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.
SYSTEME D'ECLAIRAGE DIRECTIONNEL EQUIPANT UN AERONEF ET PROCEDE D'ECLAIRAGE ASSOCIE
DIRECTIONAL LIGHTING SYSTEM PROVIDED IN AN AIRCRAFT AND ASSOCIATED LIGHTING METHOD
RICHTUNGBELEUCHTUNGSSYSTEM EINES LUFTFAHRZEUGS, UND ENTSPRECHENDES BELEUCHTUNGSVERFAHREN
27.01.2021
Patent
Elektronische Ressource
Französisch
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
Système d’éclairage directionnel équipant un aéronef et procédé d’éclairage associé
Europäisches Patentamt | 2021
|Europäisches Patentamt | 2019
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