基于迭代学习观测器的三旋翼无人机预定义时间抗扰容错跟踪控制
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作者单位:

1.山东航空学院自动化与电气工程学院;2.山东航空学院飞行学院

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中图分类号:

V249.1;V279

基金项目:

国家自然科学基金(62103060);山东省高等学校“青创团队计划”团队(2023KJ274);山东省自然科学基金(ZR2019PF021,ZR2020MF142);滨州市“揭榜挂帅”技术攻关项目(2025JBGS020)


Predefined-time disturbance-rejection fault-tolerant tracking control for tri-rotor UAVs based on an iterative learning observer
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Fund Project:

National Natural Science Foundation of China(62103060);Young Innovation Talent Team Program of Colleges and Universities in Shandong Province(2023KJ274);Shandong Natural Science Foundation of China(ZR2019PF021,ZR2020MF142);Technology Research and Development Project of Binzhou(2025JBGS020)

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    摘要:

    针对三旋翼无人机系统同时存在外部扰动、执行器故障时的跟踪控制,提出一种基于迭代学习观测器的预定义时间容错控制策略.考虑未知时变扰动和不同类型执行器故障,建立三旋翼无人机故障动力学模型;设计迭代学习观测器对扰动和执行器偏置故障进行实时估计,不依赖系统精确模型实现观测误差的渐近收敛;引入自适应算法估计执行器失效故障,设计基于预定义时间的自适应容错控制器保证无人机精确跟踪预定轨迹.采用Lyapunov理论证明了闭环系统在预定义时间内收敛.飞控半实物仿真平台实时实验表明,与有限时间滑模控制方法相比,本文所设计容错控制策略在保证系统稳定性的同时,提升了系统收敛速度与跟踪精度,能够在预定义时间内实现对无人机的精确跟踪控制.

    Abstract:

    To address the tracking control problem of tri-rotor unmanned aerial vehicles (UAVs) subject to simultaneous external disturbances and actuator faults, a predefined-time fault-tolerant tracking control strategy based on an iterative learning observer is proposed. Considering unknown time-varying disturbances and various types of actuator faults, a faulty dynamic model of the tri-rotor UAV is established. An iterative learning observer is designed to provide real-time estimation of disturbances and actuator bias faults, achieving asymptotic convergence of the observation errors without relying on an accurate system model. An adaptive algorithm is further introduced to estimate actuator loss-of-effectiveness faults, and an adaptive fault-tolerant controller with predefined-time performance is developed accordingly. The Lyapunov stability theory is applied to rigorously prove the convergence of the closed-loop system within the predefined time. Real-time experiments conducted on a flight control hardware-in-the-loop simulation platform demonstrate that, in comparison with finite-time sliding mode control, the proposed strategy not only guarantees system stability but also significantly enhances convergence speed and tracking accuracy, enabling precise tracking of the UAV within the predefined time.

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  • 收稿日期:2026-04-09
  • 最后修改日期:2026-08-06
  • 录用日期:2026-08-10
  • 在线发布日期: 2026-08-21
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