RETRACTED: A flight control method for unmanned aerial vehicles based on vibration suppression
Abstract The development of unmanned aerial vehicle (UAVs) has gained importance in recent years for various applications like photography, inspection of infrastructure and various agricultural applications. Various researchers have carried out numerous attempts at optimisation control of UAVs and t...
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| Format: | Article |
| Language: | English |
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Wiley
2021-09-01
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| Series: | IET Collaborative Intelligent Manufacturing |
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| Online Access: | https://doi.org/10.1049/cim2.12027 |
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| _version_ | 1850145850980827136 |
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| author | Xinhua Wang Xiulin Zhang Huajun Gong Ju Jiang Hari Mohan Rai |
| author_facet | Xinhua Wang Xiulin Zhang Huajun Gong Ju Jiang Hari Mohan Rai |
| author_sort | Xinhua Wang |
| collection | DOAJ |
| description | Abstract The development of unmanned aerial vehicle (UAVs) has gained importance in recent years for various applications like photography, inspection of infrastructure and various agricultural applications. Various researchers have carried out numerous attempts at optimisation control of UAVs and their flight range maximisation. However, a few attempts have addressed structural deformation effects on the reliability and safety of UAVs. In order to study the effect of structural deformation on the reliability and safety of UAVs under normal flight conditions, a certain type of UAV as a research object is discussed and the augmented tracking model based on the original object system by using the Lyapunov function is built up. The performance is observed in terms of rise time and overshoot and it is observed from the simulation outcomes that the system is stable at all design points in the range of 0–9000 m, providing a rise time of 10 s and zero overshoot. From this study, it is revealed that the designed controller can effectively suppress the vibration of the flexible mode while ensuring the stability and tracking performance of the UAV. |
| format | Article |
| id | doaj-art-fe8ad1e4486a41be84d197ca75160a33 |
| institution | OA Journals |
| issn | 2516-8398 |
| language | English |
| publishDate | 2021-09-01 |
| publisher | Wiley |
| record_format | Article |
| series | IET Collaborative Intelligent Manufacturing |
| spelling | doaj-art-fe8ad1e4486a41be84d197ca75160a332025-08-20T02:28:00ZengWileyIET Collaborative Intelligent Manufacturing2516-83982021-09-013325226110.1049/cim2.12027RETRACTED: A flight control method for unmanned aerial vehicles based on vibration suppressionXinhua Wang0Xiulin Zhang1Huajun Gong2Ju Jiang3Hari Mohan Rai4College of Automation Engineering Nanjing University of Aeronautics and Astronautics Nanjing ChinaCollege of Automation Engineering Nanjing University of Aeronautics and Astronautics Nanjing ChinaCollege of Automation Engineering Nanjing University of Aeronautics and Astronautics Nanjing ChinaCollege of Automation Engineering Nanjing University of Aeronautics and Astronautics Nanjing ChinaDepartment of Electronics and Communication Engineering Krishna Engineering College Ghaziabad IndiaAbstract The development of unmanned aerial vehicle (UAVs) has gained importance in recent years for various applications like photography, inspection of infrastructure and various agricultural applications. Various researchers have carried out numerous attempts at optimisation control of UAVs and their flight range maximisation. However, a few attempts have addressed structural deformation effects on the reliability and safety of UAVs. In order to study the effect of structural deformation on the reliability and safety of UAVs under normal flight conditions, a certain type of UAV as a research object is discussed and the augmented tracking model based on the original object system by using the Lyapunov function is built up. The performance is observed in terms of rise time and overshoot and it is observed from the simulation outcomes that the system is stable at all design points in the range of 0–9000 m, providing a rise time of 10 s and zero overshoot. From this study, it is revealed that the designed controller can effectively suppress the vibration of the flexible mode while ensuring the stability and tracking performance of the UAV.https://doi.org/10.1049/cim2.12027vehicle dynamicsaircraft controlcontrol system synthesisoptimisationremotely operated vehiclesautonomous aerial vehicles |
| spellingShingle | Xinhua Wang Xiulin Zhang Huajun Gong Ju Jiang Hari Mohan Rai RETRACTED: A flight control method for unmanned aerial vehicles based on vibration suppression IET Collaborative Intelligent Manufacturing vehicle dynamics aircraft control control system synthesis optimisation remotely operated vehicles autonomous aerial vehicles |
| title | RETRACTED: A flight control method for unmanned aerial vehicles based on vibration suppression |
| title_full | RETRACTED: A flight control method for unmanned aerial vehicles based on vibration suppression |
| title_fullStr | RETRACTED: A flight control method for unmanned aerial vehicles based on vibration suppression |
| title_full_unstemmed | RETRACTED: A flight control method for unmanned aerial vehicles based on vibration suppression |
| title_short | RETRACTED: A flight control method for unmanned aerial vehicles based on vibration suppression |
| title_sort | retracted a flight control method for unmanned aerial vehicles based on vibration suppression |
| topic | vehicle dynamics aircraft control control system synthesis optimisation remotely operated vehicles autonomous aerial vehicles |
| url | https://doi.org/10.1049/cim2.12027 |
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