The invention provides a method for controlling a quadrotor aircraft by a vector rotation method. The method comprises the steps that Roll-direction controlled quantity and Pitch-direction controlled quantity which are received by the quadrotor aircraft and sent by a remote control unit are converted to be vectors; the vectors correspond to the X direction and the Y direction in a coordinate system respectively; then the vectors are rotated and then are mapped again to a new coordinate system X'Y' according to the rotating angles of an aircraft body to control the entire aircraft body to advance, retreat, fly leftwards and fly rightwards.


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    Titel :

    Method for controlling quadrotor aircraft by vector rotation method


    Beteiligte:
    CHEN ERZHENG (Autor:in)

    Erscheinungsdatum :

    2015-07-08


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / G05D SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES , Systeme zum Steuern oder Regeln nichtelektrischer veränderlicher Größen




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