![]() | Propagates the satellite's path using the specified time interval. |
![]() | The propagator's ephemeris interval. |
![]() | Get the initial state. |
![]() | Step size. Uses Time Dimension. |
Implemented Interface |
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IAgVePropagator |
STK Objects | Send comments on this topic. |
IAgVePropagatorTwoBody Interface |
![]() |
![]() | Propagates the satellite's path using the specified time interval. |
![]() | The propagator's ephemeris interval. |
![]() | Get the initial state. |
![]() | Step size. Uses Time Dimension. |
Implemented Interface |
---|
IAgVePropagator |