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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    Title :

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


    Contributors:
    ZHANG QIAN (author) / ZHANG YINGSHU (author)

    Publication date :

    2015-11-25


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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