Design and Simulation of Eight-Rotor Unmanned Aerial Vehicle Based on Hybrid Control System
In order to control the position and attitude of unmanned aerial vehicle (UAV) better in different environments, this study proposed a hybrid control system with backstepping and PID method for eight-rotor UAV in different flight conditions and designed a switching method based on altitude and attit...
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| Main Authors: | , , |
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| Format: | Article |
| Language: | English |
| Published: |
Wiley
2018-01-01
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| Series: | International Journal of Aerospace Engineering |
| Online Access: | http://dx.doi.org/10.1155/2018/5306125 |
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| _version_ | 1832548705628061696 |
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| author | Xueqiang Shen Jiwei Fan Haiqing Wang |
| author_facet | Xueqiang Shen Jiwei Fan Haiqing Wang |
| author_sort | Xueqiang Shen |
| collection | DOAJ |
| description | In order to control the position and attitude of unmanned aerial vehicle (UAV) better in different environments, this study proposed a hybrid control system with backstepping and PID method for eight-rotor UAV in different flight conditions and designed a switching method based on altitude and attitude angle of UAV. The switched process of hybrid controller while UAV taking off, landing, and disturbance under the gust is verified in MATLAB/Simulink. A set of appropriate controllers always matches to the flight of UAV in different circumstances, which can speed up the system response and reduce the steady-state error to improve stability. The simulation results show that the hybrid control system can suppress the drift efficiently under gusts, enhance the dynamic performance and stability of the system, and meet the position and attitude of flight control requirements. |
| format | Article |
| id | doaj-art-d7db584a3d5642bdbeb5293bd4f3dce6 |
| institution | Kabale University |
| issn | 1687-5966 1687-5974 |
| language | English |
| publishDate | 2018-01-01 |
| publisher | Wiley |
| record_format | Article |
| series | International Journal of Aerospace Engineering |
| spelling | doaj-art-d7db584a3d5642bdbeb5293bd4f3dce62025-02-03T06:13:27ZengWileyInternational Journal of Aerospace Engineering1687-59661687-59742018-01-01201810.1155/2018/53061255306125Design and Simulation of Eight-Rotor Unmanned Aerial Vehicle Based on Hybrid Control SystemXueqiang Shen0Jiwei Fan1Haiqing Wang2Northeast Electric Power University, Jilin 132000, ChinaNortheast Electric Power University, Jilin 132000, ChinaNortheast Electric Power University, Jilin 132000, ChinaIn order to control the position and attitude of unmanned aerial vehicle (UAV) better in different environments, this study proposed a hybrid control system with backstepping and PID method for eight-rotor UAV in different flight conditions and designed a switching method based on altitude and attitude angle of UAV. The switched process of hybrid controller while UAV taking off, landing, and disturbance under the gust is verified in MATLAB/Simulink. A set of appropriate controllers always matches to the flight of UAV in different circumstances, which can speed up the system response and reduce the steady-state error to improve stability. The simulation results show that the hybrid control system can suppress the drift efficiently under gusts, enhance the dynamic performance and stability of the system, and meet the position and attitude of flight control requirements.http://dx.doi.org/10.1155/2018/5306125 |
| spellingShingle | Xueqiang Shen Jiwei Fan Haiqing Wang Design and Simulation of Eight-Rotor Unmanned Aerial Vehicle Based on Hybrid Control System International Journal of Aerospace Engineering |
| title | Design and Simulation of Eight-Rotor Unmanned Aerial Vehicle Based on Hybrid Control System |
| title_full | Design and Simulation of Eight-Rotor Unmanned Aerial Vehicle Based on Hybrid Control System |
| title_fullStr | Design and Simulation of Eight-Rotor Unmanned Aerial Vehicle Based on Hybrid Control System |
| title_full_unstemmed | Design and Simulation of Eight-Rotor Unmanned Aerial Vehicle Based on Hybrid Control System |
| title_short | Design and Simulation of Eight-Rotor Unmanned Aerial Vehicle Based on Hybrid Control System |
| title_sort | design and simulation of eight rotor unmanned aerial vehicle based on hybrid control system |
| url | http://dx.doi.org/10.1155/2018/5306125 |
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