CONTROL SYSTEM FOR CONTROLLING AN AIRCRAFT TRAJECTORY AND METHOD FOR CONTROLLING A TRAJECTORY OF AN AIRCRAFT

摘要

A system for controlling the path of an aircraft on the ground, comprising a determination module configured to determine the current trajectory of the aircraft on the ground, including a series of reference points provided for an aircraft element with unchanged motion device conditions. at least one limit trajectory, including a series of limit reference points that can be reached by the element by driving at least one lateral movement device. The system includes a display assembly comprising a display configured to display a view (200) of a portion of the runway located near the aircraft, and a display generator module configured to display a representative current trajectory curve (202) on the display. said current path and at least one boundary curve (204a, 204b, 206a, 206b) representative of the boundary path, superimposed on the view (200).