A flight control system for an aircraft comprises a processor that processes a plurality of inputs from the aircraft, that contains a plurality of control laws that control operation of the aircraft, and that provides a plurality of outputs that control a plurality of devices located on the aircraft. Also included is a pair of first input devices, wherein a first one of the first input devices is controlled by a pilot of the aircraft, a second one of the first input devices is controlled by a co-pilot of the aircraft, each one of the first input devices being operable to input a first control signal to the processor to cause the aircraft to be in a momentary first priority control condition; and a pair of second input devices located apart from the pair of first input devices, a first one of the second input devices controlled by a pilot of the aircraft, a second one of the second input devices controlled by a co-pilot of the aircraft, each one of the second input devices being operable to input a second control signal to the processor to cause the aircraft to be in a permanent second priority control condition.


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    Title :

    AIRCRAFT SIDESTICK PRIORITY AND DUAL INPUT CONTROL LOGIC


    Additional title:

    FLUGZEUG-SIDESTICK-PRIORITÄT UND DOPPELEINGANGS-STEUERLOGIK
    LOGIQUE DE COMMANDE DE PRIORITÉ DE MANCHE LATÉRAL ET D'ENTRÉE DOUBLE D'AÉRONEF


    Contributors:

    Publication date :

    2019-12-25


    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 / B64C AEROPLANES , Flugzeuge



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