The invention relates to a control system of an unmanned aerial vehicle, in particular to a control system of an unmanned aerial vehicle engine. The control system comprises a main control system, a propelling system, a rudder system and a feedback system; rudder sheets of the rudder system is driven to rotate by a rudder sheet driving motor through a driving transmission mechanism; the rotating shafts of the rudder sheets are arranged in a manner of being perpendicular to the central axis of the tail part of the engine of the unmanned aerial vehicle, and an included angle between any two adjacent rudder sheet rotating shafts is 90 degrees; each engine is provided with three rudder sheets, so that the layout of the rudder sheets of the two engines is symmetrical relative to the center linebetween the two engines. By the adoption of the control system of the unmanned aerial vehicle engine, on the premise that high flexibility is still achieved, compared with the mode that eight rudderpieces are arranged on double engines, the price is lower.

    本发明涉及无人飞行器的控制系统,尤其涉及一种无人飞行器发动机的控制系统,包括主控系统,推进系统,舵系统,反馈系统,舵系统的舵片由舵片驱动电机通过驱动传动机构带动舵片转动,所述舵片的旋转轴以垂直于无人飞行器发动机尾部中轴线的方式布置且任意相邻两个舵片旋转轴之间的夹角为90°;每个发动机上分别配置三个舵片,使两发动机的舵片的布局相对于两发动机之间的中线对称。采用本无人飞行器发动机的控制系统可依然在拥有较高的灵活性的前提下,同时相比于双发动机配置八个舵片而言,价格更加低廉。


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    Title :

    Control system of unmanned aerial vehicle engine


    Additional title:

    无人飞行器发动机的控制系统


    Contributors:
    TANG BING (author) / LIU YIJIAN (author)

    Publication date :

    2021-02-02


    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



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