天基激光测距载荷单反射镜组件柔性设计与力热稳定性分析

柳鸣; 李振伟; 李响; 康喆; 韩琳楚; 刘永志

doi:10.11728/cjss2020.06.1118

天基激光测距载荷单反射镜组件柔性设计与力热稳定性分析

doi: 10.11728/cjss2020.06.1118 cstr: 32142.14.cjss2020.06.1118

1. 中国科学院国家天文台长春人造卫星观测站长春 130117;
2. 长春理工大学空间光电技术国家与地方联合工程中心长春 130022;
3. 火箭军装备部驻天津地区军事代表室天津 300308

基金项目:

中国科学院天文光学技术重点实验室2018年开放课题资助（CAS-KLAOT-KF201805）

详细信息

作者简介:

柳鸣,E-mail:lium@cho.ac.cn

中图分类号: V254
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出版历程
- 收稿日期: 2019-10-21
- 修回日期: 2020-10-02
- 刊出日期: 2020-11-15

Flexible Design and Thermal Stability Analysis of Reflector Assembly of Space-based Laser Ranging Load

1 Changchun Observatory, National Astronomical Observatories, Chinese Academy of Sciences, Changchun 130117;
2 National and Local Joint Engineering Research Center of Space and Optoelectronics Technology,Changchun University of Science and Technology, Changchun 130022;
3 Military Representative Office Rocket Army Equipment Department in Tianjin Area, Tianjin 300308

摘要

摘要: 针对激光通信与测距一体化星间链路载荷轻小型单反射镜组件进行结构设计与力热稳定性研究，开展单反镜柔性支撑机构优化设计，根据运载力学环境与在轨力热环境工况，对反射镜组件进行光机集成分析，验证光机结构的在轨力热稳定性.分析结果表明，双层圆弧形槽口柔性支撑结构在温度拉偏后反射镜的面型精度均方根（RMS）可达λ/72，基频模态为417.93Hz，满足指标要求.进一步对反射镜组件进行动力学分析，随机振动分析结果表明，反射镜加速度响应均方根为11a_rms，满足3σ准则.通过0.2g正弦扫频试验验证了有限元模态分析相对误差为2.23%，实验结果表明，反射镜组件柔性支撑设计合理，力热稳定性分析结果基本准确可靠，满足工况要求.
- 反射镜 /
- 柔性支撑 /
- 有限元分析 /
- 力热稳定性 /
- 面形精度
Abstract: In this paper, the structure design and thermal stability of the light and small reflector component of laser communication and ranging integration satellite link load are studied. Optimization design of flexible support mechanism of reflector component is carried out. According to the working conditions and in-orbit thermal environment, the optical component integration analysis of the mirror assembly is carried out to evaluate the on-track thermal stability of the opto-mechanical structure. The analysis results show that the surface precision of the mirror with double-layer circular arc slot flexible support structure can be reached at λ/72 after temperature deflection, the fundamental frequency mode is 417.93Hz, meeting the requirements of the index. Furthermore, the dynamic analysis of the mirror assembly is carried out, the results of random vibration analysis show that the root mean square of the acceleration response of the mirror is 11a_rms and meet the 3σ criterion. Finally, a 0.2g sine sweep test proves that the relative error of the modal analysis is 2.24%, the experimental result show that the analysis results are basically accurate and reliable, that is, flexible support design is reliable to meet the requirements of the use.
- Reflector component /
- Flexible support mechanism /
- Finite element analysis /
- Thermal stability /
- Surface precision

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参考文献(12)

[1]	ZHAO Xin, NIU Junpo, LIU Yunqing, et al. Laser communication/rangign integrated technology and link characteristics in navigation satellite system[J]. Laser Optoelectron. Prog., 2015, 52(6):79-85(赵馨, 牛俊坡, 刘云清, 等. 导航卫星中激光通信/测距一体化技术及链路特性分析[J]. 激光与光电子学进展, 2015, 52(6):79-85)
[2]	CHEN Guimin, LIU Xiaoyuan, JIA Jianyuan, et al. Compliance calculation of elliptical flexure hinge[J]. Chin. J. Mech. Eng., 2006, 23(1):111-115(陈贵敏, 刘小院, 贾建援. 椭圆柔性铰链的柔度计算[J]. 机械工程学报, 2006, 23(1):111-115)
[3]	ZUO Xingyong, LIU Xiaoming. Calculation and analysis of rotational stiffness for three types of flexure hinges[J]. Chin. J. Sci. Instrum., 2006, 27(12):1725-1728(左行勇, 刘晓明. 三种形状柔性铰链转动刚度的计算与分析[J]. 仪器仪表学报, 2006, 27(12):1725-1728)
[4]	LI Zongxuan, CHEN Xue, ZHANG Lei, et al. Design of Cartwheel flexural support for a large aperture space mirror[J]. Acta Opt. Sin., 2014, 34(6):210-218(李宗轩, 陈雪, 张雷, 等. 大口径空间反射镜Cartwheel型柔性支撑设计[J]. 光学学报, 2014, 34(6):210-218)
[5]	PAROS J M, WEISBORD L. How to design flexure hings[J]. Mach. Design, 1965, 37(27):151-157
[6]	SMITH S T, BADAMI V G, DALE J S, et al. Elliptical flexure hinges[J]. Rev. Sci. Instrum., 1997, 68(3):1474-1483
[7]	LI Yupeng, WANG Zhi, SHA Wei, et al. Flexibility calculation and analysis of Bipod reflector support structure[J]. Opt. Prec. Eng., 2018, 26(7):136-142(李钰鹏, 王智, 沙巍, 等. Bipod反射镜支撑结构的柔度计算及分析[J]. 光学精密工程, 2018, 26(7):136-142)
[8]	WANG Xiaoyu, ZHOU Pingwei. Design of rectangular space mirror and its support structure[J]. J. Changchun Univ. Sci. Technol., 2017, 40(2):6-9(王晓宇, 周平伟. 长条形空间反射镜镜体及其支撑结构设计[J]. 长春理工大学学报: 自然科学版, 2017, 40(2):6-9)
[9]	ZHANG Lei, KE Shanliang, LI Lin, et al. Optimum design of ultra-light mirror series flexible support structure[J]. Acta Photon. Sin., 2018, 47(1):35-41(张雷, 柯善良, 李林, 等. 超轻反射镜串联柔性支撑结构优化设计[J]. 光子学报, 2018, 47(1):35-41)
[10]	(李行, 徐振邦, 李静秋. 空间反射镜新型柔性支撑结构设计[J]. 电子测量技术, 2014, 37(8):1-6 LI Xing, XU Zhenbang, LI Jingqiu. Design of new flexure hinge support of space reflector subassembly[J]. Electron. Meas. Technol., 2014, 37(8):1-6
[11]	JIA Xuezhi, JIN guang, JIA Jiqiang, et al. Topology optimization design for main board of lightweight space camera[J]. Chin. J. Space Sci., 2011, 31(3):395-400(贾学志, 金光, 贾继强, 等. 轻型空间相机主承力基板结构拓扑优化设计[J]. 空间科学学报, 2011, 31(3):395-400)
[12]	JIA Xuezhi, ZHANG Lei, JIN Guang. Optimum design based on full stress ruler and test for truss of space camera[J]. Chin. J. Space Sci., 2012, 33(3):35-40(贾学志, 张雷, 金光. 空间相机桁架支撑结构满应力优化设计与试验[J]. 空间科学学报, 2012, 33(3):35-40)