Flag indicating whether or not to calculate the state transition matrix at each integration step as part of the state integration. If the PropagateCovariance flag is set to TRUE on the SpacecraftODProperties object or if the Spacecraft is in an estimation process, the STM is always calculated. If the Spacecraft.Propagator is not an Integrator type then this property is ignored.
Timing Precision Mode
This page describes functionality in nanosecond timing precision mode.
Click here to see the documentation for this object in millisecond timing precision mode.