Landing navigation method and corresponding ground station

摘要

The method involves calculating corrected position of aircraft from radio satellite signals of differential positioning of GNSS system and correction information of the signals from a central ground station. Vertical and horizontal guiding distances of aircraft with respect to a determined approach trajectory is calculated from the corrected position of the aircraft and ideal trajectory information transmitted from a ground beacon. An independent claim is also included for a ground marker for implementing a method of guiding an aircraft.