According to the flight characteristics of canard layout Unmanned Aerial Vehicle (UAV), this paper presents a variable distance coupled canard wing vertical takeoff and landing aircraft (VDCCW-VTOL) layout design scheme. The feasibility of this configuration of aircraft in actual flight was verified through analysis of its structural layout and flight control rate design.


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    Title :

    Design of Vertical Takeoff and Landing Aircraft with Variable Distance Coupling Canard Wing


    Additional title:

    Lect. Notes Electrical Eng.


    Contributors:
    Liu, Lianqing (editor) / Niu, Yifeng (editor) / Fu, Wenxing (editor) / Qu, Yi (editor) / Liu, Yong (author) / Sun, Li (author) / Liu, ZhiChao (author) / Zhao, DongYang (author) / Wen, ShaoLun (author) / Chen, Fei (author)

    Conference:

    International Conference on Autonomous Unmanned Systems ; 2024 ; Shenyang, China September 19, 2024 - September 21, 2024



    Publication date :

    2025-03-31


    Size :

    6 pages





    Type of media :

    Article/Chapter (Book)


    Type of material :

    Electronic Resource


    Language :

    English




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