期刊文献+

一种微位移促动器的设计和检测 被引量:9

Design and test of a micro -displacement actuator
下载PDF
导出
摘要 设计制造了一套微位移促动器并进行了检测。比较了常用的实现高精度、大行程的微位移机构的工程方法,并结合大天区面积多目标光纤光谱天文望远镜(LAMOST)微位移调节机构的实现原理,采用步进电机驱动减速器、精密丝杆型式,及高精度的杠杆缩放结构,实现了高精度、大行程的微位移促动器。根据该传动机构的特点,对机构的误差进行了分析,通过计算机查表校正丝杆的传动误差。双频激光干涉仪的检测结果表明该微位移促动器在行程范围内灵敏度达到了201nm±48nm,步长为10μm,单向精度达到了标准偏差237nm。 A set of micro-displacement actuator was developed and tested for the large area multi-object fiber spectroscopic telescope (LAMOST). Conventional techniques for micro-displacement mechanism with high accuracy and long travel in engineering applications are studied. In view of implementation principle of the active-motion mechanism in the LAMOST, integrated with precision lever, a scheme of stepper motor, harmonic reducer and ball screw, the goal of both high accuracy and long travel is realized. The origins of error are investigated, before a computer look-up table is designed to calibrate transmission error and to improve absolute accuracy of the actuator. Measured with laser interferometer in laboratory, the actuator confirms itself that it can be used as micro-displacement actuator of the LAMOST, thanks to its resolution of 201 nm ± 48 nm and unidirectional accuracy of 237 nm (standard deviation) at a step of 10 μm.
出处 《光学精密工程》 EI CAS CSCD 北大核心 2005年第3期332-338,共7页 Optics and Precision Engineering
基金 "大天区多目标光纤光谱天文望远镜国家重大科学工程项目"
关键词 微位移促动器 误差分析 校正 检测 传动机构 Error analysis Error correction Interferometers Stepping motors Table lookup Telescopes
  • 相关文献

参考文献8

二级参考文献13

  • 1吴德隆.航天Smart结构与材料的开发与进展——21世纪航天技术展望[J].导弹与航天运载技术,1996(4):1-13. 被引量:13
  • 2[6]DONG S X, LI L T, GUI Z L,et al. A new type of linear piezoelectric stepper motor[J]. IEEE Transaction on Components, Packaging, and Manufacturing Technology part A, 1995,18(2) :257-260.
  • 3[7]SETTERINGTON R E,彭浩波,Van RANDERAAT J.压电陶瓷[M].北京:科学出版社,1981.SETTERINGTON R E, PENG H B, Van RANDERAAT J. Piezoceramics[M]. Beijing: Science Press, 1981.
  • 4Zhang B, Zhu Z Q. Developing a linear piezomotor with nanometer resolution and high stiffness[ J ]. IEEE/ASME Transactions on Mechatronics, 1997, 2(1): 22 - 28.
  • 5Pernette E, Clavel R. Ultra-accurate actuator with long travel[A]. In:SPIE,Vol. 3202[C]. 1998.54 - 65.
  • 6Her I. Methodology for compliant mechanism design[D]. America: Purdue university, 1986.
  • 7Breguet J M, Perez R, Bergander A, et al. Piezoactuators for motion control from centimeter to nanometer [ A ]. In: Proceedings of the 2000 IEEE/RSJ International Conference on Intelligent Robots and Systems[C]. 2000.
  • 8Chang S H, Du B C. A precision piezodriven micropositioner mechanism with large travel range[ J ]. Review of Scientific Instruments, 1998, 69(4): 1785 - 1791.
  • 9Kallio P, Lind M, Kojola H, et al. An actuation system forparallel link micromanipulators [ A]. In: Proceedings of the 1996 IEEE/RSJ International Conference on Intelligent Robots and Systems[C]. Osaka, Japan, 1996. 856 - 862.
  • 10阎绍泽,吴德隆.空间飞行器自适应结构技术[J].导弹与航天运载技术,1997(6):24-35. 被引量:7

共引文献115

同被引文献88

引证文献9

二级引证文献41

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