Non-linear mathematical model of a quad-tiltrotor UAV spatial motion
The article presents a design scheme of a quad-tiltrotor unmanned aerial vehicle (UAV), which combines a safe vertical take-off and landing procedures and a relatively large flight range inherent in the aircraft. In order to reduce the cost and weight of the quad-tiltrotor UAV, to increase its relia...
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| Hlavní autoři: | , |
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| Médium: | Статья |
| Jazyk: | English |
| Vydáno: |
Institute of Physics Publishing
2020
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| On-line přístup: | https://dspace.ncfu.ru/handle/20.500.12258/13760 |
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