2022   02   az   p.21-25 Namiq Haydarov2,3, Ramin Sattarov2,3, Ibrahim Nuriyev1,2, Maqsud Nazarov1,3,
General analysis and selection of a fixed-wing UAV model		  pdf 

ABSTRACT

Recently, unmanned aerial vehicles (UAVs) have been widely used for both military and civilian purposes. The most relevant is the use of UAVs used for military purposes in mountainous and unfavorable terrain, optimization of landing and takeoff distances. When designing and selecting a UAV, many parameters must be taken into account in order to achieve short landing and takeoff distances. Appropriate model components should be selected to be suitable for this distance, for greater payload capacity, with a small drag coefficient at high speeds, while maintaining proper airflow. Taking into account the above requirements, the My Twin Dream model (1800 mm) was chosen. The goal is to test the scheme of the stabilization system developed by us and the software on this model. The selected model was tested unloaded using the engine, propeller and battery provided by the manufacturer. Test flights were carried out manually. As a result, the flight was carried out successfully without the use of an accelerometer, gyroscope, GPS and other stabilization devices. Turnaround, takeoff and landing maneuvers were also practiced.

Keywords: Unmanned aerial vehicle; UAV, Drone, fixed-wing aircraft; wing profile; NASA 0010; airfoil; Reynolds number.
PACS: 47.85.Gj

DOI:-

Received: 18.05.2022

AUTHORS & AFFILIATIONS

1. Institute of Radiation Problems of ANAS
2. ANAS High Technology Park, Science and Technology Park
3. ANAS Management Systems Institute
E-mail: nmq.heydarov91@gmail.com 		REFERENCIES

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