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In this paper, the controller for the attitude maintenance of low altitude pitch angle, roll angle and yaw angle at low altitude is designed based on the PID algorithm. Firstly, the mathematical modeling process of the quad-copter UAV is given, then the fractional-order PID algorithm is introduced, and finally, the control system of the UAV is simulated by MATLAB/Simulink. This paper proposes a UAV attitude control system based on the fractional order PID controller to solve problem of poor anti-interference performance of the traditional attitude control system.

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Research on UAV Attitude Control Based on Fractional-Order PID Controller

  • 会议论文

  • 发表日期：

    2025年

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  • Yinghuang Liu,
  • Rui Hou,
  • Zhi Lu

摘要

In this paper, the controller for the attitude maintenance of low altitude pitch angle, roll angle and yaw angle at low altitude is designed based on the PID algorithm. Firstly, the mathematical modeling process of the quad-copter UAV is given, then the fractional-order PID algorithm is introduced, and finally, the control system of the UAV is simulated by MATLAB/Simulink. This paper proposes a UAV attitude control system based on the fractional order PID controller to solve problem of poor anti-interference performance of the traditional attitude control system.