GU Xun, WANG Pengbo. Fault-tolerant Disturbance Rejection Pose Tracking Control for Quadrotor UAV Based on RBF-SMO[J]. INFORMATION AND CONTROL, 2025, 54(4): 570-582. DOI: 10.13976/j.cnki.xk.2024.2651
Citation: GU Xun, WANG Pengbo. Fault-tolerant Disturbance Rejection Pose Tracking Control for Quadrotor UAV Based on RBF-SMO[J]. INFORMATION AND CONTROL, 2025, 54(4): 570-582. DOI: 10.13976/j.cnki.xk.2024.2651

Fault-tolerant Disturbance Rejection Pose Tracking Control for Quadrotor UAV Based on RBF-SMO

  • The quadrotor UAV is easily-influenced to actuator failure faults and unknown environmental disturbances during the practical flight, which severely affects the safety of the flight. Therefore, a novel composite fault-tolerant pose tracking control strategy is proposed for the dynamics of quadrotor UAV with the time-varying actuator faults and the time-varying external disturbances. In the position loop, a PD (Proportional-Derivative) control strategy is designed to achieve the position tracking control for quadrotor UAV. In the attitude loop, by combining an adaptive neural network with a fixed-time sliding mode observer (SMO), a composite fault-tolerant pose tracking control strategy is designed. A radial basis function (RBF) neural network is used to compensate for time-varying actuator faults in real time. Meanwhile, to overcome the impact of external disturbances on UAV flight performance, an SMO is designed to compensate for time-varying external unknowndisturbances in real time and to reduce system chattering. Finally,the stability of the closed-loop system is proven based on Lyapunov analysis theory. The numerical simulation results demonstrate that the proposed composite fault-tolerant pose tracking control strategy exhibits faster convergence speed, higher pose tracking accuracy, and stronger fault-tolerant control performance compared to the traditional PID (Proportional-Integral-Derivative) control strategy.
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