分体式超大口径空间遥感器技术及其发展

杨会生; 张学军; 李志来; 鲍赫; 樊延超

doi:10.3788/OPE.20182606.1287

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分体式超大口径空间遥感器技术及其发展

现代应用光学 | 更新时间：2020-07-05

- 分体式超大口径空间遥感器技术及其发展
- Technology and development of deployable segmented ultra-large-aperture space remote sensors
- 光学精密工程 2018年26卷第6期页码：1287-1298
- 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 100049
- 作者简介：
  
  [ "杨会生(1982-), 男, 河北献县人, 硕士, 助理研究员, 2007年、2009年于哈尔滨工业大学分别获得学士、硕士学位, 主要从事空间光学遥感器光机结构及精密机械等方面的研究。E-mail:yanghuisheng@126.com" ]
  张学军(1968-), 男, 吉林长春人, 博士, 研究员, 博士生导师, 主要从事空间光学系统超精加工与检测和空间光学遥感器总体技术等方面的研究工作。E-mail:zxj@ciomp.ac.cn ZHANG Xue-jun, E-mail:zxj@ciomp.ac.cn
- 基金信息：
  
  国家973重点基础研究发展计划资助项目(2016YFB0500100)
- DOI：10.3788/OPE.20182606.1287
  中图分类号： TP79;TH703
- 收稿日期：2017-12-06，
  
  录用日期：2018-1-8，
  
  纸质出版日期：2018-06-25
- 稿件说明：
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杨会生, 张学军, 李志来, 等. 分体式超大口径空间遥感器技术及其发展[J]. 光学精密工程, 2018,26(6):1287-1298.

Hui-sheng YANG, Xue-jun ZHANG, Zhi-lai LI, et al. Technology and development of deployable segmented ultra-large-aperture space remote sensors[J]. Optics and precision engineering, 2018, 26(6): 1287-1298.
杨会生, 张学军, 李志来, 等. 分体式超大口径空间遥感器技术及其发展[J]. 光学精密工程, 2018,26(6):1287-1298. DOI： 10.3788/OPE.20182606.1287.

Hui-sheng YANG, Xue-jun ZHANG, Zhi-lai LI, et al. Technology and development of deployable segmented ultra-large-aperture space remote sensors[J]. Optics and precision engineering, 2018, 26(6): 1287-1298. DOI： 10.3788/OPE.20182606.1287.

摘要

针对天文观测和国防建设对超大口径空间遥感器的迫切需求，对分体式超大口径空间遥感器技术进行了系统研究。首先阐述了该技术的主要实现方式和基本原理，主要包括分体自重组系统，分体空间装调系统和分体空间制造系统，概述了不同实现方式的发展历史和研究现状；总结了各种实现方式的结构特点和核心技术，并对其发展前景进行了分析和展望。最后，根据我国未来空间探测的实际需求，结合现阶段技术水平和未来的技术潜力，给出了重点发展分体自重组技术，积累完善分体空间装调技术，布局分体空间制造技术的建议。

Abstract

In view of the urgent need of astronomical observation and national defense construction for the ultra-large-aperture space remote sensors

this study systematically researches the technology of deployable segmented ultra-large-aperture space remote sensors. Three kinds of technological routes are presented

including an automatic-deployment segmented system

in-space assembly segmented system and in-space manufacture system

and the basic principle is introduced. Then

the development history and research process are described

the core technology and structure characteristics are summarized

and the development prospects are analyzed. Finally

according to the actual requirements of our future space exploration

some suggestions

including focusing on the development of the technology of the automatic-deployable segmented system

accumulating the technology of the in-space assembly segmented system

programming the technology of the in-space manufacture system strategically

are provided based on the current technical conditions and development trends.

关键词

Keywords

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