The invention discloses a control method and device for an aircraft auxiliary display assembly. The control device comprises an information display module which is configured to display a default information interface on the auxiliary display assembly; the state recognition module is configured to recognize a flight phase of the aircraft based on state information provided by a flight management system, and the information display module is configured to determine whether an additional information interface corresponding to the flight phase exists or not; if the additional information interface corresponding to the flight stage exists, the additional information interface corresponding to the flight stage is displayed on the auxiliary display assembly, and the additional information interface comprises information items different from the default information interface.

    公开了一种用于航空器辅助显示组件的控制方法和装置。该控制装置包括:信息显示模块,其被配置成在所述辅助显示组件上显示默认信息界面;状态识别模块,其被配置成基于由飞行管理系统提供的状态信息来识别所述航空器所处的飞行阶段,其中所述信息显示模块被配置成确定是否存在与所述飞行阶段相对应的附加信息界面,如果存在与所述飞行阶段相对应的附加信息界面,则在所述辅助显示组件上显示与所述飞行阶段相对应的附加信息界面,其中所述附加信息界面包含与所述默认信息界面不同的信息项。


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    Titel :

    Control method and device for auxiliary display assembly of aircraft


    Weitere Titelangaben:

    用于航空器辅助显示组件的控制方法和装置


    Beteiligte:
    WANG JUN (Autor:in) / CHEN TIANTIAN (Autor:in) / LI XIANXUE (Autor:in) / SONG TINGYING (Autor:in) / ZHU HONGYU (Autor:in) / HE SHUPEI (Autor:in)

    Erscheinungsdatum :

    2022-12-02


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

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



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