Miniaturization and mechanical simplification of aerial vehicles is always a difficult problem for micro aerial vehicles (MAVs). In this paper, we present the mechanical design, control design, system integration, and experiments of a novel electronic swashplate tandem helicopter. The sufficient lift and control torque required by the tandem helicopter can be provided by the electronic swashplate. The roll angle and pitch angle of the tandem helicopter can be controlled stably, but the yaw angle is not ideal when the helicopter flies independently. The electronic swashplate driven by a brushless motor is a promising MAV solution, which can be used as a strategy for aircraft miniaturization.


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    Title :

    Design and Experimental Validation of a Tandem Helicopter Based on Electronic Swashplate


    Additional title:

    Lect. Notes Electrical Eng.


    Contributors:
    Wu, Meiping (editor) / Niu, Yifeng (editor) / Gu, Mancang (editor) / Cheng, Jin (editor) / Ye, Weijie (author) / Zhang, Weiping (author) / Wu, Chaofeng (author)

    Conference:

    International Conference on Autonomous Unmanned Systems ; 2021 ; Changsha, China September 24, 2021 - September 26, 2021



    Publication date :

    2022-03-18


    Size :

    10 pages





    Type of media :

    Article/Chapter (Book)


    Type of material :

    Electronic Resource


    Language :

    English




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