The invention discloses a high-wind-resistance tail cone type mooring unmanned aerial vehicle and a flight control method thereof. The high-wind-resistance tail cone type mooring unmanned aerial vehicle comprises a wind speed and direction sensor, a mooring cable, a multi-rotor mechanism, a tail propulsion rotor, a flight control system and a mooring cable control device. The wind speed and direction sensor is fixed on a mounting bracket, measures the wind direction and wind speed of the position of the unmanned aerial vehicle and provides wind resistance information for the flight control system. The multi-rotor mechanism is composed of a plurality of horizontally-installed rotors and used for adjusting the lifting force and controlling the posture and position of the unmanned aerial vehicle. The tail propelling rotor wing is composed of a tail rod and a vertically-installed rotor wing body, provides horizontal thrust and is used for resisting wind resistance in the horizontal direction. The flight control system adjusts the rotating speeds of the multiple rotors and the horizontal rotor through a wind resistance control algorithm by utilizing the attitude and heading of the unmanned aerial vehicle and the wind speed and direction information, and the high wind resistance function is achieved. The mooring cable control device realizes automatic winding and unwinding of the mooring cable. The structure is simple, self-adaptive work is achieved, and use is convenient.

    一种高抗风尾椎式系留无人机及其飞行控制方法,包括风速风向传感器、系留线缆、多旋翼机构、尾部推进旋翼、飞行控制系统和系留线缆控制装置。风速风向传感器固定在安装支架上,测量无人机所在位置的风向和风速,为飞行控制系统提供风阻信息。多旋翼机构由多个水平安装的旋翼组成,用于调节升力大小,控制无人机的姿态和位置。尾部推进旋翼由尾杆和一个垂直安装的旋翼组成,提供水平推力,用于抵抗水平方向的风阻。飞行控制系统利用无人机的姿态和航向,以及风速和风向信息,通过抗风控制算法调节多旋翼和水平旋翼的转速,实现高抗风功能。系留线缆控制装置实现系留线缆自动收放。结构简单,自适应工作,使用便捷。


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    Titel :

    High-wind-resistance tail cone type mooring unmanned aerial vehicle and flight control method thereof


    Weitere Titelangaben:

    高抗风尾椎式系留无人机及其飞行控制方法


    Beteiligte:
    WANG CHUNLONG (Autor:in) / YANG LIBO (Autor:in) / ZHENG KUN (Autor:in) / SHI LIHUI (Autor:in) / MA CHUANYAN (Autor:in) / HAO BOYA (Autor:in) / LI ZHENWEI (Autor:in) / WANG CHANGQING (Autor:in) / XING XIAOBO (Autor:in) / REN XUEFENG (Autor:in)

    Erscheinungsdatum :

    2020-07-17


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen



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