Implementation of Fuzzy-PID Controller for 2-DOF Helicopter

Authors

  • Thanh-Do Huynh Ho Chi Minh city University of Technology and Education
  • Ngoc-Thanh Bach Ho Chi Minh city University of Technology and Education
  • Quang-Dao Le Ho Chi Minh city University of Technology and Education
  • Duong-Dong Le Ho Chi Minh city University of Technology and Education
  • Viet-Hoang Bui Ho Chi Minh city University of Technology and Education
  • Hoai-An Vo Ho Chi Minh city University of Technology and Education
  • Viet-Nhat-Long Nguyen Ho Chi Minh city University of Technology and Education
  • Phi-Hung Pham Ho Chi Minh city University of Technology and Education
  • Huu-Dat Nguyen Ho Chi Minh city University of Technology and Education
  • Van-Dong-Hai Nguyen Ho Chi Minh city of Technology and Education

DOI:

https://doi.org/10.59247/jfsc.v2i2.204

Keywords:

Fuzzy-PID control, PID Control, 2 Dof-Helicopter, Brushless Motor

Abstract

This article presents the model and control of a 2-DOF helicopter, a multi-input multi-output (MIMO) system that is set up in the laboratory. The conventional mathematical model, employing the Euler-Lagrange method, is utilized in this study to conduct the system modeling process. The transfer functions derived from this model are then incorporated into diverse control methodologies to optimize PID gain coefficients. The PID controllers are employed to control this system. In addition, we use a Fuzzy controller to adjust the Kp, Ki, and Kd coefficients of this PID. As a result, we obtain a fuzzy PID controller with superior control quality than a PID controller. Under Fuzzy-PID, the system operates more stably, overcoming some weaknesses of the PID linear controller. The state space model is built by considering specific design assumptions and simplifications. Results are obtained through simulation and testing on the model.

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Published

2024-05-16

How to Cite

[1]
T.-D. Huynh, “Implementation of Fuzzy-PID Controller for 2-DOF Helicopter”, JFSC, vol. 2, no. 2, pp. 74–80, May 2024.

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