Redesign, analysis, fabrication and testing of light weight fuselage, boom and empennage for solar UAV : Part 3 by Tan, Thomas Peng Ngee

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Solar UAV : design, fabrication and testing of a test wing section and integration with solar cells by Pang, Yida.

“…Minimum drag is achieved through a long and narrow fuselage section and long and thin wings. With such an aircraft design, the aircraft is able to have efficient climbing rates and can glide long distances at a high speed with a minimum loss of height in between. …”
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Design and development of solar powered glider - part b by Cheong, Wen Rong

“…In additional, in-flight telemetry and various sensors are to be integrated into the UAV fuselage and wired into the electrical system to provide live data for optimal flight and data to be analysed to better evaluate solar panel efficiency and power consumption during the various phases of flight.…”
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