The invention discloses an aircraft safety take-off control method. The method comprises the steps of 10, obtaining information of an angle between an aircraft body and the horizontal plane through an angle sensor; 20, judging whether the obtained information of the angle is smaller than or equal to the maximum safety angle threshold value or not; 30, controlling the aircraft to take off if the obtained information of the angle is smaller than or equal to the maximum safety angle threshold value. The invention further discloses an aircraft safety take-off control device. By the adoption of the technical scheme, whether the aircraft is horizontally placed or not can be accurately judged, and the aircraft can safely take off.


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    Titel :

    Aircraft safety take-off control method and device


    Beteiligte:
    ZHANG XIANZHI (Autor:in)

    Erscheinungsdatum :

    2015-07-22


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / G05D SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES , Systeme zum Steuern oder Regeln nichtelektrischer veränderlicher Größen