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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...
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| Main Authors: | , , , |
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| Formato: | Artigo |
| Idioma: | Inglês |
| Publicado em: |
Hindawi Limited
2016-01-01
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| Colecção: | Mathematical Problems in Engineering |
| Acesso em linha: | http://dx.doi.org/10.1155/2016/2141482 |
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