首页 | 本学科首页   官方微博 | 高级检索  
     检索      

倒立摆系统的建模与积分滑模控制
引用本文:李振山,陈勇,雷军委.倒立摆系统的建模与积分滑模控制[J].海军航空工程学院学报,2014,29(3):217-220.
作者姓名:李振山  陈勇  雷军委
作者单位:[1]91183部队,山东青岛266071 [2]海军装备部,北京100071 [3]海军航空工程学院控制工程系,山东烟台264001
摘    要:在研究了倒立摆系统动力学模型的基础上,提出了一种积分滑模变结构的控制方法。通过设计积分性质的非线性滑模面,可以减少系统静差,提高控制精度,系统鲁棒性能获得了很好的保存。仿真证明,该方法能够在较短时间内实现系统的稳定,提高系统的控制精度,使倒立摆系统具有更高的稳定性和鲁棒性。

关 键 词:倒立摆  积分  滑模  非线性  耦合

Modeling and Integral Sliding Mode Control of Inverted Pendulum System
LI Zheng-shan,CHEN Yong and LEI Jun-wei.Modeling and Integral Sliding Mode Control of Inverted Pendulum System[J].Journal of Naval Aeronautical Engineering Institute,2014,29(3):217-220.
Authors:LI Zheng-shan  CHEN Yong and LEI Jun-wei
Institution:1. The 91183rd Unit of PLA, Qingdao Shandong 266071, China; 2. Naval Equitment Department, Beijing 100071, China; Department of Control Engineering, NAAU, Yantai Shandong 264001, China)
Abstract:Based on the research on the inverted pendulum system dynamics model, a kind of integral sliding mode variable structure control method was proposed in this paper. The static error could be reduced and control precision could be proved by the introducing of integral item. Also the system had a strong robustness as the using of sliding mode control. Finally, a detailed numerical simulation was done and the rightness and robustness of the proposed method was testified.
Keywords:inverted pendulum  integral  sliding mode  nonlinear  coupling
本文献已被 维普 等数据库收录!
点击此处可从《海军航空工程学院学报》浏览原始摘要信息
点击此处可从《海军航空工程学院学报》下载免费的PDF全文
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号