Numerical study of the SSS frame structure of a quadcopter

In this paper, modeling and determination of the operability the original frame structure of quadcopter is carried out. The model consists of a frame, beams for installing propellers and four landing gear struts for fixing on the surface, the material is plastic. Numerical calculation of the stress-strain model of the original frame of quadcopter was carried out using the finite element method in the ANSYS software package for two spatial positions of the quadcopter - on the ground and in flight. The results allow us to draw conclusions on the emerging loads on the frame structure, the possibility of application in practice.