A flag indicating the method to be used to calculate the state transition matrix. Note that even if the CalculateSTM property is set to FALSE, this property still applies if the SpacecraftODProperties.PropagateCovariance flag is to TRUE or if the Spacecraft is included in an estimation process.
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.