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So as to deal with the poor static stability, strong nonlinear aerodynamic parameters and serious coupling of control rudder surface of flying-wing UAV. On the basis of the theory of active disturbance rejection control (ADRC), this attitude controller consists of two parts, which are outer angle controller and inner angle velocity controller. The simulation displays that this attitude controller shows advantageous control effect and strong robustness.

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Attitude Control for Flying-Wing UAV Based on Active Disturbance Rejection Control

  • 会议论文

  • 发表日期：

    2025年

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  • Boyuan Shen,
  • Xi Huang,
  • Qingxian Li,
  • Pengyuan Qi

摘要

So as to deal with the poor static stability, strong nonlinear aerodynamic parameters and serious coupling of control rudder surface of flying-wing UAV. On the basis of the theory of active disturbance rejection control (ADRC), this attitude controller consists of two parts, which are outer angle controller and inner angle velocity controller. The simulation displays that this attitude controller shows advantageous control effect and strong robustness.