Design and Development of 75 mm Fixed-Wing Nano Air Vehicle
This thesis deals with the design and development of a 75 mm fixed-wing nano-air vehicle (NAV). The NAV is designed to fit inside a cube with each side measuring 75 mm. The range and endurance of the NAV are 300 m and 2-3 minutes, respectively. The high-wing horizontal tailless NAV has a take-off we...
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| Language: | en_US |
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2018
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| Online Access: | http://etd.iisc.ernet.in/2005/3689 http://etd.iisc.ernet.in/abstracts/4559/G28507-Abs.pdf |