期刊文献+

磁流变阻尼器冲击载荷下动态响应峰值建模与分析 被引量:1

Dynamic Response Peak Values Modeling and Analysis for Magneto-rheological Damper Subject to Impact Loading
下载PDF
导出
摘要 运用基于核函数变换的多元累加模型和偏最小二乘回归方法,建立了磁流变阻尼器在冲击载荷下的冲击力和冲击加速度的峰值关于冲击质量、冲击速度和输入电流三个影响因素的线性模型。模型的回归数据和预测数据与实验数据的比较结果证明,该动态模型不仅有较高的回归精度,而且有较好的稳健性。 Exerting multivariate additive model based on kernel function and partial least-squares regression, the linear model of dynamic response peak values, such as impact force and impact acceleration of magneto-rheological damper, subject to impact mass,impact velocity and input current was established. A comparison of regressive datum and predictive datum of established model with testing datum demonstrates the dynamic model possesses higher regression precision, and beares better robustness.
出处 《中国机械工程》 EI CAS CSCD 北大核心 2008年第23期2807-2811,共5页 China Mechanical Engineering
基金 新世纪优秀人才基金资助项目(NCET-04-0766)
关键词 磁流变阻尼器 冲击载荷 偏最小二乘回归 核函数 magneto- rheological damper impact load partial least- squares regression kernel functions
  • 相关文献

参考文献10

  • 1Ahmadian M,Poynor J C. An Evaluation of Magneto Rheological Dampers for Controlling Gun Recoil Dynamics[J]. Shock and Vibration, 2001,8: 147- 155.
  • 2Ericksen E O, Gordaninejad F. A Magneto--rheological Fluid Shock Absorber for an Off--road Motorcycle[J]. International Journal of Vehicle Design, 2003,33(1) :139-152.
  • 3Choi Y T, Wereley N M. Vibration Control of a Landing Gear System Featuring Electrorheological/ Magnetorheological Fluids[J]. Journal of Aircraft, 2003,40(3) : 432-439.
  • 4Norris J A, Ahmadian M. Behavior of Magneto-- rheological Fluids Subject to Impact and Shock Loading[C]//Proc. of IMECE ' 03. Washington D C,2003 :199-204.
  • 5Wang J,Li Y C. Dynamic Simulation and Test Verification of MR Shock Absorber under Impact Load [J]. Journal of Intelligent Material Systems and Structure,2006,17(4):309-314.
  • 6侯保林,MEHDI Ahmadian.冲击载荷作用下磁流变阻尼器的建模与分析[J].机械工程学报,2006,42(4):173-178. 被引量:17
  • 7钟志华,张维刚.汽车碰撞安全技术[M].北京:机械工业出版社,2005.
  • 8Lord Corporation. Lord Technical Data-- RD-- 1005 --3 Damper[EB/OL]. [2007-10-12]. http://mutualhosting, com/- lordfulfillment/upload/DS7017. pdf.
  • 9孟洁,王惠文,黄海军,苏建宁.基于核函数变换的PLS回归的非线性结构分析[J].系统工程,2004,22(10):93-97. 被引量:10
  • 10Rosipal R,Trejo L J. Kernel Partial Least Squares Regression in Reproducing Kernel Hilbert Space [J].Journal of Machine Learning Research,2001,2 (6):97-123.

二级参考文献18

  • 1高树滋 陈运生 等.火炮反后坐装置设计[M].北京:兵器工业出版社,1995..
  • 2严士健 刘秀芳 徐承彝.概率论与数理统计[M].北京:高等教育出版社,1993.155-167.
  • 3CARLSON J D. What makes a good MR fluid[J]. Journal of Intelligent Material Systems & Structures, 2002, 13(7-8):431-435.
  • 4CARLSON J D. Critical factors for MR fluids in vehicle systems[J]. Intemational Joumal of Vehicle Design, 2003,33(1-3): 207-217.
  • 5XU Z D, SHEN Y P. Intelligent bi-state control for the structure with magnetorheological dampers[J]. Journal of Intelligent Material Systems & Structures, 2003, 14(1):35-42.
  • 6GORDANINEJAD F, KELSO SHAWN P. Magneto-rheological fluid shock absorbers for HMMWV[C]//Proceedings of SPIE - The International Society for Optical Engineering, Society of Photo-Optical Instrumentation Engineers, 2000, USA, 3 989: 266-273.
  • 7CHOI Y T, WERELEY NORMAN M. Vibration control of a landing gear system featuring electrorbeological/magneto- rheological fluids[J]. Journal of Aircraft,2003, 40(3): 432-439.
  • 8AHMAI)IAN M, POYNOR C. An evaluation of magneto rheological dampers for controlling gun recoil dynamics[J]. Shock and Vibration, 2001, 8: 147-155.
  • 9JAMES A N, AHMADIAN M. Behavior of magneto-rheological fluid subject to impact and shock loading[C]//2003 ASME International Mechanical Engineering Congress, Washington, D.C., 2003: 115-121.
  • 10LEE D Y, WERELEY NORMAN M. Quasi-steady Herschel-Bulkley analysis of electro- and magneto-rheological flow mode dampers[J]. Journal of Intelligent Material Systems & Structures, 2000, 10(10):761-769.

共引文献51

同被引文献11

  • 1夏品奇,岳海龙.磁流变阻尼器性能及振动控制[J].航空动力学报,2004,19(3):305-309. 被引量:6
  • 2Krabacher W E. A Review of Aircraft Landing Gear Dynamics, AGARD- R- 800[R]. Aneelle: Advisory Group for Aerospace Research and Development, 1995.
  • 3Glaser J, Hrycko G. Landing Gear Shimmy- De Havilland' s Experience, AGARD- R- 800[R]. Ancelle.. Advisory Group for Aerospace Research and Development, 1995.
  • 4Jr Spencer B F,Nagarajaiah S. State of the Art of Structural Control [J]. Journal of Structural Engineering, 2003,129 (7) : 845-856.
  • 5Jansen L M, Dyke S J. Semi-active Control Strategies for MR Dampers: a Comparative Study[J]. ASCE Journal of Engineering Mechanics, 2000,126 (8) : 795-803.
  • 6Yang G,Jr Spencer B F,Carlson J D,et al. Large-scale MR Fluid Dampers: Modeling and Dynamic Performance Considerations[J]. Engineering Structures, 2002,24 (3) :309-323.
  • 7Batterbee D C,Sims N D,Stanway R,et al. Magnetorheologicat Landing Gear:2. Validation Using Experimental Data[J]. Smart Materials and Structures, 2007,16 (6) : 2441-2452.
  • 8Gerhard S. Shimmy Analysis of a Simple Aircraft Nose Landing Gear Model Using Different Mathematical Methods[J]. Aerospace Science and Technology, 1997,8(1) : 545-555.
  • 9McClamroch N H, Gavin H P. Closed Loop Structural Control Using Electrorheological Dampers[C]//Proceedings of the American Control Conference, 1995. Seattle,WA ,1995..4173-4177.
  • 10顾宏斌,丁运亮,姚志,章建华,熊梅,龚良国.飞机机轮摆振的数字仿真[J].航空学报,2001,22(4):362-365. 被引量:11

引证文献1

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