A sensor (300) in an aircraft cargo handling system may comprise a housing (302), an infrared light emitter, an infrared light photoreceptor (622), and a microprism (413). The sensor may be configured to detect an object in proximity to the sensor using electromagnetic waves and voltage measurements. The sensor may include a microcontroller configured to read the voltage measurements associated with infrared electromagnetic waves, compare the voltage measurements to a threshold voltage, and determine the functional condition of the sensor based on the comparison.


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    Title :

    PDU SENSOR USING MULTI OPTICAL PRISM


    Additional title:

    PDU-SENSOR MIT EINEM OPTISCHEN MEHRFACHPRISMA
    CAPTEUR PDU UTILISANT UN PRISME OPTIQUE MULTIPLE


    Contributors:

    Publication date :

    2023-06-21


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    G01S RADIO DIRECTION-FINDING , Funkpeilung / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / G01V Geophysik , GEOPHYSICS



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