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.
Design of Vertical Takeoff and Landing Aircraft with Variable Distance Coupling Canard Wing
Lect. Notes Electrical Eng.
International Conference on Autonomous Unmanned Systems ; 2024 ; Shenyang, China September 19, 2024 - September 21, 2024
Proceedings of 4th 2024 International Conference on Autonomous Unmanned Systems (4th ICAUS 2024) ; Kapitel : 35 ; 341-346
31.03.2025
6 pages
Aufsatz/Kapitel (Buch)
Elektronische Ressource
Englisch
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