航空学报 > 2026, Vol. 47 Issue (9): 123-135   doi: 10.7527/S1000-6893.2025.32813

先进飞行器安全控制技术专刊

基于动态补偿器的四旋翼无人机全驱抗干扰控制

王晓娟, 田广泰, 李彬(), 何振清   

  1. 四川大学 空天科学与工程学院,成都 610065
  • 收稿日期:2025-09-22 修回日期:2025-10-20 接受日期:2025-11-21 出版日期:2026-05-15 发布日期:2025-12-08
  • 通讯作者: 李彬 E-mail:bin.li@scu.edu.cn
  • 基金资助:
    国家自然科学基金(U24B20156);国家自然科学基金青年科学基金(62503343);空间智能控制技术重点实验室稳定支持基金(HTKJ2023KL502005);空间智能控制技术重点实验室稳定支持基金(HTKJ2024KL502007)

Fully actuated anti-disturbance control for quadrotor UAVs based on dynamic compensator

Xiaojuan WANG, Guangtai TIAN, Bin LI(), Zhenqing HE   

  1. School of Aeronautics and Astronautics,Sichuan University,Chengdu 610065,China
  • Received:2025-09-22 Revised:2025-10-20 Accepted:2025-11-21 Online:2026-05-15 Published:2025-12-08
  • Contact: Bin LI E-mail:bin.li@scu.edu.cn
  • Supported by:
    National Natural Science Foundation of China(U24B20156);National Natural Science Foundation of China(62503343);National Key Laboratory of Space Intelligent Control(HTKJ2023KL502005)

摘要:

针对四旋翼无人机在复杂环境下的轨迹跟踪控制问题,提出一种基于动态补偿器和扩张状态观测器的全驱抗干扰运动控制方法。相比于传统位置-姿态分环控制架构,将6-DOF不确定性四旋翼无人机动力学模型通过状态变换转换为混合阶全驱系统模型,实现了输入到状态的一体化控制器设计。基于线性扩张观测器的复合控制律的内环是一个实时精确估计不可测量状态与未知扰动的线性扩张状态观测器,并通过复合控制律进行主动补偿,其外环是一个结合动态补偿器的全驱控制器,通过额外的自由度提高控制精度,同时控制器增益仅与单个参数相关,简化了参数调节过程。仿真结果表明:提出的方法能够使得四旋翼无人机高精度跟踪螺旋上升轨迹,尤其在高度和偏航角控制方面展现显著优势,有效解决了四旋翼无人机抗干扰控制问题,为四旋翼无人机的轨迹跟踪运动控制提供了一种系统化解决方案。

关键词: 四旋翼无人机, 全驱系统方法, 动态补偿器, 扩张状态观测器, 抗干扰控制

Abstract:

To address the trajectory tracking control problem of quadrotor UAVs in complex environments, this paper proposes a fully actuated anti-disturbance motion control method based on a dynamic compensator and extended state observer. Compared to the traditional position-attitude dual-loop control architecture, this paper transforms the uncertain 6-DOF quadrotor model into a mixed-order fully actuated system model via state transformation, which facilitates the design of an integrated input-to-state controller. Secondly, this paper presents a composite control law based on a linear extended state observer. The inner loop consists of a linear extended state observer that accurately estimates unmeasurable states and unknown disturbances in real time, with active compensation via the composite control law. The outer loop employs a fully actuated controller combined with a dynamic compensator, providing additional degrees of freedom to enhance control precision, while the controller gain depends only on a single parameter, simplifying parameter tuning process. Simulation results demonstrate that the proposed method enables quadrotor UAVs to track spiral ascent trajectories with high precision, showing significant advantages in altitude and yaw angle control. The approach effectively addresses the anti-disturbance control problem of quadrotor UAVs and provides a systematic solution for trajectory tracking motion control.

Key words: quadrotor UAV, fully actuated system approach, dynamic compensator, extended state observer, anti-disturbance control

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