Provided are a control device for unmanned aerial vehicle and an unmanned aerial vehicle. The control device for unmanned aerial vehicle includes a shell, an inertial measurement device fixed in the shell, a main flight control circuit board electrically connected to the inertial measurement device, and a flexible interface board electrically connected to the main flight control circuit board and appressed against the inwall of the shell. At least one external device is connected to two opposite sides of the flexible interface board through the shell.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Control device for unmanned aerial vehicle and unmanned aerial vehicle


    Beteiligte:
    YIN LIANGLIANG (Autor:in) / GAO LIANJIE (Autor:in) / LI SHAOBIN (Autor:in) / ZHANG YU (Autor:in)

    Erscheinungsdatum :

    2021-06-08


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    H05K PRINTED CIRCUITS , Gedruckte Schaltungen / B64C AEROPLANES , Flugzeuge