...
首页> 外文期刊>Applied optics >Flight model characterization of the wide-field off-axis telescope for the MATS satellite
【24h】

Flight model characterization of the wide-field off-axis telescope for the MATS satellite

机译:用于垫卫星宽轴轴外望远镜的飞行模型

获取原文
获取原文并翻译 | 示例
   

获取外文期刊封面封底 >>

       

摘要

We present optical characterization, calibration, and performance tests of the Mesospheric Airglow/Aerosol Tomography Spectroscopy (MATS) satellite, which for the first time, to the best of our knowledge, for a satellite, applies a linear-astigmatism-free confocal off-axis reflective optical design. Mechanical tolerances of the telescope were investigated using Monte Carlo methods and single-element perturbations. The sensitivity analysis results indicate that tilt errors of the tertiary mirror and a surface RMS error of the secondary mirror mainly degrade optical performance. From the Monte Carlo simulation, the tolerance limits were calculated to +/- 0.5 mm, +/- 1 mm, and 10.15 degrees for decenter, despace, and tilt, respectively. We performed characterization measurements and optical tests with the flight model of the satellite. Multi-channel relative pointing, total optical system throughput, and distortion of each channel were characterized for end-users. Optical performance was evaluated by measuring the modulation transfer function (MTF) and point spread function (PSF). The final MTF performance was 0.25 MTF at 20 lp/mm for the ultraviolet channel (304.5 nm), and 0.25-0.54 MTF at 10 lp/mm for infrared channels. The salient fact of the PSF measurement of this system is that there is no noticeable linear astigmatism detected over a wide field of view (5.67 degrees x 0.91 degrees). All things considered, the design method showed great advantages in wide field of view observations with satellite-level optical performance. (C) 2020 Optical Society of America
机译:我们介绍了Mesompheric Airglow /气溶胶断层扫描谱(MATS)卫星的光学表征,校准和性能测试,这是我们首次获得卫星的知识,适用于无线自由散的共焦 - 轴反射光学设计。使用Monte Carlo方法和单元素扰动来研究望远镜的机械公差。灵敏度分析结果表明,次镜的倾斜误差和次级镜的表面RMS误差主要降低光学性能。从蒙特卡罗模拟,分别计算公差限制,分别计算成+/- 0.5毫米,+/- 1毫米,+/- 1毫米,分别为10.15度,分别为倾斜,倾斜。我们使用卫星的飞行模型进行了表征测量和光学测试。多通道相对指向,总光学系统吞吐量和每个通道的失真都是针对最终用户的特征。通过测量调制传递函数(MTF)和点扩展功能(PSF)来评估光学性能。最终MTF性能为0.25mTF,对于20Lp / mm,紫外线通道(304.5nm),0.25-0.54mtf,用于红外通道10磅/ mm。 PSF测量的PSF测量的突出事件在于在宽视场上没有检测到明显的线性散光(5.67度×0.91度)。考虑的所有内容,设计方法在卫星电平光学性能方面的宽视野中显示出了很大的优势。 (c)2020美国光学学会

著录项

  • 来源
    《Applied optics》 |2020年第17期|共8页
  • 作者单位

    Kyung Hee Univ Sch Space Res 1732 Deogyeong Daero Yongin 17104 Gyeonggi Do South Korea;

    Omnisys Instruments AB August Barks Gata 6B SE-42132 Vastra Frolunda Sweden;

    Kyung Hee Univ Sch Space Res 1732 Deogyeong Daero Yongin 17104 Gyeonggi Do South Korea;

    Ctr Integrated Smart Sensors 291 Daehak Ro Daejeon 34141 South Korea;

    Stockholm Univ Dept Meteorol MISU SE-10691 Stockholm Sweden;

    Stockholm Univ Dept Meteorol MISU SE-10691 Stockholm Sweden;

    Stockholm Univ Dept Meteorol MISU SE-10691 Stockholm Sweden;

    Omnisys Instruments AB August Barks Gata 6B SE-42132 Vastra Frolunda Sweden;

    Univ Arizona James C Wyant Coll Opt Sci 1630 E Univ Blvd Tucson AZ 85721 USA;

  • 收录信息
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类 应用;
  • 关键词

获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号