Aircraft e.g. cargo aircraft, piloting assisting device for use during approach phase, has guidance system automatically carrying out transition between two guiding modes corresponding to initial and terminal phases, respectively

摘要

The device has a control system (10) e.g. flight control unit, including control units (11A-11n) for controlling a pilot of an aircraft in two guiding modes. A calculation system (7) determines vertical and lateral deviations related to the guiding modes. A guidance system (8) automatically carries out transition between the two guiding modes corresponding to initial and terminal phases, respectively. A display system (9) displays activation of the control system on navigation and primary flight displays (12, 13).