期刊文献+

基于LFT的鲁棒变增益控制的降保守性设计 被引量:2

Reduction of Conservatism in Robust Gain-Scheduling Control Based on LFT
下载PDF
导出
摘要 研究了线性变参数系统的鲁棒变增益控制,介绍了基于LFT的鲁棒变增益控制的思想;针对目前基于LFT的鲁棒变增益控制的保守性,采用全块标量矩阵,通过减少对全块标量矩阵的结构约束;提出了一种保守性更小的稳定性判据,并且利用消元定理,给出了基于LFT的鲁棒变增益的输出反馈控制器存在的条件;同时给出了控制器的构建方式,并且给出了求解控制器的迭代LMI算法。仿真结果表明,所提方法能够得到更小的性能指标,比现有方法具有更小的保守性,验证了方法的有效性。 Robust gain-scheduling based on LPV system was studied, and the LFT robust gain-scheduling method was introduced. Due to the conservatism of the current method, a new stability criterion based on full block matrixes which have relaxed the structure restriction was proposed. With the help of elimination lemma. the sufficient condition of the dynamic output controller to robust gain-scheduling based on LFT exist was given, and the algorithm to construct controller based on iterative LMI was given. Finally, the result of simulation showed that the proposed method could give smaller performance index and had less conservative validity, the valid was verified
出处 《海军航空工程学院学报》 2011年第5期533-538,共6页 Journal of Naval Aeronautical and Astronautical University
关键词 鲁棒变增益 线性变参数系统 线性分式变换 迭代LMI 全块标量矩阵 robust gain-scheduling linear parameter varying system linear fractional transformation iterative LMI full block scaling matrix
  • 相关文献

参考文献9

  • 1SHAMMA J S, ATHANS M. Guaranteed properties of gain scheduled control for linear parameter-varying plants[J]. Automatica, 1991,27(3):559-564.
  • 2于剑桥,刘莉,靳东亚,许承东.导弹线性分式变换模型及其在H_∞增益调度自动驾驶仪设计中的应用[J].兵工学报,2007,28(7):844-848. 被引量:8
  • 3APKARIAN P, GAHINET R A convex characterization of gain-scheduled H1 controllers[J]. IEEE Trans. Auto. Control, 1995,40(9):853-864.
  • 4PACKARD A. Gain scheduling via linear fractional trans formations[J]. System and Control Letters, 1994, 22(2):79-92.
  • 5SCHERER C W. LPV control and full block multipliers[J]. Automatic, 2001,37(3):361-375.
  • 6WU E DONG K synthesis for LFT Robust and gain-schduling H2 parameter-dependent system[C]// American Control Conference. USA, Portland, 2005 2851-2856.
  • 7SCHERER C W. Robust mixed control and LPV control with full block scalings[J]. Recent Advance of LMI Methods in Control, 2000,12(4): 187-207.
  • 8GHAOUI L E, OUSTRY F, AITRAMI M. A cone complementarity linearization algorithm for static output-feedback and related problems[J]. IEEE Trans. Auto. Control, 1997,42(8): 1171-1176.
  • 9WANG F, BALAKRISHNAN V. Improved stability analysis and gain-scheduled controller synthesis for parameter-dependent system[J]. IEEE Trans. Auto. Control, 2002,47(5):720-734.

二级参考文献7

  • 1钱杏芳,等.导弹飞行力学[M].北京:北京理工大学出版社.1999.
  • 2Breton M R.Gain-scheduled aircraft control using linear parameter-varying feedback[D].Ohio:Air Force Institute of Technology,1996:1-7.
  • 3Belcastro C M,Chang B C.LFT formulation for multivariate polynomial problems[C].Proceedings of the American Control Conference,Philadelphia,Pennsylvania,1998:1002-1007.
  • 4Cockburn J,Morton B.Linear fractional representations of uncertain systems[J].Automatica,1997,33(7):1263-1271.
  • 5Belcastro C M.Parametric uncertainty modeling:an overview[C].Proceedings of the American Control Conference,Philadelphia,Pennsylvania,1998:992-996.
  • 6Packard A.Gain scheduling via linear fractional transformations[J].System and Control Letters,1994,22(2):79-92.
  • 7Apkarian P,Gahinet P.A convex characterization of gain-scheduled H∞ controllers[J].IEEE Transactions on Automatic Control,1995,40:853-864.

共引文献7

同被引文献20

引证文献2

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