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变拓扑柔性多体系统接触碰撞动力学研究 被引量:3

STUDY ON CONTACT/IMPACT DYNAMICS OF FLEXIBLE MULTIBODY SYSTEM WITH TOPOLOGY VARIABLE
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摘要 在实际工程领域中存在着大量接触碰撞等非连续动力学问题,现有的解决柔性多体系统连续动力学过程的建模理论与方法,已经无法解决或无法很好解决这些问题.本文基于变拓扑思想,提出了附加接触约束的柔性多体系统碰撞动力学建模理论;通过设计柔性圆柱杆接触碰撞实验,验证了所提出附加约束接触碰撞模型的有效性;针对柔性多体系统全局动力学仿真面临时间和空间的多尺度问题,提出多变量的离散方法,从而提高了柔性多体系统非连续动力学的仿真效率. There is an increasing number of discontinuous dynamics problems, such as contact and impact, in the engineering field. The known modelling theories and methods, which are used to solve the continuous dynamics of flexible multibody systems, are not able to solve those problems or to solve those problems perfectly. In this paper, an appending constraint method was proposed to solve the contact/impact dynamics of flexible multibody system based on the idea of topology variable. The impact experiment of flexible bars was designed to verify the validity of the proposed method. At last, a multi-variable method was proposed to solve the multi-scale problems of time and space when the global simulation of the discontinuous dynamics of flexible multibody systems was carried out, and the computational efficiency of the global simulation of the discontinuous dynamics of flexible multibody systems was improved by using this method.
出处 《动力学与控制学报》 2013年第1期5-11,共7页 Journal of Dynamics and Control
基金 国家自然科学基金重点项目(11132007 11202126) 博士点基金(20090073110009) 上海市自然科学基金(11ZR1417000)资助~~
关键词 柔性多体系统 接触碰撞 变拓扑 数值仿真 实验研究 flexible multibody sytem, contact/impact, topology variable, numerical simulation, experimental research
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参考文献4

  • 1Diolaiti N, Melchiorri C, Stramigioli S. Contact impedance estimation for robotic systems. 1EEE Transactions on Robot- ics, 2005, 21(5) : 925 -935.
  • 2Zhang Y, Sharf I. Experimental validation of nonlinear compliant contact force models. Proceedings of the ASME 2007 International Design Engineering Technical Confer- ences & Computers and Information in Engineering Confer- ence, September 4 - 7, 2007 , Las Vegas, Nevada, USA.
  • 3Thomas Klisch. Contact mechanics in muhibody system. Multibody System Dynamics, 1998, 2 (4) : 335 - 354.
  • 4董富祥.刚柔耦合多体系统碰撞动力学建模理论与实验研究[博士学位论文].上海:上海交通大学,2010.

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  • 2吴鹏,马成江,朱国民.直升机吊挂飞行动力学建模与分析[J].直升机技术,2010(4):33-36. 被引量:9
  • 3Brown O, Eremenko P. Fractionated space architectures a vision for responsive space. The 4th Responsive Space Conference Paper RS4- 2006-1002, 2006.
  • 4Wigbert E Automated Rendezvous and Docking of Space-craft. Cambridge: Cambridge University Press, 2003.
  • 5Adams J, Robertson A, Zimmerman K, et al. Technologies for spacecraft formation flying. ION GPS-96 Conference, September, 1996. 1321-1330.
  • 6Bauer E Bristow J, Folta D, et al. Satellite formation flying using an innovative autonmous control system (AutoCon) environment. In: Proc of AIAA/AAs Astrodynamics Specialists Conference, (New Orleans, LA), Aug, 1997. 657-666.
  • 7Jeyakumar D, Nageswara RB. Dynamics of satellite separation system. Journal of Sound and Vibration, 2006, 29(7): 444-455.
  • 8Flores P, Ambrosio J, Claro JCP, et al. Spatial revolute joints with clearances for dynamic analysis of multi-body systems. Journal of Multi-Body Dynamics, 2006, 220(4): 257-271.
  • 9Tian Q, Liu C, Machado M, et al. A new model for dry and lubri- cated cylindrical joints with clearance in spatial flexible multibody systems. Nonlinear Dynamics, 2011, 64(1-2): 25-47.
  • 10Zhao Y, Bai ZE Effects of clearance on deployment of solar panels on spacecraft system. Transactions of the Japan Society for Aero- nautical and Space Sciences, 2011, 53(182): 291-295.

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