The invention provides a tailstock type vertical take-off and landing unmanned aerial vehicle control system, and the system comprises a main control system, a propelling system, a rudder system and afeedback system; the rudder system comprises a steering engine, and the steering engine is mainly composed of rudder pieces, a corresponding rudder piece driving motor, a rudder piece driving transmission mechanism and a rudder piece driving control circuit. The rudder pieces comprise a gas rudder piece arranged at an engine spray pipe and an air rudder piece arranged on the side of an engine; anair rudder piece rotating shaft is arranged on a wing of the unmanned aerial vehicle, the rudder piece driving transmission mechanism comprises a long control rod movably connected with the engine, and the two ends of the long control rod are connected with the gas rudder piece and the air rudder piece respectively, which are used for the linkage of the gas rudder sheet and the air rudder sheet.The control long rod is driven by the rudder sheet driving motor, and the gas rudder sheet and the air rudder sheet can be driven by the control long rod, so that the rudder system has enough controlcapability.

    本申请提供了一种尾座式垂直起降无人飞行器的控制系统,包括主控系统、推进系统、舵系统、反馈系统,舵系统包含舵机,上述舵机主要由舵片和相应的舵片驱动电机、舵片驱动传动机构和舵片驱动控制电路所组成。舵片包括设置于发动机喷管处的燃气舵片和布置于发动机侧方的空气舵片,空气舵片转轴设置于无人飞行器的机翼上,舵片驱动传动机构包含与发动机活动连接的控制长杆,控制长杆两端分别连接燃气舵片和空气舵片,用于将燃气舵片和空气舵片联动。通过一个舵片驱动电机驱动控制长杆,控制长杆就可带动燃气舵片和空气舵片,使本舵系统就具有足够的操纵能力。


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    Title :

    Control system of tailstock type vertical take-off and landing unmanned aerial vehicle


    Additional title:

    一种尾座式垂直起降无人飞行器的控制系统


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

    Publication date :

    2021-02-05


    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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