空间光学相机在乃奎斯特频率处的调制传递函数测试与实验

吕恒毅; 薛旭成; 赵运隆; 韩诚山

doi:10.3788/OPE.20152305.1484

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空间光学相机在乃奎斯特频率处的调制传递函数测试与实验

信息科学 | 更新时间：2020-08-13

- 空间光学相机在乃奎斯特频率处的调制传递函数测试与实验
- Measurement and experiment of modulation transfer function at Nyquist frequency for space optical cameras
- 光学精密工程 2015年23卷第5期页码：1484-1489
- 作者机构：
  
  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
- 作者简介：
- 基金信息：
  
  国家自然科学基金资助项目(No.61036015)()
- DOI：10.3788/OPE.20152305.1484
  中图分类号： V447.3
- 收稿日期：2014-04-21，
  
  修回日期：2014-06-10，
  
  纸质出版日期：2015-05-25
- 稿件说明：
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吕恒毅, 薛旭成, 赵运隆等. 空间光学相机在乃奎斯特频率处的调制传递函数测试与实验[J]. 光学精密工程, 2015,23(5): 1484-1489

L&#220, Heng-yi, XUE Xu-cheng etc. Measurement and experiment of modulation transfer function at Nyquist frequency for space optical cameras[J]. Editorial Office of Optics and Precision Engineering, 2015,23(5): 1484-1489
吕恒毅, 薛旭成, 赵运隆等. 空间光学相机在乃奎斯特频率处的调制传递函数测试与实验[J]. 光学精密工程, 2015,23(5): 1484-1489 DOI： 10.3788/OPE.20152305.1484.

L&#220, Heng-yi, XUE Xu-cheng etc. Measurement and experiment of modulation transfer function at Nyquist frequency for space optical cameras[J]. Editorial Office of Optics and Precision Engineering, 2015,23(5): 1484-1489 DOI： 10.3788/OPE.20152305.1484.

摘要

为了精确地测试空间光学相机入轨之前在乃奎斯特频率处的调制传递函数

开展了整机在乃奎斯特频率处的传递函数测试实验。给出了相机在乃奎斯特频率处的调制传递函数测试链路图;推导了乃奎斯特频率的方波靶标在整个链路中的传递过程和终端靶标图像的精确对比度函数模型;计算了终端靶标图像的对比度与相机在乃奎斯特频率处的调制传递函数转换关系和理论误差形式。最后

在真空环境下测试了相机在乃奎斯特频率下的调制传递函数

并依据本文推导的结论对结果进行了修正。实验结果表明:某空间光学相机在实验室条件下测得的乃奎斯特频率处的调制传递函数为0.213

经折算时间延迟积分CCD(TDICCD)及处理电路的调制传递函数为0.602

TDICCD外围处理电路的调制传递函数等效衰减系数为0.946

与理论值接近。测试结果表明提出的方法基本准确

能够满足空间光学相机地面研制阶段对调制传递函数测试的要求。

Abstract

To precisely measure the Modulation Transfer Function(MTF) of a space camera at the Nyquist frequency before entering orbit

measuring methods were researched and some experiments for measuring the MTF at the Nyquist frequency were carried out. The schematic diagram of the MTF measurement was given. On the basis of the schematic diagram

the transfer process of a square wave target at Nyquist frequency in whole chain and the contrast ratio model of a terminal target image were investigated. Furthermore

the relationship between the contrast ratio of terminal target image and the MTF at Nyquist frequency and the error formation were given. Finally

the MTF at Nyquist frequency of the camera was measured in a vacuum environment and the obtained results were corrected. The result shows that the MTF of a space camera at Nyquis frequency is 0.213 at a lab condition

and that after the optical system in the camera architecture is 0.602 by conversion. Moreover

the MTF after Time Delay and Integration(TDICCD) is calculated as 0.946

which is close to the theoretical value. These results indicate that the derivation of our method is basically precise

and is capable of satisfying the requirement of space optical cameras for the MTF measurement before entering orbit.

关键词

Keywords

references

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