Disclosed is a method for controlling minimum-radius limitation turning of an airplane through differential braking. According to a friction coefficient of a tire and a track, visualized braking pressure and turning linear speed control parameters are provided for an aviator, and rapid turning of the airplane with the structurally-allowable minimum turning radius is achieved. Maneuverability and safety of the airplane turning process controlled by the aviator on the ground through the differential braking are ensured.


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    Titel :

    Method for controlling minimum-radius limitation turning of airplane through differential braking


    Beteiligte:
    ZHANG QIAN (Autor:in) / ZHANG YINGSHU (Autor:in)

    Erscheinungsdatum :

    25.11.2015


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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