Aircraft landing with decelerated approach (Longitudinal movement model)

The paper deals with a mathematical model for airplanes' longitudinal movement during the approach-stage of the landing. One has described an aerodynamic decelerated approach and has established the correlation between airplane's flight commands and thrust level (engines' commands). Airplane's command law was issued (a common law, for rudder and throttle positions), according to the approach law, which should be implemented into its board computer for the landing phase of the flight; system's mathematical model was used for some simulations concerning its quality.