高温窗口作用下红外导引头性能建模与评估

柴国贝; 赵晓宁; 刘玮; 鲍文卓; 谢晓阳; 李强

doi:10.3788/IRLA201948.0904003

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高温窗口作用下红外导引头性能建模与评估

柴国贝, 赵晓宁, 刘玮, 鲍文卓, 谢晓阳, 李强

文章导航 > 红外与激光工程 > 2019 > 48(9): 904003-0904003(7)

柴国贝, 赵晓宁, 刘玮, 鲍文卓, 谢晓阳, 李强. 高温窗口作用下红外导引头性能建模与评估[J]. 红外与激光工程, 2019, 48(9): 904003-0904003(7). doi: 10.3788/IRLA201948.0904003

引用本文:

Chai Guobei, Zhao Xiaoning, Liu Wei, Bao Wenzhuo, Xie Xiaoyang, Li Qiang. Modeling and evaluation of infrared seeker in high temperature window[J]. Infrared and Laser Engineering, 2019, 48(9): 904003-0904003(7). doi: 10.3788/IRLA201948.0904003

Citation:

Chai Guobei, Zhao Xiaoning, Liu Wei, Bao Wenzhuo, Xie Xiaoyang, Li Qiang. Modeling and evaluation of infrared seeker in high temperature window[J]. Infrared and Laser Engineering, 2019, 48(9): 904003-0904003(7). doi: 10.3788/IRLA201948.0904003

高温窗口作用下红外导引头性能建模与评估

doi: 10.3788/IRLA201948.0904003

1.
中国运载火箭技术研究院,北京 100076

详细信息

作者简介:
柴国贝(1988-),男,工程师,博士,主要从事目标特性建模与仿真方面的研究。Email:chaiguobei@sina.com

中图分类号: TP216

Modeling and evaluation of infrared seeker in high temperature window

1.
China Academy of Launch Vehicle Technology,Beijing 100076,China

摘要: 高超声速飞行器的高温窗口会对红外导引头成像性能产生严重影响。为了定量分析高温窗口效应，通过红外导引头信号响应特性和高温热辐射特性耦合的方法，建立了高温窗口作用下的红外导引头成像量化表征模型，并利用典型红外导引头系统高温窗口实验对该模型进行验证。基于量化表征模型，结合外场试验获取的船海辐射数据，实现了多种温度窗口作用下红外导引头成像结果计算，并对高温窗口作用下的红外导引头成像性能进行评估分析。分析结果表明：当窗口温度超过250℃时，肉眼基本无法通过图像分辨船只；当窗口温度超过300℃时，基本无法通过导引头识别算法实现目标的分辨和跟踪。
- 高温窗口 /
- 响应特性 /
- 成像性能 /
- 红外导引头
Abstract: The high temperature window of a hypersonic vehicle can have a severe impact on the imaging performance of the infrared seeker. In order to quantitatively analyze the high temperature window effect, the imaging and quantitative characterization model of the infrared seeker in high temperature window was established through the coupling of the signal response characteristics of the infrared seeker and the high temperature thermal radiation characteristics. The quantiative charateriation model was verified by high temperature window experiment of typical infrared seeker system. Based on the quantitative characterization model, combined with the ship radiation data obtained from the external field test, the imaging results of the infrared seeker under various temperature windows were calculated, and the imaging performance of the infrared seeker under the high-temperature window was evaluated. The analysis results indicate that when the window temperature exceeds 250℃, the naked eye can hardly distinguish the ship through the image; when the window temperature exceeds 300℃, the target resolution and tracking cannot be achieved by the seeker recognition algorithm.
- high temperature window /
- response characteristics /
- imaging performance /
- infrared seeker

[1]	Deep S, Jagadeesh G. Aerothermodynamic effects of controlled heat release within the hypersonic shock layer around a large angle blunt cone[J]. Physics of Fluids, 2018, 30(10):106103.
[2]	Niu Q, Gao P, Yuan Z, et al. Numerical analysis of thermal radiation noise of shock layer over an infrared optical dome at near-ground altitudes[J]. Infrared Physics Technology, 2019, 97:74-84.
[3]	Wang Yahui, Wang Qiang, Gao Lei, et al. Aero-thermo-radiation of a hy-personic vehicle[J]. Infrared and Laser Engineering, 2013, 42(6):1399-1403. (in Chinese)王亚辉, 王强, 高磊, 等. 高超声速飞行器气动热辐射特性[J]. 红外与激光工程, 2013, 42(6):1399-1403.
[4]	Niu Q, Gao P, Yuan Z, et al. Numerical analysis of thermal radiation noise of shock layer over an infrared optical dome at near-ground altitudes[J]. Infrared Physics Technology, 2019, 97:74-84.
[5]	Zhou T. Precision molding of microstructures on chalcogenide glass for infrared optics[J]. Micro and Nano Fabrication Technology, 2018:1-26.
[6]	Zhang Xingde, Liu Lin, Li Ronggang. IR optical window for airborne photoelectric equipments[J]. Infrared and Laser Engineering, 2010, 39(4):601-606. (in Chinese)张兴德, 刘琳, 李荣刚. 机载光电设备红外窗口技术[J]. 红外与激光工程, 2010, 39(4):601-606.
[7]	Donegan B E, Greendyke R, Ravichandran R, et al. Experimental analysis of the interaction of carbon and silicon ablation products in expanding hypersonic flows[C]//22nd AIAA International Space Planes and Hypersonics Systems and Technologies Conference. 2018:5325.
[8]	Liu X, Zhu J, Han J. Numerical and experimental investigation on thermal shock failure of Y2O3-coated CVD ZnS infrared windows[J]. International Journal of Heat and Mass Transfer, 2018, 124:124-130.
[9]	Liu Li, Meng Weihua, Pan Guoqing. Modeling and analysis of infrared radiation from the dome flying at supersonic speed[J]. Infrared and Laser Engineering, 2011, 40(7):1193-1198. (in Chinese)刘立, 孟卫华, 潘国庆. 超音速飞行环境中光学头罩热辐射建模与分析[J]. 红外与激光工程, 2011, 40(7):1193-1198.
[10]	Wang Y, Wang Q, Zhang B, et al. Evaluation of thermo-radiation characteristics of IR windows in hypersonic vehicles[C]//Selected Papers from Conferences of the Photoelectronic Technology Committee of the Chinese Society of Astronautics 2014, Part Ⅱ. International Society for Optics and Photonics, 2015, 9522:95220R.
[11]	Wang Y H, Wang Q, Zhang B C, et al. Measurement of thermo-radiation characteristics of IR window materials[J]. Advanced Materials Research, 2015, 1083:104.
[12]	Zhang X, Li H. Research on target capture probability calculation model of composite photoelectric detection imaging sensor system[J]. Optik, 2018, 166:161-168.
[13]	Modest M F. Radiative Heat Transfer[M]. New York:Academic Press, 2013.
[14]	Chatterjee R S, Singh N, Thapa S, et al. Retrieval of land surface temperature(LST) from landsat TM6 and TIRS data by single channel radiative transfer algorithm using satellite and ground-based inputs[J]. International Journal of Applied Earth Observation and Geoinformation, 2017, 58:264-277.

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高温窗口作用下红外导引头性能建模与评估

doi: 10.3788/IRLA201948.0904003

1. 中国运载火箭技术研究院,北京 100076

作者简介:
柴国贝(1988-),男,工程师,博士,主要从事目标特性建模与仿真方面的研究。Email:chaiguobei@sina.com

收稿日期: 2019-04-05
修回日期: 2019-05-03
刊出日期: 2019-09-25

中图分类号: TP216

关键词:

摘要: 高超声速飞行器的高温窗口会对红外导引头成像性能产生严重影响。为了定量分析高温窗口效应，通过红外导引头信号响应特性和高温热辐射特性耦合的方法，建立了高温窗口作用下的红外导引头成像量化表征模型，并利用典型红外导引头系统高温窗口实验对该模型进行验证。基于量化表征模型，结合外场试验获取的船海辐射数据，实现了多种温度窗口作用下红外导引头成像结果计算，并对高温窗口作用下的红外导引头成像性能进行评估分析。分析结果表明：当窗口温度超过250℃时，肉眼基本无法通过图像分辨船只；当窗口温度超过300℃时，基本无法通过导引头识别算法实现目标的分辨和跟踪。

English Abstract

Modeling and evaluation of infrared seeker in high temperature window

1. China Academy of Launch Vehicle Technology,Beijing 100076,China

Received Date: 2019-04-05
Rev Recd Date: 2019-05-03
Publish Date: 2019-09-25

Keywords:

Abstract: The high temperature window of a hypersonic vehicle can have a severe impact on the imaging performance of the infrared seeker. In order to quantitatively analyze the high temperature window effect, the imaging and quantitative characterization model of the infrared seeker in high temperature window was established through the coupling of the signal response characteristics of the infrared seeker and the high temperature thermal radiation characteristics. The quantiative charateriation model was verified by high temperature window experiment of typical infrared seeker system. Based on the quantitative characterization model, combined with the ship radiation data obtained from the external field test, the imaging results of the infrared seeker under various temperature windows were calculated, and the imaging performance of the infrared seeker under the high-temperature window was evaluated. The analysis results indicate that when the window temperature exceeds 250℃, the naked eye can hardly distinguish the ship through the image; when the window temperature exceeds 300℃, the target resolution and tracking cannot be achieved by the seeker recognition algorithm.