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Flight Tests of Autopilot Integrated with Fault-Tolerant Control of a Small Fixed-Wing UAV
A fault-tolerant control scheme for the autopilot of the small fixed-wing UAV is designed and tested by the actual flight experiments. The small fixed-wing UAV called Xiang Fei is developed independently by Nanjing University of Aeronautics and Astronautics. The flight control system is designed bas...
Kaydedildi:
| Asıl Yazarlar: | , , , |
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| Materyal Türü: | Artigo |
| Dil: | Inglês |
| Baskı/Yayın Bilgisi: |
Hindawi Limited
2016-01-01
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| Seri Bilgileri: | Mathematical Problems in Engineering |
| Online Erişim: | http://dx.doi.org/10.1155/2016/2141482 |
| Etiketler: |
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