基于在轨更换的光学载荷定位机构研究

李清雅; 赵伟国; 石震; 王严; 杨立保

doi:10.3788/OPE.20192710.2233

您当前的位置：

首页 >

文章列表页 >

基于在轨更换的光学载荷定位机构研究

微纳技术与精密机械 | 更新时间：2020-08-13

- 基于在轨更换的光学载荷定位机构研究
- Research on positioning mechanism of optical device based on on-orbit replacement
- 光学精密工程 2019年27卷第10期页码：2233-2240
- 作者机构：
  
  1.中国科学院长春光学精密机械与物理研究所, 吉林长春130033
  2.中国科学院大学, 北京 100039
- 作者简介：
  
  [ "李清雅(1993-)，女，黑龙江大庆人，博士研究生，主要从事在轨维护及航天器结构设计方面的研究。E-mail：liqing_ya@163.com" ]
  杨立保(1972-)，男，河北唐山人，博士，副研究员，主要从事光学仪器总体设计方面的研究以及空间光学载荷在轨维护技术研究。E-mail：yanglibao228@163.com YANG Li-bao, yanglibao228@163.com
- 基金信息：
  
  中国科学院战略性先导科技专项(A类)资助项目(XDA17010205)
- DOI：10.3788/OPE.20192710.2233
  中图分类号： V476
- 收稿日期：2019-03-13，
  
  录用日期：2019-4-15，
  
  纸质出版日期：2019-10-15
- 稿件说明：
移动端阅览
李清雅, 赵伟国, 石震, 等. 基于在轨更换的光学载荷定位机构研究[J]. 光学精密工程, 2019,27(10):2233-2240.

Qing-ya LI, Wei-guo ZHAO, Zhen SHI, et al. Research on positioning mechanism of optical device based on on-orbit replacement[J]. Optics and precision engineering, 2019, 27(10): 2233-2240.
李清雅, 赵伟国, 石震, 等. 基于在轨更换的光学载荷定位机构研究[J]. 光学精密工程, 2019,27(10):2233-2240. DOI： 10.3788/OPE.20192710.2233.

Qing-ya LI, Wei-guo ZHAO, Zhen SHI, et al. Research on positioning mechanism of optical device based on on-orbit replacement[J]. Optics and precision engineering, 2019, 27(10): 2233-2240. DOI： 10.3788/OPE.20192710.2233.

摘要

为了实现空间望远镜大型光学载荷的在轨更换，设计了一种能够实现在轨快速拆装的定位机构，并针对其核心问题即在轨重复定位精度进行了研究。首先，选定了一种能够避免热应力的运动学定位方式。在此基础上设计了定位机构，并根据刚体的微小角位移是矢量并符合矢量合成法则的原则，利用角位移矢量合成的方法推导出了光学载荷的转角数学模型；然后，设计杆系结构模拟了光学载荷及其框架，同时为了模拟光学载荷在轨拆装的微重力环境，利用微重力模拟的常用方法悬吊法设计了悬吊装置，以实现光学载荷模块的重力卸载；最后，搭建了试验检测环境，对光学载荷模块进行重复拆装试验，利用经纬仪及数显千分表进行检测，并处理试验结果得到了重复定位误差值。结果表明，光学载荷模块的重复安装转角误差最大为±28.8″，平移误差最大为±0.057 mm。本文研究能够为在轨可更换载荷定位机构的设计提供参考，具有理论意义和应用价值。

Abstract

A kind of positioning mechanism that ensured large optical device could be replaced quickly was designed in order to realize the on-orbit replacement of a large optical device

and the accuracy of the re-orientation of the device was studied as the key issue of on-orbit replacement. Firstly

a kinematic positioning method that can prevent thermal stress was studied. On the basis of this method

the positioning mechanism was designed. And according to the principle that the microrotation angles of the rigid body are vectors and meets the vector synthesis rule

the mathematical model of the rotation angle of the optical device was derived by the method of synthesizing angular displacement vectors. Then

the beam structure simulating the optical device and frame was designed

simultaneously suspending device was designed based on the common sling suspension method of unloading gravity to imitate the replacement of the device on-orbit in microgravity. Finally

the experimental environment was set up

and the optical device module was repeatedly inserted and taken out of the frame to measure the re-orientation accuracy by theodolites and digital micrometers. The results show that the maximum repeated installation rotational error of the optical device module is ±28.8″ while the maximum translation error is ±0.057 mm. This study provides reference for the design of the positioning mechanism of an on-orbit replaceable device

and has theoretical significance and application value.

关键词

Keywords

references

陈小前, 袁建平, 姚雯, 等.航天器在轨服务技术[M].北京:中国宇航出版社, 2009.

CHEN X Q, YUAN J P, YAO W, et al .. The Technology of On-orbit Spacecraft Servicing [M]. Beijing: Chinese Astronautics publishing company, 2009. (in Chinese)

马聪.在轨更换单元组件设计及动力学分析[D].哈尔滨: 哈尔滨工业大学, 2014.

MA C. The Design and Dynamics Analysis of the Orbital Replacement Unit Assembly [D]. Harbin: Harbin Institute of Technology, 2014. (in Chinese)

ROBERT B F. Orbital Express program summary and mission overview.[J]. SPIE , 2008, 6958: 695803.

KEVIN H, JAMES J, MALOOLM N, et al .. NASA, Hubble 2009:Science year in Review [M]. Greenbelt: NASA Pub, 2010.

洪津, 王征云, 胡亚东, 等.星载红外探测器组件寿命试验研究及系统设计[J].光学精密工程, 2018, 26(5): 1148-1155.

HONG J, WANG ZH Y, HU Y D, et al .. Research of life test and design of system for satellite-borne infrared detector assembly[J]. Opt. Precision Eng ., 2018, 26(5): 1148-1155. (in Chinese)

邵亮, 杨飞, 王富国, 等. 1.2 m轻量化SiC主镜支撑系统优化设计[J].中国光学, 2012, 5(3): 229-234.

SHAO L, YANG F, WANG F G, et al .. Design and optimization of supporting system for 1.2 m lightweight SiC primary mirror[J]. Chinese Optics , 2012, 5(3): 229-234. (in Chinese)

马聪, 李威, 张远清, 等.深空探测遥感相机支撑结构设计[J].红外与激光工程, 2018, 47(6): 184-189.

MA C, LI W, ZHANG Y Q, et al .. Design of support structure for deep space detection remote sensing camera[J]. Infrared and Laser Engineering , 2018, 47(6): 184-189. (in Chinese)

刘强.超宽覆盖空间遥感器底部支撑结构的研究[D].长春: 中国科学院研究生院, 2013. http://www.irgrid.ac.cn/handle/1471x/681417?mode=full&submit_simple=Show+full+item+record

LIU Q. Research on the Bottom Support Structure of the Extra-wide Coverage Remote Senor [D]. Changchun: Graduate School of Chinese Academy of Sciences, 2013. (in Chinese)

李钰鹏, 王智, 沙巍, 等. Bipod反射镜支撑结构的柔度计算与分析[J].光学精密工程, 2018, 26(7): 1691-1697.

LI Y P, WANG ZH, SHA W, et al .. Flexibility calculation and analysis of Bipod reflector support structure[J]. Opt. Precision Eng ., 2018, 26(7): 1691-1697. (in Chinese)

原帅, 张景旭, 王富国, 等.大口径主镜的侧向定位系统[J].光学精密工程, 2017, 25(10): 2564-2571.

YUAN SH, ZHANG J X, WANG F G, et. al .. Lateral positioning system for large aperture primary mirror[J]. Opt. Precision Eng ., 2017, 25(10): 2564-2571. (in Chinese)

王辉.极紫外光刻系统物镜光学元件的支撑与分析[J].中国光学与应用光学, 2010, 3(6): 598-604.

WANG H. Objective optical mounts and analysis for EUVL[J]. Chinese journal of optics and applied optics , 2010, 3(6): 598-604. (in Chinese)

谢传锋, 等.动力学[M].北京:高等教育出版社, 2006.

XIE CH F, et al .. Dynamics [M]. Beijing: Higher education press, 2006. (in Chinese)

项升.悬吊式宇航员低重力模拟系统动力学建模及控制分析[D].哈尔滨: 哈尔滨工业大学, 2015. http://cdmd.cnki.com.cn/Article/CDMD-10213-1015982469.htm

XIANG SH. Dynamic Modeling and Control Analysis for Suspended Type Astronauts Low-gravity Simulation System [D]. Harbin: Harbin Institute of Technology, 2015. (in Chinese)

高云国, 王超, 江展洪, 等.光电跟踪设备载车平台的重复定位精度[J].光学精密工程, 2015, 23 (5), 1322-1328.

GAO Y G, WANG CH, JIANG ZH H, et al .. Re-orientation accuracy of vehicle-born photoelectric tracking equipment[J]. Opt. Precision Eng ., 2015, 23 (5): 1322-1328. (in Chinese)

马宏, 王金波.仪器精度理论[M].北京:北京航空航天大学出版社, 2014.

MA H, WANG J B. Instrument Accuracy Theory [M]. Beijing: Beihang university press, 2014. (in Chinese)

浏览量

113

下载量

CSCD

文章被引用时，请邮件提醒。

提交

工具集

关联资源

应用于Φ300 mm平面反射镜的精密二维转台轴系设计

高时空分辨率动态星模拟器设计

空间大口径单体反射镜计量卸荷支撑研制中的关键技术

基于混合灵敏度的空间望远镜次镜调整机构鲁棒控制

用于太空望远镜的大口径薄膜菲涅尔衍射元件