A system and various methods for determining a center of mass of an aircraft with a plurality of shock strut assemblies is illustrated. Multiple sensors, including a gas pressure sensor, and/or a position sensor, may be used to gather data and determine the center of mass of the aircraft. Various methods illustrated herein may evaluate the center of mass relative to a wheelbase axis and a wheel tread axis based on the gathered data.


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    Titel :

    AIRCRAFT WEIGHT AND CENTER OF MASS ESTIMATION SYSTEM


    Beteiligte:
    REBER SUSANNE M (Autor:in) / HAWKO KEVIN (Autor:in) / FAZELI AMIR (Autor:in) / CEPIC ADNAN (Autor:in)

    Erscheinungsdatum :

    2022-01-13


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    G01M TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES , Prüfen der statischen oder dynamischen Massenverteilung rotierender Teile von Maschinen oder Konstruktionen / B64C AEROPLANES , Flugzeuge



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