The invention discloses a method for displaying a required navigation performance (RNP) parameter of an aircraft. The method comprises: displaying a first frame expressing a range of an RNP value, displaying a second frame expressing a navigation system error (NSE) real-time value of the aircraft; and displaying a third frame expressing an RNP tolerance area. In addition, the invention also discloses a system for displaying a required navigation performance parameter of an aircraft and an aircraft containing the same. With the method and system, an RNP running state of an aircraft in three-dimensional space can be monitored visually.


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    Title :

    Method and system for displaying required navigation performance parameter


    Contributors:
    ZHENG ZHIMING (author) / YE JUNHUI (author) / YU LIANG (author) / ZHAO CHUNLING (author) / YAN LINFANG (author) / ZHANG KEZHI (author) / MENG FANDONG (author)

    Publication date :

    2015-12-23


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    G08G Anlagen zur Steuerung, Regelung oder Überwachung des Verkehrs , TRAFFIC CONTROL SYSTEMS



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