Аннотация
The use of radio-controlled unmanned aerial vehicles is widespread in the world. The article presents the development in computer programs of models of a hybrid unmanned aerial vehicle in SolidWorks environment. The developments were carried out in cooperation with senior students in the process of training. We consider a hybrid propulsion system that will expand the scope of the unmanned aerial vehicle (UAV). To create a 3D model of a hybrid unmanned aerial vehicle (UAV) - aerodynamic calculations of the aircraft were performed. In the SolidWorks computer environment, test plots of the parameters listed below were obtained and the geometric topology of the hybrid unmanned aerial vehicle was optimized. 3D models of the hybrid unmanned aerial vehicle were developed on the CAD channel.