Mini UAV Design and Manufacture with Bungee Launched / Parachute Recovery

Lih Shyng Shyu; Yung Chia Hsiao

doi:10.4028/www.scientific.net/AMM.610.97

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HomeApplied Mechanics and MaterialsApplied Mechanics and Materials Vol. 610Mini UAV Design and Manufacture with Bungee...

Mini UAV Design and Manufacture with Bungee Launched / Parachute Recovery

Abstract:

In the past ten years, the R&D of UAV (Unmanned Aerial Vehicle) is very popular and has the trend to replacing with the manned aerial vehicle due to its low-cost and high-mobility. According to the specifications, this project completes special contour and function of a mini-UAV design and passes the strict fabrication, prototyping, and aerial test processes. With the advantages of long flight endurance, speedy assembly/disassembly, simply contour, and portable, the developed mini-UAV has the capabilities of bungee launch and parachute recovery. Thus, it makes much progress in Taiwan’s mini-UAV area.

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Periodical:

Applied Mechanics and Materials (Volume 610)

Pages:

97-100

DOI:

https://doi.org/10.4028/www.scientific.net/AMM.610.97

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Online since:

August 2014

Authors:

Lih Shyng Shyu*, Yung Chia Hsiao

Keywords:

Bungee Launched, Mini-UAV, Parachute Recovery

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* - Corresponding Author

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