Single Rotor Mini Reconnaissance Aircraft Design

[摘要] The micro rotor aircraft has the advantages of small noise, good concealment and so on, which make it has wide application potential in both military and civilian applications. Aiming at the problems of public security organs such as counter-terrorism, anti-drugs, and disaster relief, a single-rotor wing micro-reconnaissance aircraft was designed. In this paper, the structure of the aircraft is analyzed and designed. Secondly, the aerodynamic characteristics and adsorption capacity of the aircraft are analyzed. Finally, the work flow of the UAV is introduced. The UAV can achieve multi-directional flight, vertical take-off and landing and hovering, and has good prospects for investigation and surveillance.

[发布机构] College of Transportation, Shandong University of Science and Technology, Qingdao; 266590, China^1;College of Electronic Communication and Physics, Shandong University of Science and Technology, Qingdao; 266590, China^2

[效力级别] 无线电电子学 [学科分类] 材料科学（综合）

[关键词] Adsorption capacities;Aerodynamic characteristics;Counter terrorism;Disaster relief;Micro rotors;Public security;Rotor wings;Vertical take-off and landings