Dynamics and control in aeronautics is a key area of research and application within our department. We are specialists in multi-disciplinary design of flight control laws, as well as in development of multi-disciplinary models for aircraft flight dynamics and aircraft on-board systems. We apply, and continuously improve, an integrated flight control laws design process that is supported by methods and tools developed in our department. We further perform modelling and model integration of on-board aircraft systems, aiming at reduction of peak power loads and overall power consumption by systems on-board the aircraft.