The present invention relates to a system and method for detecting an aircraft jitter. The aircraft jitter detection system comprises: a jitter detection apparatus, which detects accelerations of pitch and yaw of the aircraft; a data acquisition apparatus, which obtains accelerations in two directions detected by the jitter detection apparatus; and a jitter determination apparatus, which extracts frequency spectrum and energy information of the jitter according to the accelerations in two directions obtained by the data acquisition apparatus, and determines whether the aircraft jitters.


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    Titel :

    SYSTEM AND METHOD FOR DETECTING AN AIRCRAFT JITTER


    Beteiligte:
    WU JIAJU (Autor:in) / GU ZHUPING (Autor:in) / HUANG LEI (Autor:in) / DING HUIFENG (Autor:in) / ZHENG FENGLIANG (Autor:in) / REN QIFENG (Autor:in) / ZHANG YANFENG (Autor:in)

    Erscheinungsdatum :

    23.07.2015


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



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