期刊文献+

采用可变边界层法削弱一类非线性变结构系统的抖振 被引量:3

CHATTERING REDUCTION USING VARIABLE BOUNDARY LAYER SOLUTION IN A CLASS OF NONLINEAR VARIABLE STRUCTURE SYSTEMS
原文传递
导出
摘要 针对一类非线性系统,提出一种削弱变结构控制系统抖振的新方法—可变边界层法,推导出变结构控制系统的稳态误差与饱和特性宽度之间定量的数学关系,通过系统的稳态误差指标可以设计出边界层宽度变化的饱和特性,从而既削弱了系统的抖振又满足系统稳态误差指标,仿真结果验证了该方法的有效性. A new method, variable boundary layer solution, is proposed in this paper for a class of nonlinear variable structure systems to restrain the chattering. The mathematical relationship between the static errors and the width of saturating property is presented. The saturating property with time-varying boundary layer width can be designed through the specification of the static errors, which can not only reduce the chattering in the system but also simultaneously satisfy the specification of the static errors. The simulation results show the validity of the method.
出处 《系统科学与数学》 CSCD 北大核心 2008年第9期1084-1091,共8页 Journal of Systems Science and Mathematical Sciences
关键词 变结构控制 非线性系统 边界层 抖振 Variable structure control, nonlinear systems, boundary layer, chattering.
  • 相关文献

参考文献7

  • 1Lee Jujang, Xu Yangsheng. A new method of switching surface design for multivaxiable variable structure systems. Journal of the Royal Statistical Society, Series B, 2001, 63(1): 19-29.
  • 2L in F J, Chiu S L. Adaptive fuzzy sliding-mode control for PM synchronous servo motor drives. IEEE Proceedings Control Theory and Applications, 1998, 145(1): 63-72.
  • 3Pushkin Kachroo, Masayo Shi, Tom Izuka. Chattering reduction and error convergence in the sliding-mode control of a class of nonlinear systems. IEEE Trans on Aurora Contr, 1996, 41(7): 1063-1068.
  • 4Xu Jianxin, Lee Tongheng, Wang Mao et al. Design of variable structure controllers with continuous switching control. Int J Contr, 1996, 65(3): 409-431.
  • 5Bonto Lini G. An improved, chattering free, VSC scheme for uncertain dynamical system. IEEE Trans on Aurora Control, 1996, 41(8): 241-246.
  • 6Nguyen Q I, Rye D C, Durrantwhyte H F. Fuzzy sliding-mode controllers with application. IEEE, 2001, 48(1): 38-46.
  • 7Utkin V I. Variable structure control systems with sliding mode. IEEE Transactions on Automatic Control, 1977, 22: 212-222.

同被引文献41

  • 1胡剑波,时满宏,庄开宇,褚健,苏宏业.一类非线性系统的Terminal滑模控制[J].控制理论与应用,2005,22(3):495-498. 被引量:20
  • 2SINGH A, KHALIL H K. Regulation of nonlinear systems using conditional integrators [ J ]. International Journal of Robust and Nonlinear Control,2005, 15 (8) : 339 - 362.
  • 3SINGH A, KHALIL H K. State feedback regulation of nonlinear systems using conditional integrators [ C ]// Proceedings of the IEEE Conference on Decision and Control. Nassau : CDC, 2004 : 4560 - 4564.
  • 4SESHAGIRI S, KHALIL H K. Robust output feedback regulation of minimum-phase nonlinear systems using conditional integrators[J]. Automatica, 2005, 41 ( 1 ) : 43 - 54.
  • 5TIAN Fu-yang, WU Hong-tao, SUN Hong-li. Efficient numerical integration method for dynamic of flexible space robots system [ C ]//2009 International Asia Conference on Informatics in Control, Automation, and Robotics. Bangkok : CAR, 2009 : 102 - 106.
  • 6YU Zhi-fu, YU Yong-bo, SHANG De-yong, et al. On orbit servicing flexible space robots dynamics and control during capturing target [ C ]//2010 International Conference on Measuring Technology and Mechatronics Automation. Changsha: ICMTMA, 2010 : 817 - 820.
  • 7KIRAN G S, KUMAR A, PATHAK P M, et al. Trajectory control of flexible space robot [ C ]//Proceedings of 2008 IEEE International Conference on Mechatronics and Automation. Takamatsu : ICMA, 2008 : 738 - 743.
  • 8ZHAO Hong-chao, CHEN De-qang. Optimal motion planning for flexible space robots [ C ]//ProceedingsIEEE International Conference on Robotics and Automation. Piscataway: IEEE, 1996 : 393 - 398.
  • 9MUROTSU Y, TSUJIO S, SENDA K, et al. Trajectory control of flexible manipulators on a free-flying space robot[J]. IEEE, 1992, 12(3):51-57.
  • 10GREEN A, SASIADEK J Z. Intelligent tracking control of a free-flying flexible space robot manipulator [ C ]// Collection of Technical Papers-AIAA Guidance, Navigation, and Control Conference 2007. Hilton Head: American Institute of Aeronautics and Astronautics, 2007 : 132 - 156.

引证文献3

二级引证文献13

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部