The invention discloses a method for controlling the hovering of an aircraft around airflow and the aircraft, and the method comprises the following steps: S1, obtaining the rising acceleration of the aircraft; s2, judging whether a cyclone capable of allowing the aircraft to fly around exists or not according to the rising acceleration of the aircraft; s3, obtaining the state of the aileron of the aircraft; s4, adjusting the course according to the state of the aileron; and S5, the circling radius is adjusted. According to the invention, the cruising ability of the fixed wing or flapping wing type unmanned aerial vehicle can be improved by utilizing the energy of the upflow in the cyclone.

    本发明公开了一种飞行器绕气流盘旋控制的方法及飞行器,其中,该方法包括以下步骤,S1,获取飞行器上升加速度;S2,根据飞行器上升加速度判断是否存在能够供飞行器绕飞的气旋;S3,获取飞行器的副翼的状态;S4,根据副翼的状态调整航向;S5,调节盘旋半径。本发明能够利用气旋中上升气流的能量来提高固定翼或扑翼式无人机的续航能力。


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    Titel :

    Aircraft circling control method around airflow and aircraft


    Weitere Titelangaben:

    一种飞行器绕气流盘旋控制的方法及飞行器


    Beteiligte:
    ZHAO LONGFEI (Autor:in) / WANG XIAORAN (Autor:in) / MAO RUIYANG (Autor:in) / LI HAO (Autor:in) / JIAO ZONGXIA (Autor:in) / TIAN TAO (Autor:in)

    Erscheinungsdatum :

    2023-11-17


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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