Design of Dual-tiltable Ducted-Fan Aircraft Based on Cross-coupling Network Control

Authors

  • Xinchao Liu
  • Zeqing Chen
  • Ronghao Guo

DOI:

https://doi.org/10.54097/ajst.v7i3.13413

Keywords:

Cross-coupling network, Tilt angle, Ducted fan, Aircraft.

Abstract

In recent years, with the rapid development of drone technology, unmanned aerial systems have been widely applied in various fields. Although the flight control and airframe structure of traditional multirotor aircraft are fairly mature, they still face challenges such as low aerodynamic efficiency, low safety, and complex structure. In order to solve these issues, a dual-tiltable-ducted-fan aircraft system is designed. The system is equipped with an STM32F407 processor as the main controller, which receives motion control information from the remote control module. By employing cross-coupling network control methods, it coordinates the output values and tilt angles of the two channeling fans to achieve stable control of the aircraft's flight attitude.

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References

Liu, C. Design and Implementation of Dual Ducted Fan VTOL Aircraft. South China University of Technology, 2015.

Zhang, F. Research and Design of Dual PMSM Speed Synchronization Control System. [Published on October 14, 2023].

Chen, S., Hua, R., & Ji, B. Modeling and System Studies of Dual Ducted Tilt VTOL Aircraft. Aerospace Control, 2017, 35(1): 6. DOI: CNKI:SUN:HTKZ.0.2017-01-006.

Chen, F. Control Study on the High-Speed-to-Hover Transition Flight Process of Ducted Fan Aircraft. South China University of Technology, 2021.

Cong, S., & Liu, Y. Cross-Coupling Control in Multi-Axis Coordinated Motion. Machinery Design and Manufacturing, 2006(10): 3. DOI: 10.3969/j.issn.1001-3997.2006.10.069.

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Published

29-10-2023

Issue

Section

Articles

How to Cite

Liu, X., Chen, Z., & Guo, R. (2023). Design of Dual-tiltable Ducted-Fan Aircraft Based on Cross-coupling Network Control. Academic Journal of Science and Technology, 7(3), 274-279. https://doi.org/10.54097/ajst.v7i3.13413