The invention provides an unmanned aerial vehicle load electrical connection interface system, and relates to the technical field of unmanned aerial vehicle system integration, unmanned aerial vehiclemeasurement and control software design and the like. The electric connector comprises an electric connector end A and an electric connector end B which are connected with each other, the electric connector end A is connected with the airborne power supply module through the power supply interface module; the electric connector end A is connected with the flight control module through the serialport communication module; the electric connector end A is connected with the data link machine-mounted end module through the network port communication module; and the electric connector end B is connected with a plurality of loads. Data communication between the load equipment and ground station software can be realized, flexible integration of the unmanned aerial vehicle ground station software and the load equipment is realized, and developers can realize load integration under the condition of not changing the existing system of the unmanned aerial vehicle.

    本发明提供一种无人机载荷电气连接接口系统,涉及无人机系统集成、无人机测控软件设计等技术领域。本发明包括相互连接的电连接器端A、电连接器端B,所述电连接器端A通过电源接口模块与机载供电模块连接,所述电连接器端A通过串口通信模块与飞控模块连接,所述电连接器端A通过网口通信模块与数据链机载端模块连接,所述电连接器端B连接若干载荷,本发明可实现载荷设备与地面站软件的数据通信,实现了无人机地面站软件与载荷设备的灵活集成,开发人员可以在不改动无人机现有系统的情况下实现载荷集成。


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    Titel :

    Unmanned aerial vehicle load electrical connection interface system


    Weitere Titelangaben:

    一种无人机载荷电气连接接口系统


    Beteiligte:
    SHAO YI (Autor:in)

    Erscheinungsdatum :

    23.06.2020


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    H04L TRANSMISSION OF DIGITAL INFORMATION, e.g. TELEGRAPHIC COMMUNICATION , Übertragung digitaler Information, z.B. Telegrafieverkehr / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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