Computer Simulation of a Convertor-Type UAV Planer Based on Applied Applications

Abstract

The paper shows how important it is when designing to take into account the features of the wing aerodynamics and solving the issues of regulating the stability of the aircraft. Further development of unmanned aviation to ensure long-term flight of unmanned aerial vehicles directly depends on the ratio of power and weight, power and overall dimensions of control systems (propulsion systems), aerodynamic features of the wing, as well as aerodynamic quality factors of the wing of the aircraft. The energy consumed during flight by an aircraft directly depends on the chosen wing shape. At the same time, in order to save the energy of the aircraft during flight, in order to quantitatively exceed the coefficient of lift created by the angle of attack of the wing from the coefficient of resistance, during the design period of the aircraft it is necessary to use mainly this wing design.