Rope-Hook Recovery Controller Designed for a Flying-Wing UAV
Due to the complexity of landing environments, precision guidance and high-precision control technology have become key to the rope-hook recovery of shipborne unmanned aerial vehicles (UAVs). The recovery process was divided into three stages and a reasonable guidance strategy had been designed for...
| Main Authors: | , , , |
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| Format: | Article |
| Language: | English |
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MDPI AG
2021-12-01
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| Series: | Aerospace |
| Subjects: | |
| Online Access: | https://www.mdpi.com/2226-4310/8/12/384 |
| _version_ | 1827674579248611328 |
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| author | Zhao Deng Fuqiang Bing Zhiming Guo Liaoni Wu |
| author_facet | Zhao Deng Fuqiang Bing Zhiming Guo Liaoni Wu |
| author_sort | Zhao Deng |
| collection | DOAJ |
| description | Due to the complexity of landing environments, precision guidance and high-precision control technology have become key to the rope-hook recovery of shipborne unmanned aerial vehicles (UAVs). The recovery process was divided into three stages and a reasonable guidance strategy had been designed for them, respectively. This study separated the guidance and control issues into an outer guidance loop and an inner control loop. The inner loop (attitude control loop) controled the UAV to follow the acceleration commands generated by the outer loop (trajectory tracking loop). The inner loop of the longitudinal controller and the lateral controller were designed based on active disturbance rejection control (ADRC), which has strong anti-interference ability. In the last phase, the outer loop of the longitudinal controller switched from a total energy control system (TECS), which greatly decoupled the altitude channel and speed channel, to the proportional navigation (PN) guidance law, while the outer loop of lateral controller switches from the proportional control law based on the L<sub>1</sub> guidance law, which can reduce the tracking error and deviation, to the PN guidance law, which considerably enhances the tracking precision. Finally, the simulation data and flight test data show that the controller has strong robustness and good tracking precision, which ensures safe rope-hook recovery. |
| first_indexed | 2024-03-10T04:41:23Z |
| format | Article |
| id | doaj.art-4ac9e838fff147e7a38fe7337fd47627 |
| institution | Directory Open Access Journal |
| issn | 2226-4310 |
| language | English |
| last_indexed | 2024-03-10T04:41:23Z |
| publishDate | 2021-12-01 |
| publisher | MDPI AG |
| record_format | Article |
| series | Aerospace |
| spelling | doaj.art-4ac9e838fff147e7a38fe7337fd476272023-11-23T03:18:13ZengMDPI AGAerospace2226-43102021-12-0181238410.3390/aerospace8120384Rope-Hook Recovery Controller Designed for a Flying-Wing UAVZhao Deng0Fuqiang Bing1Zhiming Guo2Liaoni Wu3School of Aerospace Engineering, Xiamen University, Xiamen 361000, ChinaSchool of Aerospace Engineering, Xiamen University, Xiamen 361000, ChinaSchool of Aerospace Engineering, Xiamen University, Xiamen 361000, ChinaSchool of Aerospace Engineering, Xiamen University, Xiamen 361000, ChinaDue to the complexity of landing environments, precision guidance and high-precision control technology have become key to the rope-hook recovery of shipborne unmanned aerial vehicles (UAVs). The recovery process was divided into three stages and a reasonable guidance strategy had been designed for them, respectively. This study separated the guidance and control issues into an outer guidance loop and an inner control loop. The inner loop (attitude control loop) controled the UAV to follow the acceleration commands generated by the outer loop (trajectory tracking loop). The inner loop of the longitudinal controller and the lateral controller were designed based on active disturbance rejection control (ADRC), which has strong anti-interference ability. In the last phase, the outer loop of the longitudinal controller switched from a total energy control system (TECS), which greatly decoupled the altitude channel and speed channel, to the proportional navigation (PN) guidance law, while the outer loop of lateral controller switches from the proportional control law based on the L<sub>1</sub> guidance law, which can reduce the tracking error and deviation, to the PN guidance law, which considerably enhances the tracking precision. Finally, the simulation data and flight test data show that the controller has strong robustness and good tracking precision, which ensures safe rope-hook recovery.https://www.mdpi.com/2226-4310/8/12/384rope-hook recoveryTECSADRCtrajectory trackingL1 guidanceproportional navigation |
| spellingShingle | Zhao Deng Fuqiang Bing Zhiming Guo Liaoni Wu Rope-Hook Recovery Controller Designed for a Flying-Wing UAV Aerospace rope-hook recovery TECS ADRC trajectory tracking L1 guidance proportional navigation |
| title | Rope-Hook Recovery Controller Designed for a Flying-Wing UAV |
| title_full | Rope-Hook Recovery Controller Designed for a Flying-Wing UAV |
| title_fullStr | Rope-Hook Recovery Controller Designed for a Flying-Wing UAV |
| title_full_unstemmed | Rope-Hook Recovery Controller Designed for a Flying-Wing UAV |
| title_short | Rope-Hook Recovery Controller Designed for a Flying-Wing UAV |
| title_sort | rope hook recovery controller designed for a flying wing uav |
| topic | rope-hook recovery TECS ADRC trajectory tracking L1 guidance proportional navigation |
| url | https://www.mdpi.com/2226-4310/8/12/384 |
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