四旋翼无人机轨迹稳定跟踪控制
CSTR:
作者:
作者单位:

(天津理工大学电气电子工程学院,天津300384)

作者简介:

通讯作者:

E-mail: FengL_stu93@163.com.

中图分类号:

TP273

基金项目:

国家自然科学基金项目(61603274).


Trajectory stable tracking control of quadrotor UAV
Author:
Affiliation:

(School of Electrical and Electronic Engineering,Tianjin University of Technology,Tianjin300384,China)

Fund Project:

  • 摘要
  • |
  • 图/表
  • |
  • 访问统计
  • |
  • 参考文献
  • |
  • 相似文献
  • |
  • 引证文献
  • |
  • 资源附件
  • |
  • 文章评论
    摘要:

    针对四旋翼无人机轨迹稳定跟踪控制问题,为抑制外界扰动和参数不确定性的影响,设计一种双环鲁棒控制系统.首先,基于动态面内模法设计输出调节器进行位置控制,可解决系统的渐近跟踪及干扰抑制问题;其次,利用高阶滑模设计姿态控制器,可实现全局有限时间收敛,消除系统抖振和相对阶的限制;再次,为进一步提高控制精度,采用一种鲁棒精确微分器对姿态角指令信号进行精确求导;最后,对系统稳定性进行严格的数学证明,并与PID控制和传统滑模控制进行仿真对比,结果验证了所提出控制策略的优越性和鲁棒性.

    Abstract:

    Aiming at the problem of stable tracking control of quadrotor trajectory, a double-loop robust control system is designed to suppress the influence of external disturbance and parameter uncertainty. Firstly, the output regulator is designed for position control based on the dynamic surface internal model method, which can solve the problems of asymptotic tracking and disturbance rejection. Then, the higher order sliding mode is used to design the attitude controller, which can realize the global finite-time convergence, eliminate the chattering and relative order limitation of the system. In order to further improve the control precision, a robust accurate differentiator is adopted to accurately differentiate the attitude angle command signal. Finally, the strict mathematical proof for the stability of the system is given, and compared with PID control and traditional sliding mode control, the simulation results verify the superiority and robustness of the proposed control strategy.

    参考文献
    相似文献
    引证文献
引用本文

李俊芳,李峰y,吉月辉,等.四旋翼无人机轨迹稳定跟踪控制[J].控制与决策,2020,35(2):349-356

复制
分享
文章指标
  • 点击次数:
  • 下载次数:
  • HTML阅读次数:
  • 引用次数:
历史
  • 收稿日期:
  • 最后修改日期:
  • 录用日期:
  • 在线发布日期: 2020-01-18
  • 出版日期:
文章二维码