期刊文献+

高保真气动伺服弹性系统降阶技术研究

Investigation of Model Reduction for High-order Aeroservoelasticity System
下载PDF
导出
摘要 采用高保真非定常气动力辨识技术获得的气动伺服弹性(ASE)系统时域模型往往阶次较高,不利于控制系统设计的应用。为了有效降低高阶ASE系统阶次,研究了高保真ASE模型的降阶特性,分别采用平衡截断、奇异摄动以及平衡奇异摄动模型降阶技术,结合BACT系统讨论了各种方法在ASE模型降阶中的应用情况,通过仿真比较得知,平衡奇异摄动法应用于ASE模型的降阶具有一定的优势,可以大幅降低模型阶次,且能够保证降阶模型的精度。 The high-order Aeroservoelasticity(ASE) model obtained by using the high fidelity unsteady aerodynamics from system differentiating and analyse is disadvantaged for the control system designs.In order to achieve order reduction of ASE system effectively,reduction characteristics of high fidelity ASE model have been studied in this paper.The balanced truncation reduction method,the singular perturbation method and the balanced singular perturbation method have been mentioned,and these three methods have been applied in the ASE model reduction combining with BACT system.Simulation results show that the balanced singular perturbation method used in the ASE model reduction has more advantages.It can reduce the order of model greatly,and ensure the precision.
作者 张子健 刘斌
出处 《航空计算技术》 2013年第3期34-38,共5页 Aeronautical Computing Technique
基金 陕西省自然科学基金项目资助(2013JM1015)
关键词 气动伺服弹性 模型降阶 平衡截断 奇异摄动 平衡奇异摄动 aeroservoelasticity order reduction balanced truncation singular perturbation balanced singular perturbation
  • 相关文献

参考文献8

二级参考文献16

  • 1[1]Craig R R Jr, Bampton M C C. Coupling of substructures for dynamic analysis [J]. AIAA J, 1968,6(7):1313~1319 被引量:1
  • 2[2]MacNeal R H. A hybrid method of component mode synthesis [J]. J Computers and Structures, 1971, 1(4) :581 ~601 被引量:1
  • 3[3]Rubin S. Improved component-mode representation for structural dynamic analysis [J]. AIAA J, 1975,13(8):995 ~ 1006 被引量:1
  • 4[4]Skelton R E, Hughes P C, Hablani H B. Order reduction for models of space structures using modal cost analysis [J]. J Guidance and Control,1982,5(4) :351~357 被引量:1
  • 5[5]Skelton R E, Hughes P C. Modal cost analysis for linear matrix-second order systems [J]. J Dynamics Systems,Measurement, and Control, 1980,102:151 ~ 163 被引量:1
  • 6[6]Moore B C. Principal component analysis in linear systems: Controllability, observability, and model reduction [J ]. IEEE Transaction on Automatic Control,1981 ,AC - 26:17 ~32 被引量:1
  • 7[7]Gregory C Z. Reduction of large flexible spacecraft models using internal balancing theory [ J ]. Journal of Guidance, Control, and Dynamics, 1984,7 (6) .: 724 ~732 被引量:1
  • 8[8]Spanos J T, Truha W. Selection of component modes for the simulation of flexible multibody spacecraft [ J ].Journal of Guidance, Control, and Dynamics, 1991,14(2) :278~286 被引量:1
  • 9Silva W A, Robert E B. Development of Reduced OrderModels for Aeroelastic Analysis and Flutter Prediction Using the CFL3Dv6.0 Code. AIAA paper 2002-1596 被引量:1
  • 10Dowell E H, Hall K C. Modeling of Fluid-Structure Interaction. Journal of Annual Review of Fluid Mechanics, 1993, 33: 445-490 被引量:1

共引文献28

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