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...

Celý popis

Uloženo v:
Podrobná bibliografie
Vydáno v:Chinese Control Conference s. 2364 - 2369
Hlavní autoři: Zheng, Yuemin, Tao, Jin, Sun, Qinglin, Sun, Hao, Sun, Mingwei, Chen, Zengqiang
Médium: Konferenční příspěvek
Jazyk:angličtina
Vydáno: Technical Committee on Control Theory, Chinese Association of Automation 24.07.2023
Témata:
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
ISSN:1934-1768
On-line přístup:Získat plný text
Tagy: Přidat tag
Žádné tagy, Buďte první, kdo vytvoří štítek k tomuto záznamu!
Popis
Shrnutí: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.
ISSN:1934-1768
DOI:10.23919/CCC58697.2023.10240655