期刊文献+

柔性机械臂模型非约束模态降维绝对误差准则 被引量:1

Absolute Error Selection Criteria of Unconstrained Mode for Flexible Manipulator Dynamics Model Dimension Reduction
下载PDF
导出
摘要 描述柔性结构振动的非约束模态展开方法仅考虑结构参数而不考虑外部作用力,当外部驱动力频率与非约束模态的某几阶频率相等或者相近时,这样的处理将影响动力学响应的近似精度。针对此问题,且考虑到任意驱动力都可以用傅里叶分析的方法将其等效为无穷多个正弦力的叠加,提出了一种正弦力作用下基于非约束模态降维的绝对误差准则。采用有限元法描述柔性机械臂的弹性变形,应用拉格朗日法建立其动力学方程,并用非约束模态降维模型与其作对比,仿真验证了所提出的非约束模态选取准则的正确性。 The unconstrained mode dynamics dimension reduction methods only consider the structural parameters without analyzing the impact of the control force. Due to any control force can be equivalent to the superposition of an infinite number of sinusoidal force by Fourier analysis method, an unconstrained mode selection criteria under sinusoidal force based on the absolute error was presented. The elastic deformation of flexible manipulator was modeled by using the finite element (FE) method. The dynamics model of flexible manipulator was deduced by using the Lagrange approach. The solution of unconstrained mode was used for dimension reduction of the dynamics equations. The dimension reduction of the dynamics equations and the original dynamics equations were compared. Numerical simulations demonstrate the correctness of the proposed approach.
出处 《中国空间科学技术》 EI CSCD 北大核心 2012年第2期22-28,共7页 Chinese Space Science and Technology
基金 国家自然科学基金(61171189) 航天科技创新基金(CASC200902-81)资助项目
关键词 动力学降维 有限元法 绝对误差 非约束模态 柔性机械臂 Dynamics dimension reduction Finite element method Absolute error Unconstrained mode Flexible manipulator
  • 相关文献

参考文献7

二级参考文献14

  • 1刘暾,杨大明.带挠性附件卫星的模型化及截断[J].宇航学报,1989,10(4):87-95. 被引量:9
  • 2胡庆雷,马广富.挠性航天器姿态机动控制的主动振动抑制[J].振动工程学报,2005,18(3):375-380. 被引量:10
  • 3LIU Dun, WU Guang-yu. An active vibration suppression method for the flexible spacecrafts and its application [ C ]//AIAA/AAS Astrodynamics Conference. Washington: American Institute of Aeronautics and Astronautics, 1994:376 - 381.
  • 4SHAN Jin-jun, SUN Dong, LIU Dun. Design for robust component synthesis vibration suppression of flexible structures with on-off actuators [ J ]. IEEE Transactions on Robutics and Automation, 2004, 20 ( 3 ) :512 - 525.
  • 5HU Qing-lei, MA Guang-fu. Vibration suppression of flexible spacecraft during attitude maneuvers [ J ]. Journal of Guidance, Control, and Dynamics, 2005, 28 (2):377 -380.
  • 6张建英,刘暾.分力合成主动振动抑制方法和闭环反馈控制的同时设计[C]//第二十七届中国控制会议论文集.昆明:中国自动化学会控制理论专业委员会,2008:667-671.
  • 7 Enrique Barbieri.Unconstrained and constrained mode expansions for a flexibleslewing link [J].Transaction of ASME,1998,110.
  • 8 刘 暾,杨大明,张为平.On optimal control strategy of maneuver ofsatellites with flexible appendages [C].Proceedings of PISSTA,June 7-10,1987,Beijing,China.
  • 9J R Higgins.Completeness and Basis Properties of Sets of Special Functions[]..1977
  • 10P C Hughes.Modal Identities for Elastic Bodies, with Application to Vehicle Dynamics and Control, Journal of Applied Mechanics[]..1980

共引文献18

同被引文献13

引证文献1

二级引证文献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