Abstract:

The use of unmanned aerial vehicles is increasing due to the cost and staff security required to fulfill the tasks of the aircraft being used in the civilian and military field. Many countries and scientific organizations are involved in the study of high altitude long endurance unmanned aerial vehicles, especially preferred for military purposes. In this study, geometric and detailed design phases of an unmanned aerial vehicle which had been conceptually designed before were examined, and what optimizations could be made according to the task expected by aerial and useful load were studied.

Keywords: