본 발명은 항공기 진동 검출 시스템 및 방법에 관한 것이다. 항공기 진동 검출 시스템은, 항공기의 피칭 및 요잉 가속도를 감지하는 진동 감지 장치; 상기 진동 감지 장치에 의해 감지된 2개의 방향에서의 가속도를 취득하는 데이터 취득 장치; 및 상기 데이터 취득 장치에 의해 취득된 2개의 방향에서의 가속도에 로부터, 진동 주파수 스팩트럼과 에너지 정보를 추출하고, 항공기에 진동이 발생하였는지를 판단하는 진동 확정 장치; 를 포함한다.

    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 :

    A SYSTEM AND METHOD FOR DETECTING AN AIRCRAFT JITTER


    Weitere Titelangaben:

    항공기 진동 검출 시스템 및 방법


    Erscheinungsdatum :

    09.07.2019


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Koreanisch


    Klassifikation :

    IPC:    B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen / G01P MEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION OR SHOCK , Messen der Linear- oder Winkelgeschwindigkeit, der Beschleunigung, der Verzögerung oder des Stoßes



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