The invention provides an avionics system of an oil-driven direct-driven multi-rotor unmanned aerial vehicle, which comprises a power supply management unit used for converting battery voltage into voltage required by a flight control unit and an engine control unit and correspondingly distributing the voltage; the engine control unit is used for controlling normal work of the two-stroke engine and sending the engine rotating speed numerical value, the engine temperature numerical value and the self-state data which are read in real time to the flight control unit. The ground control unit is used for transmitting the differential positioning information to the flight control unit in real time; the flight control unit is used for sending instructions to the engine control unit and the power management unit according to the engine rotating speed value, the engine temperature value, the self-state data and the differential positioning information which are acquired in real time to control the unmanned aerial vehicle to work. By means of the method, the problems that when multiple engines of an avionics system of an existing oil-driven multi-rotor unmanned aerial vehicle work cooperatively, the engine performance consistency is poor, and compared with a motor, the engine is long in response time, high in non-linear degree and the like can be solved.

    本发明提供的油动直驱多旋翼无人机航电系统,包括电源管理单元用于将电池电压变换为飞行控制单元、发动机控制单元所需电压,并进行相应分配;发动机控制单元用于控制两冲程发动机的正常工作,并将实时读取的发动机转速数值、发动机温度数值和自身状态数据发给飞行控制单元;地面控制单元用于将差分定位信息实时传输至飞行控制单元;飞行控制单元用于根据实时获取的发动机转速数值、发动机温度数值和自身状态数据、差分定位信息,向发动机控制单元、电源管理单元发出指令,控制无人机作业。利用本发明,能够解决目前油动多旋翼无人机航电系统的多台发动机协同作业时所面临的发动机性能一致性差、发动机较电机相比响应时间长、非线性程度高等问题。


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    Title :

    Oil-driven direct-driven multi-rotor unmanned aerial vehicle avionics system


    Additional title:

    油动直驱多旋翼无人机航电系统


    Contributors:
    CAI MAOLIN (author) / GUO XIANGQUN (author) / XIN HAODA (author) / MA GUOPENG (author) / YU MENG (author) / JIANG HAOKUN (author) / LI QUN (author) / CHANG JIAN (author) / YANG CHENGZHANG (author) / LIU FANBIN (author)

    Publication date :

    2023-11-03


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

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



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