Systems and methods for controlling a hybrid aerial vehicle. The flight control unit controls an internal combustion engine for driving the lift rotor by providing a lift control command and provides a steering control command for a motor for driving the steering control rotor as required to manipulate the air vehicle. In this way, the vehicle is manipulated in synchronization with a motor-driven steering control rotor device for controlling torque force and a separate fuel-driven lift control device for controlling linear force.

    用于对混合动力式空中运载工具进行控制的系统和方法。飞行控制单元通过提供升力控制指令来对驱动升力旋翼的内燃机进行控制并且根据需要向驱动转向控制旋翼的电动机提供转向控制指令来对空中运载工具进行操纵,从而使用于对扭矩力进行控制的电动机驱动的转向控制旋翼装置和用于对线性力进行控制的单独的燃料驱动的升力控制装置同步来对该运载工具进行操纵。


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    Title :

    SYSTEM AND METHOD FOR CONTROLLING A HYBRID MULTI-ROTOR AERIAL VEHICLE


    Additional title:

    用于对混合动力式多旋翼空中运载工具进行控制的系统和方法


    Contributors:
    SAYAG ELI (author) / SVIRSKY ALON (author)

    Publication date :

    2024-11-26


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64C AEROPLANES , Flugzeuge / B64U



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