期刊文献+

基于交叉Gram矩阵的离散周期系统模型降阶 被引量:2

Model Order Reduction Based on Cross Gramians of Discrete Periodic Systems
下载PDF
导出
摘要 针对单输入单输出离散周期系统的模型降阶问题,提出了基于交叉Gram矩阵的奇异值分解截断模型降阶方法。首先,定义了离散周期系统的交叉Gram矩阵,并将离散线性时不变系统交叉Gram矩阵的相关性质推广到离散周期系统中。其次,基于交叉Gram矩阵,通过矩阵奇异值分解截断方法得到降阶系统。再次,利用输出多相采样传递函数证明了该方法与传统平衡截断方法的等价性。最后,数值算例验证了基于交叉Gram矩阵奇异值分解截断模型降阶方法是行之有效的。 On the basis of cross gramians,a singular value decomposition(SVD)truncation model order reduction method is proposed for the model order reduction of single input and single output(SISO)discrete periodic systems.Firstly,the cross gramians of the discrete periodic systems were defined,and the correlative properties of the cross gramians of the discrete linear time invariant systems were generalized to discrete periodic systems.Then,the cross gramians were employed to obtain the reduced order system and the matrix SVD truncation method was established.Moreover,the equivalence between the proposed method and the traditional balanced truncation method was demonstrated by the use of output sampling polyphase(OSP)transfer function.Finally,a numerical example illustrates the effectiveness of SVD truncation model order reduction method.
作者 孙丽丽 李延鹏 蒋耀林 SUN Li-li;LI Yan-peng;JIANG Yao-lin(College of Mathematics and System Sciences,Xinjiang University,Urumqi Xinjiang 830046,China;School of Mathematics and Statistics,Xi’an Jiaotong University,Xi’an Shanxi 710049,China)
出处 《计算机仿真》 北大核心 2020年第6期268-272,共5页 Computer Simulation
基金 国家自然科学基金(11871393 61663043)。
关键词 模型降阶 周期系统 奇异值分解 Model order reduction Periodic systems Singular value decomposition
  • 相关文献

参考文献3

二级参考文献36

  • 1邱志成.航天器挠性板系统的模态分析和模型降阶[J].航天控制,2006,24(3):89-96. 被引量:8
  • 2张明廉.飞行控制系统[M].北京:航空工业出版社,1994.41-45.
  • 3M R Waszak, D K Schmidt. Flight Dynamics of Aeroelastic Vehicles[J]. Journal of Aircraft, June 1988, 25(6) :563 -571.
  • 4Xiaohong Li. Robust Control of Flexible Aircraft with Uncertainty [ D]. Wichita State University ,USA, May 2002.
  • 5M R Waszak, C S Buttrill and D K Schmidt. Modeling and Model Simplification of Aeroelastic Vehicles : An Overview [ R ], NASA Technical Memorandum 107691, September 1992.
  • 6D K Schmidt, D L Raney. Modeling and Simulation of Flexible Flight Vehicles[ J]. Journal of Guidance, Control and Dynamics,May -June 2001,24(3 ).
  • 7B C Moore. principal component analysis in linear system: controllability, observability and model reduction [ J ]. IEEE Trans. on Automatic Control, 1981,26 ( 1 ) : 17:31.
  • 8Giuseppe Rega,Hans Troger.Dimension Reduction of Dynamical Systems: Methods, Models, Applications[J]. Nonlinear Dynamics . 2005 (1-3)
  • 9S. C. SINHA,SANGRAM REDKAR,VENKATESH DESHMUKH,ERIC A. BUTCHER.Order Reduction of Parametrically Excited Nonlinear Systems: Techniques and Applications[J]. Nonlinear Dynamics . 2005 (1-3)
  • 10C. Sansour,P. Wriggers,J. Sansour.A finite element post-processed Galerkin method for dimensional reduction in the non-linear dynamics of solids. Applications to shells[J]. Computational Mechanics . 2003 (1-2)

共引文献12

同被引文献1

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