The invention relates to the technical field of an airplane flying control system and especially relates to a control method for loading signals of main wheels of an airplane. The method is adopted for preventing the situation of incorrect bearing state switching. The control method for the loading signals of the main wheels of the airplane comprises the following steps: during the takeoff or landing of the airplane, collecting the two-redundancy loading signals of a left main wheel of the airplane and the two-redundancy loading signals of a right main wheel by using an airplane control computer; judging if the airplane is loaded by using the airplane control computer according to the quantity of the collected loading signals and the bearing information in the loading signals. According to the control method for the loading signals of the main wheels of the airplane, provided by the invention, during the takeoff or landing of the airplane and under the condition of frequently grounding/leaving of left and right main wheels, the aerial/grounding state of the airplane can be correctly judged by the flying control system according to mechanical two-redundancy electric four-redundancy main wheel loading signals, so that the flying safety of the airplane can be ensured.


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    Titel :

    Control method for loading signals of main wheels of airplane


    Beteiligte:
    ZHANG DONG (Autor:in) / LYU JIAKAI (Autor:in) / HAN SHUMEI (Autor:in)

    Erscheinungsdatum :

    17.02.2016


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / G05B Steuer- oder Regelsysteme allgemein , CONTROL OR REGULATING SYSTEMS IN GENERAL



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