Reconfiguration Control Design of UAV against Actuator Faults Based on Control Allocation Method
The paper concentrates on the problem of fault-tolerant control of UAV against actuator faults from the perspective of flight control system architecture. Using backstepping control method and inverse optimization theory, the design of backstepping optimal control law was constructed. Based on the f...
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| Main Authors: | , , , |
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| Format: | Article |
| Language: | English |
| Published: |
Wiley
2022-01-01
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| Series: | International Journal of Aerospace Engineering |
| Online Access: | http://dx.doi.org/10.1155/2022/4481553 |
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| _version_ | 1849686893798621184 |
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| author | Yuwei Cui Aijun Li Biao Duan Shabbir Wasif |
| author_facet | Yuwei Cui Aijun Li Biao Duan Shabbir Wasif |
| author_sort | Yuwei Cui |
| collection | DOAJ |
| description | The paper concentrates on the problem of fault-tolerant control of UAV against actuator faults from the perspective of flight control system architecture. Using backstepping control method and inverse optimization theory, the design of backstepping optimal control law was constructed. Based on the fault monitoring mechanism of vehicle management computer in the distributed flight control and control allocation system, a fault-tolerant control design method was established in the case of multiple failure modes of the actuators, which compensates the influence caused by the failures. Finally, the effectiveness of the proposed strategy was verified by numerical simulation. |
| format | Article |
| id | doaj-art-00aeeda8b0024b6eb247f0b27a27ec01 |
| institution | DOAJ |
| issn | 1687-5974 |
| language | English |
| publishDate | 2022-01-01 |
| publisher | Wiley |
| record_format | Article |
| series | International Journal of Aerospace Engineering |
| spelling | doaj-art-00aeeda8b0024b6eb247f0b27a27ec012025-08-20T03:22:31ZengWileyInternational Journal of Aerospace Engineering1687-59742022-01-01202210.1155/2022/4481553Reconfiguration Control Design of UAV against Actuator Faults Based on Control Allocation MethodYuwei Cui0Aijun Li1Biao Duan2Shabbir Wasif3School of AutomationSchool of AutomationSchool of AutomationSchool of AutomationThe paper concentrates on the problem of fault-tolerant control of UAV against actuator faults from the perspective of flight control system architecture. Using backstepping control method and inverse optimization theory, the design of backstepping optimal control law was constructed. Based on the fault monitoring mechanism of vehicle management computer in the distributed flight control and control allocation system, a fault-tolerant control design method was established in the case of multiple failure modes of the actuators, which compensates the influence caused by the failures. Finally, the effectiveness of the proposed strategy was verified by numerical simulation.http://dx.doi.org/10.1155/2022/4481553 |
| spellingShingle | Yuwei Cui Aijun Li Biao Duan Shabbir Wasif Reconfiguration Control Design of UAV against Actuator Faults Based on Control Allocation Method International Journal of Aerospace Engineering |
| title | Reconfiguration Control Design of UAV against Actuator Faults Based on Control Allocation Method |
| title_full | Reconfiguration Control Design of UAV against Actuator Faults Based on Control Allocation Method |
| title_fullStr | Reconfiguration Control Design of UAV against Actuator Faults Based on Control Allocation Method |
| title_full_unstemmed | Reconfiguration Control Design of UAV against Actuator Faults Based on Control Allocation Method |
| title_short | Reconfiguration Control Design of UAV against Actuator Faults Based on Control Allocation Method |
| title_sort | reconfiguration control design of uav against actuator faults based on control allocation method |
| url | http://dx.doi.org/10.1155/2022/4481553 |
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