Structural Optimization Design of Solar UAV

Abstract

According to the current status of solar energy the development of unmanned aerial vehicle (uav), the difficulties, the development of solar uav based on solar energy new materials research and application of the unmanned aerial vehicle (uav) structure scheme of structure optimization, optimization model is established, research and development to make a fixed wing flight available solar powered platform. This paper will analyze the overall scheme design of the system, the performance of the wing of the solar uav, the structure design and test results of the solar uav. Is obtained by the experimental data and theoretical data analysis, as the change of structure, the resistance of the aircraft fuselage become smaller, at the same time, the grid carbon rod piece structure also makes the body has the very high intensity, so in this paper, the design platform for the big wings flying wing structure and body strength fully meet the design requirements.