中国激光, 2013, 40 (9): 0916003, 网络出版: 2013-08-27   

天基紫外跟踪详查光学系统设计

Optical Design of Space-Based Ultraviolet Tracking and Detailed Reconnaissance System
作者单位
中国科学院长春光学精密机械与物理研究所, 吉林 长春 130033
摘要
为满足天基紫外跟踪观测需求,设计了一套紫外跟踪详查系统,该系统由跟踪相机与详查相机两部分组成。利用望远系统与中继透镜结合的方式实现双视场与双角分辨率。望远系统采用曼金卡塞格林结构,口径为100 mm,焦距为605 mm。跟踪系统波段范围为250~400 nm,跟踪相机视场为2.5°×1.9°,角分辨率优于180 μrad,详查相机波长范围为200~360 nm,视场角为0.15°×0.11°,角分辨率优于13 μrad。利用光学软件设计并进行分析,跟踪相机与详查相机各视场调制传递函数分别高于0.9和0.8,满足设计指标要求。
Abstract
A tracking and detailed reconnaissance system is designed for space-based ultraviolet (UV) tracking requirement. The system consists of two parts, tracking camera and detailed reconnaissance camera. Dual field of view and dual angular resolution are achieved by combining telescope system and relay lens. The telescope system is Mangin-Cassegrain structure, with diameter of 100 mm, focal length of 605 mm. For the tracking camera, the wavelength range is 250~400 nm, the field of view is 2.5°×1.9°, and the angular resolution is better than 180 μrad. For the detailed reconnaissance camera, the wavelength range is 200~360 nm, the field of view is 0.15°×0.11°, and the angular resolution is better than 13 μrad. The modulation transfer function (MTF) of tracking camera is better than 0.9, and the MTF of detailed reconnaissance camera is better than 0.8. The results meet the requirements of specifications through the design and optical software analysis.
参考文献

[1] Adalbert Mclntyre. Multispectral measurements program (MSMP) results and status[C]. SPIE, 1978, 156,116-119.

[2] Bruce D Guilmain. Midcourse space experiment (MSX), an overview of the program, organization, targets, and schedule[C]. SPIE, 1993, 2232,188-199.

[3] 国爱燕, 白廷柱, 胡海鹤, 等. 固体火箭发动机羽烟紫外辐射特性分析[J]. 光学学报, 2012, 32(10): 1016002.

    Guo Aiyan, Bai Tingzhu, Hu Haihe, et al.. Analysis of ultraviolet radiation characteristics of solid propellant rocket motor exhaust plume[J]. Acta Optica Sinica, 2012, 32(10): 1016002.

[4] Lou Ying, Bai Tingzhu. A study on UV missile plume emission model[C]. SPIE, 2006, 6031: 60310F.

[5] 王正凤, 付秀华, 张静, 等. 日盲紫外告警系统中成像滤光片的研制[J]. 中国激光, 2011, 38(12): 1207002.

    Wang Zhengfeng, Fu Xiuhua, Zhang Jing, et al.. Research of imaging filter in solar blind ultraviolet alarm system[J]. Chinese J Lasers, 2011, 38(12): 1207002.

[6] J L Rapanotti. Fluent-based modeling of rocket exhaust signatures[C]. SPIE, 2006, 6239: 62390S.

[7] 国爱燕, 白廷柱, 唐义, 等. 固体火箭发动机羽烟紫外辐射仿真研究[J]. 光学学报, 2009, 29(s1): 295-299.

    Guo Aiyan, Bai Tingzhu, Tang Yi, et al.. UV plume simulation for a solid propellant rocket[J]. Acta Optica Sinica, 2009, 29(s1): 295-299.

[8] 于向阳, 王淑荣, 黄煜, 等. 地球临边/天底同时探测的紫外环形成像仪[J]. 光学学报, 2012, 32(12): 1211004.

    Yu Xiangyang, Wang Shurong, Huang Yu, et al.. Development of ultraviolet annular imager for earth limb and nadir sounding simultaneously[J]. Acta Optica Sinica, 2012, 32(12): 1211004.

[9] 张振铎, 王淑荣. 星载臭氧垂直探测仪地外太阳紫外光谱测量[J]. 激光与光电子学进展, 2012, 49(6): 061201.

    Zhang Zhenduo, Wang Shurong. Measurement of extraterrestrial solar ultraviolet spectrum from the solar backscatter ultraviolet spectrometer[J]. Laser & Optoelectronics Progress, 2012, 49(6): 061201.

[10] R Jeenu, K Pinumalla, D Deepak. Size distribution of particles in combustion products of aluminized composite propellant[J]. J Propulsion and Power, 2010, 26(4): 715-723.

[11] F W Schenkel, B S Orgorzalek. Auroral images from space: imagery,spectroscopy, and photometry[J]. APL Tech Dig, 1987, 8: 308-317.

[12] R C Henry, J Murthy, M Allen, et al.. Spectroscopy and imaging of the cosmic diffuse UV background radiation[C]. SPIE, 1992, 1764: 61-71.

李博, 王淑荣, 王俊博. 天基紫外跟踪详查光学系统设计[J]. 中国激光, 2013, 40(9): 0916003. Li Bo, Wang Shurong, Wang Junbo. Optical Design of Space-Based Ultraviolet Tracking and Detailed Reconnaissance System[J]. Chinese Journal of Lasers, 2013, 40(9): 0916003.

本文已被 7 篇论文引用
被引统计数据来源于中国光学期刊网
引用该论文: TXT   |   EndNote

相关论文

加载中...

关于本站 Cookie 的使用提示

中国光学期刊网使用基于 cookie 的技术来更好地为您提供各项服务,点击此处了解我们的隐私策略。 如您需继续使用本网站,请您授权我们使用本地 cookie 来保存部分信息。
全站搜索
您最值得信赖的光电行业旗舰网络服务平台!