The invention discloses a multi-axis rotor wing unmanned aerial vehicle and a flight control method thereof. A large blank area of the plane center position of a fuselage is fully utilized, on the basis of rotor wings of a conventional structure, a coaxial upper and lower double-propeller rotor wing is additionally arranged at the center position of the rotor wings to assist in providing lift force, and the bearing capacity of the unmanned aerial vehicle can be effectively improved on the basis that the overall size of the unmanned aerial vehicle is not increased.

    本发明公开了一种多轴旋翼无人机及其飞行控制方法。本发明充分利用机身平面中心位置大片的空白区域,在常规构型的旋翼基础上,在其中心位置添加一个同轴上下双桨旋翼,辅助提供升力,可在不增加无人机的整体尺寸的基础上,有效提升无人机的承载能力。


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    Titel :

    Multi-axis rotor wing unmanned aerial vehicle and flight control method thereof


    Weitere Titelangaben:

    一种多轴旋翼无人机及其飞行控制方法


    Beteiligte:
    WANG JIANAN (Autor:in) / MENG JIN (Autor:in) / WANG CHUNYAN (Autor:in) / WANG DANDAN (Autor:in)

    Erscheinungsdatum :

    09.04.2021


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    G05D SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES , Systeme zum Steuern oder Regeln nichtelektrischer veränderlicher Größen / B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / G05B Steuer- oder Regelsysteme allgemein , CONTROL OR REGULATING SYSTEMS IN GENERAL




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