A directional lighting system fitted to an aircraft and comprising firstly a light source mounted on a motor-driven support and secondly a control device serving to control the motor-driven support. According to the invention, such a directional lighting system comprises a selector member for selecting a pointing target that is to be pointed to, a camera for acquiring a plurality of images of the surroundings outside the aircraft, image processor means for identifying the selected pointing target, a calculation unit configured to calculate the current coordinates of the pointing target, and a servocontrol member of the control device for servocontrolling the position of the motor-driven support to occupy an angular orientation as determined by the calculation unit.


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    Title :

    SYSTEME D'ECLAIRAGE DIRECTIONNEL EQUIPANT UN AERONEF ET PROCEDE D'ECLAIRAGE ASSOCIE


    Additional title:

    DIRECTIONAL LIGHTING SYSTEM PROVIDED IN AN AIRCRAFT AND ASSOCIATED LIGHTING METHOD
    RICHTUNGBELEUCHTUNGSSYSTEM EINES LUFTFAHRZEUGS, UND ENTSPRECHENDES BELEUCHTUNGSVERFAHREN


    Contributors:

    Publication date :

    2021-01-27


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    French


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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