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螺旋桨转速受限多四旋翼无人机的编队运输分层控制方案

武权伟 王翔宇 刘金浩

武权伟, 王翔宇, 刘金浩. 螺旋桨转速受限多四旋翼无人机的编队运输分层控制方案. 自动化学报, xxxx, xx(x): x−xx doi: 10.16383/j.aas.c250439
引用本文: 武权伟, 王翔宇, 刘金浩. 螺旋桨转速受限多四旋翼无人机的编队运输分层控制方案. 自动化学报, xxxx, xx(x): x−xx doi: 10.16383/j.aas.c250439
Wu Quan-Wei, Wang Xiang-Yu, Liu Jin-Hao. A hierarchical control scheme for formation transportation of multiple quadrotors with propeller speed constraints. Acta Automatica Sinica, xxxx, xx(x): x−xx doi: 10.16383/j.aas.c250439
Citation: Wu Quan-Wei, Wang Xiang-Yu, Liu Jin-Hao. A hierarchical control scheme for formation transportation of multiple quadrotors with propeller speed constraints. Acta Automatica Sinica, xxxx, xx(x): x−xx doi: 10.16383/j.aas.c250439

螺旋桨转速受限多四旋翼无人机的编队运输分层控制方案

doi: 10.16383/j.aas.c250439 cstr: 32138.14.j.aas.c250439
基金项目: 国家自然科学基金(62533012, 62373099, 62025302), 东南大学未来技术学院"太湖创新基金项目"资助
详细信息
    作者简介:

    武权伟:东南大学自动化学院博士研究生.主要研究方向为多机器人协同规划与控制技术. E-mail: w_qw@seu.edu.cn

    王翔宇:东南大学自动化学院教授.主要研究方向为非光滑控制, 抗干扰控制及在多机器人协同系统, 电力电子系统中的应用. 本文通信作者. E-mail: w.x.y@seu.edu.cn

    刘金浩:中国矿业大学信息与控制工程学院博士后研究员. 主要研究方向为抗干扰控制、模型预测控制及其在运动控制系统与机器人系统中的应用. E-mail: liujinhao@cumt.edu.cn

  • 中图分类号: Y

A Hierarchical Control Scheme for Formation Transportation of Multiple Quadrotors With Propeller Speed Constraints

Funds: Supported by National Natural Science Foundation of China(62533012, 62373099, 62025302), Taihu Innovation Fund Project for the School of Future Technology of Southeast University
More Information
    Author Bio:

    WU Quan-Wei Ph.D. candidate at the School of Automation, Southeast University. His research interests cover cooperative planning and control technology of multiple robots

    WANG Xiang-Yu Professor at the School of Automation, Southeast University. His research interests cover non-smooth control, anti-disturbance control and their applications in multi-robot cooperative systems and power electronic systems. Corresponding author of this paper

    LIU Jin-Hao Postdoctoral Researcher at the School of Information and Control Engineering, China University of Mining and Technology. His research interests include disturbance rejection control, model predictive control, and their applications in motion control systems and robotic systems

  • 摘要: 多四旋翼无人机协同编队运输技术因其高容错性和强灵活性等特点, 近年来受到广泛关注. 针对受到螺旋桨转速约束和外界环境干扰影响的多四旋翼无人机系统, 提出一种分层控制方案以实现多无人机协同编队运输. 该方案设计主要包含分布式协调器设计和跟踪控制器设计. 在分布式协调器中, 位置协调器基于虚拟领导者的位置、速度等信息生成各带载无人机的期望位置, 然后微分平坦器输出无人机的期望无偏轨迹; 跟踪控制器采用非线性模型预测控制、角速度控制以及螺旋桨转速分配算法相结合的策略, 为各带载无人机生成合理的螺旋桨转速指令, 确保无人机精确跟踪其期望轨迹. 在所提方案作用下, 多带载无人机能维持期望编队队形并跟踪虚拟领导者, 从而实现多无人机协同编队运输. 特别地, 当省略位置协调器时, 该方案可简化为单无人机轨迹跟踪控制器. 数值仿真包括单机轨迹跟踪和多机协同运输两个场景, 结果表明: 在单机跟踪任务中, 所提方案展现出良好的跟踪精度; 在多机运输场景下, 多无人机能够有效实现协同编队运输.
  • 图  1  携带负载的四旋翼无人机示意图

    Fig.  1  Schematic diagram of the quadrotor with payload

    图  2  分层控制方案设计结构图

    Fig.  2  Schematic diagram of the hierarchical control scheme design

    图  3  无人机1和虚拟领导者的轨迹

    Fig.  3  The trajectories of the quadrotor 1 and virtual leader

    图  4  无人机1的跟踪距离误差曲线

    Fig.  4  The response curves of tracking distance error for the quadrotor 1

    图  5  干扰和干扰的估计

    Fig.  5  The disturbance and estimate of disturbance

    图  6  螺旋桨转速$ \mathbf{\Omega}_{1,\;i}(i=1,\;2,\;3,\;4) $响应曲线

    Fig.  6  The response curves for propeller speed $ \mathbf{\Omega}_{1,\;i}(i=1,\;2,\;3,\;4) $

    图  7  各方案的距离误差$ e_d $的分布对比

    Fig.  7  Comparison of the distribution of distance errors $ e_d $ among various schemes

    图  8  虚拟领导者-无人机系统的通信拓扑

    Fig.  8  The communication topology of the virtual leader - quadrotors system

    图  9  无人机和虚拟领导者的轨迹

    Fig.  9  Trajectories of the quadrotors and the virtual leader

    图  10  无人机和虚拟领导者的轨迹 (俯视)

    Fig.  10  Trajectories of the quadrotors and the virtual leader(planform)

    图  11  编队误差曲线

    Fig.  11  The response curve for formation error

    图  12  各无人机螺旋桨的转速曲线

    Fig.  12  The propeller speed curves of all the quadrotors

    表  1  变量符号表

    Table  1  Nomenclature

    符号 物理意义
    $ \boldsymbol{p}_{0},\;\boldsymbol{v}_{0},\; \boldsymbol{a}_{0},\; \boldsymbol{j}_{0} \in \mathbf{R}^{3} $ 虚拟领导者在惯性系$ \mathcal{F}_{I} $下的位置, 速度, 加速度, 加加速度
    $ \boldsymbol{p}_{r,\;i},\; \boldsymbol{v}_{r,\;i},\; \boldsymbol{a}_{r,\;i},\; \boldsymbol{j}_{r,\;i} \in \mathbf{R}^{3} $ 无人机$ i $参考轨迹在惯性系 $ \mathcal{F}_{I} $下的位置, 速度, 加速度, 加加速度
    $ \boldsymbol{\Theta}_{r,\;i},\; \boldsymbol{\omega}_{r,\;i} $ 无人机$ i $参考轨迹的姿态和角速度
    $ f_{r,\;i},\; \boldsymbol{\tau}_{r,\;i} $ 无人机$ i $参考轨迹的推力和力矩
    $ \boldsymbol{p}_{i},\;\boldsymbol{v}_{i},\; \boldsymbol{a}_{i},\; \boldsymbol{j}_{i} \in \mathbf{R}^{3} $ 无人机$ i $在惯性系$ \mathcal{F}_{I} $下的位置, 速度, 加速度, 加加速度
    $ \boldsymbol{\Theta}_{i} = [\psi_{i},\; \theta_{i},\; \phi_{i}]^{\mathrm{T}},\; \boldsymbol{\omega}_{i} $ 无人机$ i $的姿态和角速度
    $ \boldsymbol{\omega}_{de,\;i}\in \mathbf{R}^{3} $ 无人机$ i $NMPC算法输出的角速度信号
    $ \boldsymbol{f}_{c,\;i},\; \boldsymbol{\tau}_{c,\;i}\in \mathbf{R}^{3} $ 无人机$ i $受到来自负载的耦合力和力矩
    $ \boldsymbol{f}_{d,\;i},\; \boldsymbol{\tau}_{d,\;i}\in \mathbf{R}^{3} $ 无人机$ i $受到的外部力干扰和力矩干扰
    $ \boldsymbol{p}_{c,\;i}^{B_{i}} $ 在体坐标系$ \mathcal{F}_{B_{i}} $下, 无人机$ i $负载的质心
    $ J_{b,\;i}\in \mathbf{R}^{3\times 3} $ 在体坐标系$ \mathcal{F}_{B_{i}} $下, 无人机$ i $的惯量张量
    $ J_{c,\;i}\in \mathbf{R}^{3\times 3} $ 在体坐标系$ \mathcal{F}_{B_{i}} $下, 无人机$ i $负载的惯量张量
    $ m_{b,\;i},\; m_{c,\;i} $ 无人机$ i $的质量和其负载的质量
    $ f_{i},\; \boldsymbol{\tau}_{i} $ 无人机$ i $的推力和力矩
    $ \Omega_{i,\;j} $ 无人机$ i $的第$ j $个螺旋桨的转速
    $ R_{B,\;i}^{I}\in \mathbf{R}^{3\times 3} $ 从惯性系$ \mathcal{F}_{I} $到体坐标系$ \mathcal{F}_{B_{i}} $的旋转矩阵
    下载: 导出CSV

    表  2  无人机参数

    Table  2  Quadrotor parameters

    参数 数值 参数 数值
    $ m_{b,\; i} $ 1.0 kg $ d $ 0.3 m
    $ J_x $ $ 2.64 \times 10^{-3}\,\; \text{kg}\cdot\text{m}^2 $ $ c_T $ $ 1.984 \times 10^{-7}\,\; \text{N/PRM}^{2} $
    $ J_y $ $ 2.64 \times 10^{-3}\,\; \text{kg}\cdot\text{m}^2 $ $ c_M $ $ 3.733 \times 10^{-9}\,\; \text{N/PRM}^{2} $
    $ J_z $ $ 4.96 \times 10^{-3}\,\; \text{kg}\cdot\text{m}^2 $
    下载: 导出CSV

    表  3  各方案对比

    Table  3  Comparison of various schemes

    方案 分布式协调器是
    否考虑干扰
    动态(1a) $ \sim $ (1c)的控制算法
    DOB-PID $ - $ PID
    DOB-NMPC $ - $ NMPC
    所提方案
    (Proposed scheme, PS)
    $ \checkmark $ NMPC
    下载: 导出CSV

    表  4  各无人机携带负载

    Table  4  The payloads carried by quadrotors

    无人机 负载质量 负载质心 负载惯量张量
    $ 1,\;2,\;3 $ 0.10 kg $ {\begin{bmatrix} -0.05\\ 0.03\\ -0.10 \end{bmatrix}} $ m $ {\begin{bmatrix} 0.01083& 0.00500& -0.00500\\ 0.00500& 0.01083& 0.00500\\ -0.00500& 0.00500& 0.01083 \end{bmatrix}} $ kg·m $ ^{2} $
    $ 4,\;5 $ 0.13 kg $ {\begin{bmatrix} -0.05\\ 0.05\\ -0.12 \end{bmatrix}} $ m $ {\begin{bmatrix} 0.01470& 0.00700& -0.00700\\ 0.00700& 0.0147& 0.00700\\ -0.00700& 0.00700& 0.01470 \end{bmatrix} }$ kg·m $ ^{2} $
    下载: 导出CSV
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  • 收稿日期:  2025-08-31
  • 录用日期:  2025-11-14
  • 网络出版日期:  2026-01-20

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