Solar-powered unmanned aerial vehicles

• Main Authors: Reinhardt, K.C., Lamp, T.R., Geis, J.W., Colozza, A.J.
• Format: Conference Proceeding
• Language: English
• Subjects: Aerospace electronics; Energy storage; Fuel cells; Military aircraft; Performance analysis; Photovoltaic systems; Power electronics; Power system analysis computing; Solar power generation; Unmanned aerial vehicles
• ISSN: 1089-3547
• DOI: 10.1109/IECEC.1996.552842

An analysis was performed to determine the impact of various power system components and mission requirements on the size of solar-powered high altitude long endurance (HALE)-type aircraft. The HALE unmanned aerial vehicle (UAV) has good potential for use in many military and civil applications. The primary power system components considered in this study were photovoltaic (PV) modules for power generation and regenerative fuel cells for energy storage. The impact of relevant component performance on UAV size and capability were considered; including PV module efficiency and mass, power electronics efficiency, and fuel cell specific energy. Mission parameters such as time of year, flight altitude, flight latitude and payload mass and power were also varied to determine impact on UAV size. The aircraft analysis method used determines the required aircraft wing aspect ratio, wing area and total mass based on maximum endurance or minimum required power calculations. The results indicate that the capacity of the energy storage system employed, fuel cells in this analysis, greatly impacts aircraft size, whereas the impact of PV module efficiency and mass is much less important. It was concluded that an energy storage specific energy (total system) of 250-500 Whr/kg is required to enable most useful missions, and that PV cells with efficiencies greater than /spl sim/12% are suitable for use.