期刊文献+

高阶系统方法——I全驱系统与参数化设计 被引量:38

High-order System Approaches:I.Fully-actuated Systems and Parametric Designs
在线阅读 下载PDF
导出
摘要 本文首先指出了控制领域中普遍使用的增广一阶系统方法的弊端,介绍了高阶全驱系统的概念及其在控制器设计方面的优势,并通过一些基础物理定律、串联系统、严反馈系统和可反馈线性化系统等例子说明了高阶全驱系统的普遍性,进而指出高阶全驱系统是动态系统的一种描述形式,是面向控制的模型.然后介绍了一类高阶全驱系统的一种参数化设计方法.通过适当选取一类非线性状态反馈控制律,可获得一个具有希望特征结构的线性定常闭环系统,并给出了闭环系统特征向量和反馈控制律的完全参数化表示,讨论了解的存在性条件以及设计参数集合的稠密性等相关问题.最后对高阶全驱系统方法的后续问题做了说明和展望. In this paper, the drawback of the first-order system approaches which are widely used in the field of control systems is firstly pointed out, meanwhile the concept of high-order fully-actuated systems and, in particular, its advantage in controller design are introduced. The type of systems is demonstrated to be of wide existence by examining a number of basic physical laws and a few examples, including the common cascaded systems, the well-known strict-feedback systems,and those which can be linearized through feedback, and thus can be taken as a description of dynamical systems,more precisely, as a model for control. Then, a parametric design approach for the type of high-order fully-actuated systems is presented. With a proper nonlinear state feedback controller, a linear constant closed-loop system with desired eigenstructure can be derived, and complete parametric presentations for the closed-loop eigenvectors and the feedback law are given. Conditions of existence of solutions as well as the density of the set of design parameters are discussed.Finally, some further comments are made about future problems existing in the field of high-order fully-actuated systems.
作者 段广仁 DUAN Guang-Ren(Center for Control Theory and Guidance Technology,Harbin Institute of Technology,Harbin 150001)
出处 《自动化学报》 EI CSCD 北大核心 2020年第7期1333-1345,共13页 Acta Automatica Sinica
基金 国家自然科学基金重大项目(61690210,61690212) 国家自然科学基金(61333003) 机器人与系统国家重点实验室自主计划任务(HIT)(SKLRS201716A)资助。
关键词 高阶系统 全驱系统 参数化方法 特征结构 设计自由度 High-order systems fully-actuated systems parametric approaches eigenstructure design degrees of free-dom
作者简介 段广仁,中国科学院院士,国家杰出青年基金获得者,长江学者奖励计划特聘教授,哈尔滨工业大学控制理论与制导技术研究中心主任,CAA Fellow,IEEE Fellow,IET Fellow.1989年获得哈尔滨工业大学博士学位.主要研究方向为控制系统的参数化设计,鲁棒控制,广义系统,航天器制导与控制.E-mail:g.r.duan@hit.edu.cn。
  • 相关文献

参考文献5

二级参考文献58

  • 1王文涛,刘晓平,赵军.非线性奇异系统的能控性子分布[J].自动化学报,2004,30(5):716-722. 被引量:2
  • 2段广仁,王好谦.多模型切换控制及其在BTT导弹设计中的应用[J].航空学报,2005,26(2):144-147. 被引量:22
  • 3井元伟,胡三清,刘晓平,张嗣瀛.可解的具有广义对称性的非线性系统的同构分解与可控性[J].控制理论与应用,1996,13(2):259-263. 被引量:1
  • 4Chu P Y, Wie B, Gretz B, et al. Approach to large structure control system design using traditional tools [ J ]. Journal of Guidance, Control, and Dynamics, 1990,13 (5) : 874 - 880.
  • 5Meirovitch L, Kwak M K. Control of flexile spacecraft with time- varying configuration [ J ]. Journal of Guidance, Control, and Dynamics, 1992, 15 (2) : 314 - 324.
  • 6Fujisaki Y, Ikeda M, Miki K. Robust stabilization of large space structures via displacement feedback [ J]. IEEE Transactions on Automatic Control, 2001, 46(12) : 1993 -1996.
  • 7Nagashio T, Kida T. Robust control of flexible mechanical system by utilizing symmetry and its application to large space structures [ C ]. The IEEE International Conference on Control Applications, Taipei, China, September 2 -4, 2004.
  • 8Li Z, Bainum P M. Momentum exchange: feedback control of flexible spacecraft maneuvers and vibration [ J ]. Journal of Guidance, Control, and Dynamics,1992(15) : 1354-1360.
  • 9Li Z, Bainum P M. Vibration control of flexible spacecraft integrating a momentum exchange controller and a distributed piezoelectric Actuator [ J ]. Journal of Sound and Vibration, 1994, 177 (4) :539 -553.
  • 10Hu Q L, Ma G F. Vibration during attitude maneuvers [ J ] and Dynamics, 2005, 28(2): suppression of flexible spacecra~ Journal of Guidance, Control, 377 -380.

共引文献47

同被引文献169

引证文献38

二级引证文献59

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