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April 4, 2026Symmetry0 citationsOpen Access

Anti-Wind Disturbance Algorithms for Small Rotorcraft UAVs

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YCYini ChengFTFeng TangLPLili Pei

Key Points

  • The aim is to develop an improved control strategy for small rotorcraft UAVs to counteract wind disturbances.
  • Proposed a fuzzy logic-based linear active disturbance rejection control (Fuzzy-LADRC) strategy.
  • Employed a hybrid optimization algorithm combining particle swarm optimization and gray wolf optimization.
  • Conducted simulation experiments in MATLAB/Simulink under complex wind-field conditions.
  • Control performance for roll and pitch angles improves by approximately 5%.
  • Yaw angle control shows an improvement of up to 30%.
  • Position deviation and fluctuation in the X and Y directions significantly suppressed.
  • Overshoot in the Z-axis during UAV takeoff reduced by 75%.

Abstract

Small rotorcraft unmanned aerial vehicles (UAVs) are highly susceptible to wind disturbances when performing tasks such as fixed-point hovering, low-altitude inspection, and aggressive maneuvers. Under complex, variable meteorological conditions, attitude stability and position-holding accuracy are particularly critical. Although quadrotor UAVs exhibit structural and dynamic symmetry, real wind disturbances are often asymmetric, disrupting the original balance and leading to intensified attitude oscillations, position drift, and degraded data quality. To effectively address the challenges of wind-induced oscillation and positional deviation, this paper proposes a fuzzy logic-based linear active disturbance rejection control (Fuzzy-LADRC) strategy. This approach employs a hybrid algorithm combining particle swarm optimization and gray wolf optimization to optimize controller parameters and incorporates fuzzy logic to enhance the adaptive capability of the linear active disturbance rejection controller (LADRC). Simulation experiments conducted in MATLAB/Simulink under complex wind-field conditions demonstrate that the proposed method significantly outperforms traditional PID controllers: in the regulation of roll and pitch angles, control performance improves by approximately 5%, while in yaw angle control, the improvement reaches up to 30%. Furthermore, this method can significantly suppress position deviation and fluctuation in the X and Y directions, and reduce the overshoot in the Z-axis during the UAV’s takeoff phase by 75%.

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Cite This Study

Cheng et al. (2026) studied this question.

synapsesocial.com/papers/69d0afde659487ece0fa6007https://doi.org/10.3390/sym18040594
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