Optimising the aircraft lateral stabilization system in landing mode

Controlling position of an aircraft in its trajectory is a matter of high precision. The requirement on precision is becoming a priority primarily in the phase of landing, when the aircraft is in automated mode of landing controlling/maintaining lateral deviation along the trajectory by autopilot. The contribution is describing shaping and modeling control signals in the stage of final approach for landing. It proposes a system that can eliminate the interfering high-frequency defects of lateral control system stabilizing aircraft deviation during the landing maneuver and simulating the effects of filters onto the feedback dynamics.