摘要
This article investigates the trajectory tracking control problem for quadrotor UAVs using the dynamic event-triggered control approach. Unlike existing results, the dynamic event-triggered control strategy proposed in this work ensures that the trajectory tracking error of quadrotor UAVs converges to zero asymptotically for a class of external disturbances. Specifically, an event-triggered mechanism is introduced in the position loop to reduce the resource transmission consumption. To address the non-differentiable nature of the event-triggered signal, a fourth-order linear system model for the position loop is derived, ensuring the existence of a twice-differentiable acceleration reference which is essential for the attitude loop. Subsequently, based on the internal model principle, we develop a class of dynamic event-triggered control strategies with dynamic triggering mechanisms. Furthermore, to handle the challenges posed by the unknown parameters and external perturbations within the attitude-loop subsystem, a robust adaptive dynamic control law is implemented based on the attitude rotation matrix. Rigorous Lyapunov analysis demonstrates that the overall control approach ensures asymptotic stability of the closed-loop system. Finally, we verify the effectiveness and robustness of the controller through numerical simulations.
| 源语言 | 英语 |
|---|---|
| 页(从-至) | 4669-4685 |
| 页数 | 17 |
| 期刊 | International Journal of Robust and Nonlinear Control |
| 卷 | 35 |
| 期 | 11 |
| DOI | |
| 出版状态 | 已出版 - 25 7月 2025 |
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