The method involves determining a pitch angle limiting value representative of a maximum admissible angle of incidence, depends on a set of flight parameters and aircraft configurations. A maximum angle of incidence pointer (33) indicating pitch angle limiting value is displayed on pitch scale (23) of the display screen. The maximum angle of incidence pointer and trajectory pointer (27) is provided to form upper and lower limits of dynamic safety envelope (37) representative of normal flight of the aircraft respectively. An independent claim is included for a system to assist piloting of aircraft.


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    Title :

    AIDE AU PILOTAGE D'UN AÉRONEF EN SITUATION DE DÉCROCHAGE


    Additional title:

    PILOT SUPPORT SYSTEM OF AN AIRCRAFT DURING STALL
    PILOTENASSISTENZSYSTEM FÜR EIN LUFTFAHRZEUG BEI STRÖMUNGSABRISS


    Contributors:

    Publication date :

    2020-01-01


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    French


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / G01C Messen von Entfernungen, Höhen, Neigungen oder Richtungen , MEASURING DISTANCES, LEVELS OR BEARINGS / G05D SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES , Systeme zum Steuern oder Regeln nichtelektrischer veränderlicher Größen



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