Path following control for powered parafoil system based on TD3-LADRC
The powered parafoil system is a distinctive flight vehicle that comprises a thrust device and an airdrop parafoil, affording significant advantages such as elevated load-bearing capacity and extended flight endurance. Nonetheless, the control of this system is intricate and nonlinear due to the com...
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| Vydáno v: | Chinese Control Conference s. 2364 - 2369 |
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| Hlavní autoři: | , , , , , |
| Médium: | Konferenční příspěvek |
| Jazyk: | angličtina |
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Technical Committee on Control Theory, Chinese Association of Automation
24.07.2023
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| ISSN: | 1934-1768 |
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| Abstract | The powered parafoil system is a distinctive flight vehicle that comprises a thrust device and an airdrop parafoil, affording significant advantages such as elevated load-bearing capacity and extended flight endurance. Nonetheless, the control of this system is intricate and nonlinear due to the complex dynamics and coupling effects. This study addresses the issue of path following control for a powered parafoil using two linear active disturbance rejection control (LADRC) controllers, specifically designed for lateral path following and altitude control. The plane path following controller incorporates a guidance law to address the underactuated problem. To enhance the controllers efficacy, controller parameters are optimized via the twin delayed deep deterministic policy gradient (TD3) algorithm. Simulation outcomes evince that the proposed TD3-LADRC path following method adeptly tracks the intended path and altitude. The proposed approach exhibits a promising solution for the motion control of powered parafoil and possesses prospective applications in an array of aerial vehicles. |
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| AbstractList | The powered parafoil system is a distinctive flight vehicle that comprises a thrust device and an airdrop parafoil, affording significant advantages such as elevated load-bearing capacity and extended flight endurance. Nonetheless, the control of this system is intricate and nonlinear due to the complex dynamics and coupling effects. This study addresses the issue of path following control for a powered parafoil using two linear active disturbance rejection control (LADRC) controllers, specifically designed for lateral path following and altitude control. The plane path following controller incorporates a guidance law to address the underactuated problem. To enhance the controllers efficacy, controller parameters are optimized via the twin delayed deep deterministic policy gradient (TD3) algorithm. Simulation outcomes evince that the proposed TD3-LADRC path following method adeptly tracks the intended path and altitude. The proposed approach exhibits a promising solution for the motion control of powered parafoil and possesses prospective applications in an array of aerial vehicles. |
| Author | Sun, Qinglin Zheng, Yuemin Tao, Jin Sun, Hao Sun, Mingwei Chen, Zengqiang |
| Author_xml | – sequence: 1 givenname: Yuemin surname: Zheng fullname: Zheng, Yuemin email: zhengyueminylm@163.com organization: College of Artificial Intelligence, Nankai University,Tianjin,P. R. China,300350 – sequence: 2 givenname: Jin surname: Tao fullname: Tao, Jin email: taoj@nankai.edu.cn organization: Silo AI,Helsinki,Finland,00100 – sequence: 3 givenname: Qinglin surname: Sun fullname: Sun, Qinglin email: sunql@nankai.edu.cn organization: College of Artificial Intelligence, Nankai University,Tianjin,P. R. China,300350 – sequence: 4 givenname: Hao surname: Sun fullname: Sun, Hao email: sunh@nankai.edu.cn organization: College of Artificial Intelligence, Nankai University,Tianjin,P. R. China,300350 – sequence: 5 givenname: Mingwei surname: Sun fullname: Sun, Mingwei email: smw_sunmingwei@163.com organization: College of Artificial Intelligence, Nankai University,Tianjin,P. R. China,300350 – sequence: 6 givenname: Zengqiang surname: Chen fullname: Chen, Zengqiang email: chenzq@nankai.edu.cn organization: College of Artificial Intelligence, Nankai University,Tianjin,P. R. China,300350 |
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| Snippet | The powered parafoil system is a distinctive flight vehicle that comprises a thrust device and an airdrop parafoil, affording significant advantages such as... |
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| StartPage | 2364 |
| SubjectTerms | Aerospace electronics Control systems Couplings Deep reinforcement learning Linear active disturbance rejection control Nonlinear dynamical systems Path following control Powered parafoil system Robust control Tracking Transforms twin delayed deep deterministic policy gradient algorithm |
| Title | Path following control for powered parafoil system based on TD3-LADRC |
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