1. General optimal design of solar-powered unmanned aerial vehicle for priority considering propulsion system
- Author
-
Kaijun Sun, Feng Li, and Xinhua Li
- Subjects
Battery (electricity) ,Optimal design ,0209 industrial biotechnology ,Aspect ratio ,Computer science ,Aerospace Engineering ,Route analysis ,ComputerApplications_COMPUTERSINOTHERSYSTEMS ,02 engineering and technology ,Propulsion ,Electricity demand ,01 natural sciences ,Automotive engineering ,Energy storage ,010305 fluids & plasmas ,020901 industrial engineering & automation ,0103 physical sciences ,Motion planning ,Aircraft design optimization ,Motor vehicles. Aeronautics. Astronautics ,Mechanical Engineering ,TL1-4050 ,Unmanned aerial vehicle ,Solar-powered ,General design technology ,Solar powered - Abstract
This paper describes the general optimization design method of Solar-Powered Unmanned Aerial Vehicle which priority considering propulsion system planning. Based on the traditional solar powered aircraft design method, the propulsion system top-level target parameters which affect the path planning are integrated into the general optimization design. According to the typical mission requirements of Solar-Powered Unmanned Aerial Vehicle, considering the design variables such as wing area, aspect ratio, design mission date and so on, the general optimization is carried out with the minimum aircraft weight as the optimization objective. The influence of wing area and aspect ratio on the optimal design results is analyzed and compared with the traditional design method. The results show that the general design method of Solar-Powered Unmanned Aerial Vehicle for priority considering propulsion system can greatly reduce the electricity demand of energy storage battery, greatly reduce the aircraft weight of Solar-Powered Unmanned Aerial Vehicle.
- Published
- 2020