A flight control system includes at least one flight domain protection module intended at least for manual piloting and an auxiliary element configured to automatically transmit to the protection module, upon a detection of automatic piloting of the aircraft using an automatic piloting device, a predetermined auxiliary position, representing a control stick position equivalent, the protection module using the auxiliary position as a control stick position to implement a flight domain protection during the automatic piloting.


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    Title :

    Electric flight control system and method for an aircraft


    Contributors:

    Publication date :

    2016-04-19


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    G05D SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES , Systeme zum Steuern oder Regeln nichtelektrischer veränderlicher Größen / G01C Messen von Entfernungen, Höhen, Neigungen oder Richtungen , MEASURING DISTANCES, LEVELS OR BEARINGS / B64C AEROPLANES , Flugzeuge / G06F ELECTRIC DIGITAL DATA PROCESSING , Elektrische digitale Datenverarbeitung



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