Studying Unmanned Aerial Vehicles (Uav) Two Tailed Fixed Wing Type for Flight Training Missions

Abstract

           The purpose of this investigation is to investigate, design, and construct a twin-tailed fixed-wing unmanned aerial vehicle for flight training missions. Our investigation revealed that the unmanned aerial vehicle is a two-tailed, fixed-wing, propeller-powered aircraft with an ideal aspect ratio (AR) of around 6.7, a wingspan of one meter, a wing chord of 0.15 m, and a total area of 0.15 m². The air pan has a concave top with a peak elevation of 0.021 m and a flat bottom. The fusiform fuselage, with dimensions of 0.07 m in width, 0.35 m in length, and 0.13 m in height, is appropriate for aerodynamics due to its strength and light weight. The size of an aircraft's tail wing design is 0.0138 m², or 9.20% of the overall wing area. The combined area of the raised and level rudders is 0.0480 m², or 32% of the overall wing area. and 37.50% of the rudder area, or 0.0180 m², is made up of the elevated rudder. The constructed twin-tailed fixed-wing unmanned aerial vehicle's take-off distance is around 5 meters, according to testing the necessary flight mission. The aircraft is very maneuverable and climbs ascent with great efficiency. It flies directly ahead. Simple to turn in circles using for testing purposes, raise the speed by about half of the maximum speed. The aircraft features excellent mobility, strong lift power, steady flight, decent balance, and no wobbling. The glide rate is excellent for both climbing and downhill high maneuverability and the landing distance is around ten meters. The findings of aircraft studies are simply produced. Simple controls for flying excellent flexibility and flying stability can accelerate at around 40 km/hr. It is a method of producing unmanned aerial vehicles for flying training flights at a low cost. Provide educational resources about weather for the general public and students.