A system (12) for an aircraft (10) includes an optical sensor, at least one aircraft sensor, and a controller (18). The optical sensor is configured to emit a laser outside the aircraft (10), and the at least one aircraft sensor is configured to sense at least one aircraft condition. The controller (18) is configured to determine a first operational state of the aircraft (10) based upon the at least one aircraft condition and determine a second operational state of the aircraft (10) based on the at least one aircraft condition, and operate the optical sensor to emit the laser at a first intensity during the first operational state and a second intensity during the second operational state, wherein the second intensity is greater than the first intensity.


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    Titel :

    MULTIPLE OPERATIONAL MODES FOR AIRCRAFT LASER SENSING SYSTEMS


    Weitere Titelangaben:

    MEHRERE BETRIEBSMODI FÜR FLUGZEUGLASERMESSSYSTEME
    MODES DE FONCTIONNEMENT MULTIPLES POUR SYSTÈMES DE DÉTECTION DE LASER POUR AÉRONEF


    Beteiligte:
    SLY JAIME (Autor:in) / MILLER MARK SHERWOOD (Autor:in)

    Erscheinungsdatum :

    2024-01-03


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    G01S RADIO DIRECTION-FINDING , Funkpeilung / G08G Anlagen zur Steuerung, Regelung oder Überwachung des Verkehrs , TRAFFIC CONTROL SYSTEMS



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