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

  • 会议论文

  • 发表日期：

    2025年

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  • Yong Liu,
  • Li Sun,
  • ZhiChao Liu,
  • DongYang Zhao,
  • ShaoLun Wen,
  • Fei Chen,
  • Tong Wang,
  • Nian Ding,
  • Xing Li,
  • Ruijie Li

摘要

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.