A wing deformation monitoring and analysis system includes at least one image sensor (02a, 102b) installed on a portion of the aircraft (100) such that at least one wing (110a, 110b) of the aircraft is located in a field of view (FOV) of the at least one image sensor. The image sensor outputs at least one image signal representing a captured wing image of the at least one wing. An electronic deformation controller (202) is configured to compare the captured wing image to a nominal wing image, determines a deformation of the at least one wing based on the comparison.


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    Title :

    AIRCRAFT WING DEFORMATION MONITORING AND ANALYSIS SYSTEM


    Additional title:

    SYSTEM ZUR ÜBERWACHUNG UND ANALYSE VON FLUGZEUGFLÜGELVERFORMUNGEN
    SYSTÈME DE SURVEILLANCE ET D'ANALYSE DE DÉFORMATION D'AILE D'AÉRONEF


    Contributors:

    Publication date :

    2019-12-04


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

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



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