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基于自适应通信拓扑四旋翼无人机编队重构控制

马思迁 董朝阳 马鸣宇 王青

马思迁, 董朝阳, 马鸣宇, 等 . 基于自适应通信拓扑四旋翼无人机编队重构控制[J]. 北京亚洲成人在线一二三四五六区学报, 2018, 44(4): 841-850. doi: 10.13700/j.bh.1001-5965.2017.0281
引用本文: 马思迁, 董朝阳, 马鸣宇, 等 . 基于自适应通信拓扑四旋翼无人机编队重构控制[J]. 北京亚洲成人在线一二三四五六区学报, 2018, 44(4): 841-850. doi: 10.13700/j.bh.1001-5965.2017.0281
MA Siqian, DONG Chaoyang, MA Mingyu, et al. Formation reconfiguration control of quadrotor UAVs based on adaptive communication topology[J]. Journal of Beijing University of Aeronautics and Astronautics, 2018, 44(4): 841-850. doi: 10.13700/j.bh.1001-5965.2017.0281(in Chinese)
Citation: MA Siqian, DONG Chaoyang, MA Mingyu, et al. Formation reconfiguration control of quadrotor UAVs based on adaptive communication topology[J]. Journal of Beijing University of Aeronautics and Astronautics, 2018, 44(4): 841-850. doi: 10.13700/j.bh.1001-5965.2017.0281(in Chinese)

基于自适应通信拓扑四旋翼无人机编队重构控制

doi: 10.13700/j.bh.1001-5965.2017.0281
基金项目: 

国家自然科学基金 61374012

详细信息
    作者简介:

    马思迁  男, 硕士研究生。主要研究方向:飞行器协同控制

    董朝阳  男, 博士, 教授, 博士生导师。主要研究方向:飞行器设计, 导航、制导与控制

    通讯作者:

    董朝阳, E-mail: dongchaoyang@cqjj8.com

  • 中图分类号: V249;TP273

Formation reconfiguration control of quadrotor UAVs based on adaptive communication topology

Funds: 

National Natural Science Foundation of China 61374012

More Information
  • 摘要:

    针对四旋翼无人机编队重构协同控制问题,基于切换通信拓扑结构的积分滑模控制(ISMC)方法进行了研究。根据四旋翼无人机间的通信拓扑关系以及编队重构特性,建立了四旋翼无人机编队模型。针对编队重构过程中可能出现的通信可靠性问题,提出了通信拓扑切换条件,结合积分滑模控制理论对切换通信拓扑条件下的协同控制器进行设计,并结合切换系统理论对编队系统稳定性进行了证明。仿真结果表明,无人机编队系统在编队重构过程中采用切换通信拓扑结构以及滑模控制方法能保证系统的稳定性,验证了方法的有效性。

     

  • 图 1  四旋翼无人机坐标系及姿态角

    Figure 1.  Quadrotor UAV coordinate system and attitude angle

    图 2  四旋翼无人机相对位置矢量关系

    Figure 2.  Relative position vector relationship of quadrotor UAVs

    图 3  四旋翼无人机期望队形

    Figure 3.  Desired formation of quadrotor UAVs

    图 4  四旋翼无人机编队重构仿真结果

    Figure 4.  Reconfiguration simulation results of quadrotor UAV formation

    图 5  四旋翼无人机编队通信拓扑结构

    Figure 5.  Communication topology of quadrotor UAV formation

    表  1  无人机初始状态

    Table  1.   Initial conditions of UAV

    无人机编号 位置/m 速度/(m·s-1)
    1 [3, 1, 50] [-0.1, 0, 1]
    2 [-1, 3, 50] [-0.3, -0.1, 1]
    3 [2, -1, 50] [-0.1, -0.1, 1]
    4 [1, 1, 50] [-0.1, 0, 1]
    5 [0, 0, 52] [0, -0.1, 0]
    下载: 导出CSV

    表  2  有向拓扑权重

    Table  2.   Weight of directed topology

    无人机编号 1 2 3 4 5
    1 0.77 0.56 0.69 0.27
    2 0.78 0.74 0.66 0.53
    3 0.63 0.75 0.73 0.62
    4 0.55 0.68 0.80 0.82
    5 0.31 0.49 0.61 0.74
    下载: 导出CSV
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出版历程
  • 收稿日期:  2017-05-05
  • 录用日期:  2017-08-01
  • 网络出版日期:  2018-04-20

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