大口径空间相机像质的微振动频率响应计算

朱俊青; 沙巍; 陈长征; 张星祥; 任建岳

doi:10.3788/OPE.20162405.1118

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大口径空间相机像质的微振动频率响应计算

微纳技术与精密机械 | 更新时间：2020-08-13

- 大口径空间相机像质的微振动频率响应计算
- Frequency response of imaging quality by micro-vibration for large-aperture space-borne telescope
- 光学精密工程 2016年24卷第5期页码：1118-1127
- 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,中国,130033
  2. 中国科学院大学北京,100049
- 作者简介：
- 基金信息：
  
  国家863高技术研究发展计划资助项目(No.863-2-5-1-13B)()
- DOI：10.3788/OPE.20162405.1118
  中图分类号： V447.3;TH743
- 收稿日期：2015-11-12，
  
  修回日期：2015-12-15，
  
  纸质出版日期：2016-05-25
- 稿件说明：
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朱俊青, 沙巍, 陈长征等. 大口径空间相机像质的微振动频率响应计算[J]. 光学精密工程, 2016,24(5): 1118-1127

ZHU Jun-qing, SHA Wei, CHEN Chang-zheng etc. Frequency response of imaging quality by micro-vibration for large-aperture space-borne telescope[J]. Editorial Office of Optics and Precision Engineering, 2016,24(5): 1118-1127
朱俊青, 沙巍, 陈长征等. 大口径空间相机像质的微振动频率响应计算[J]. 光学精密工程, 2016,24(5): 1118-1127 DOI： 10.3788/OPE.20162405.1118.

ZHU Jun-qing, SHA Wei, CHEN Chang-zheng etc. Frequency response of imaging quality by micro-vibration for large-aperture space-borne telescope[J]. Editorial Office of Optics and Precision Engineering, 2016,24(5): 1118-1127 DOI： 10.3788/OPE.20162405.1118.

摘要

由于大口径空间相机对空间环境变化和卫星内部振源引起的微振动十分敏感

本文研究了影响成像质量的微振动频率响应的计算方法

以改善相机的在轨动态成像质量。该方法通过实际光学模型取代线性光学模型

建立微振动光机集成模型

从而计算影响成像质量的微振动频率响应。首先

建立大口径空间相机有限元模型

进行结构频率响应计算

得到采样频率点的光学表面节点位移和相位。然后

通过蒙特卡洛分析方法

建立微振动光机集成模型

以均方根光学系统动态传递函数和视轴漂移衡量大口径空间相机动态成像性能。最后

研制了大口径空间相机力学样机

对其进行了振动试验

验证了有限元模型的正确性。试验结果表明仿真结果与试验结果接近

误差均在5%以内

满足大口径空间相机动态成像质量分析的要求。

Abstract

The imaging quality of a large-aperture space-borne telescope is very sensitive to the micro-vibration induced by space environmental variation and the vibration inner of a satellite. Therefore

this paper researches the calculation method of frequency response of imaging quality effected by the micro-vibration to improve the dynamic imaging quality of the satellite in orbit. By using a real optical model to replace the linear optical model

it establishes an optical-mechanical integrated model to calculate the frequency response of the micro-vibration. Firstly

it builds Finite Element Model(FEM) for a space-borne telescope to calculate the structural frequency response and to obtain the displacement and phase of the optical surface nodes for each sampling frequency point. Then

the Monte-Carlo statistical method is used to establish the the optical-mechanical integrated model

and the root-mean-square (RMS) of system dynamic Modulation Transfer Function(MTF) and the Line of Sight(LOS) drift are analyzed to measure dynamic imaging performance of the large-aperture space-borne telescope. Finally

a structural prototype of large-aperture space-borne telescope is developed to verify the reliability of the FEM. The results show that the measured frequency is close to that of the FEM analysis and the error is under 5%

which meets the requirements of large-aperture space-borne telescopes for analysis of the dynamic imaging quality.

关键词

Keywords

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