四旋翼飞行器有界输出控制
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  • 英文篇名:Bounded output control for quadrotors
  • 作者:师五喜 ; 李康利
  • 英文作者:SHI Wu-xi;LI Kang-li;School of Electrical Engineering and Automation,Tianjin Polytechnic University;
  • 关键词:四旋翼飞行器 ; 有界输出 ; 障碍Lyapunov函数 ; 滑模控制
  • 英文关键词:quadrotors;;bounded output;;barrier Lyapunov function;;sliding mode control
  • 中文刊名:TJFZ
  • 英文刊名:Journal of Tianjin Polytechnic University
  • 机构:天津工业大学电气工程与自动化学院;
  • 出版日期:2019-03-01 10:01
  • 出版单位:天津工业大学学报
  • 年:2019
  • 期:v.38;No.184
  • 基金:天津市自然科学基金资助项目(15JCYBJC47800)
  • 语种:中文;
  • 页:TJFZ201901013
  • 页数:7
  • CN:01
  • ISSN:12-1341/TS
  • 分类号:71-77
摘要
为了改善四旋翼飞行器实际起飞时超调过大问题,提出了一种基于障碍Lyapunov函数的有界输出控制方法。该方法采用障碍Lyapunov函数与滑模控制相结合设计控制器,利用障碍Lyapunov函数将传统滑模面约束在一定的范围内,从而来保证四旋翼飞行器输出保持在一定的范围内。仿真和实验结果表明:本方法不仅能使系统的实际输出值y_1跟踪上期望输出值y_(1d),还能够使实际输出值y_1始终保持在预先设定的范围内,即|y_1|        In order to improve the overshoot problem of quadrotors on actual takeoff, a bounded output control based on barrier Lyapunov function is proposed. The barrier Lyapunov function is combined with sliding mode control to design the controller, by using the barrier Lyapunov function, the traditional sliding mode surface is constrained within a certain range so as to ensure that the quadrotors′ outputs remain within a certain range. Simulation and experimental results show that the above method not only enables the actual output value of the system y_1 to track the desired output value y_(1 d), but also keeps the actual output value y_1 within the predetermined bounding range,|y_1| < k_c, k_c is positive constant.
引文
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