The Dynamic Stability module provides:
- The Lateral Eigenmodes (Spiral, Roll, Dutch Roll) and Longitudinal Eigenmodes (Phugoid, Short Period) of the airplane (one set of graph per Eigenmode)
- The Frequential Response Graphs (Bode Diagram) for ailerons, elevator, rudder and spoiler if any
- The Step Response to Elevator, Ailerons and Rudder deflection
The flight path of the airplane is displayed for a step response to a control surface deflection.
The results are displayed in a table and graphically