Bypassing the limitations of frequency-domain constraints for a truly modern control paradigm.
Applying Convex Stability across domains
Dynamics & Control
Current literature Aircraft Dynamics Models in the open loop situation are categorized as having Phugoid and Short-Period Modes and are designed for closed loop stability separating the dynamics under `fast dynamics (short period)' and `slow dynamics (phugoid)' type time scale separation viewpoint which introduces non-robustness. Our RES CSSP Tool-Box designs do not need such assumptions. They promise very high robust stability margins for various types of perturbations.