Abstract
In order to calculate the temperature and infrared radiation characteristics of space target, it is necessary to master the distribution and variation regularity of the orbit external thermal flux on target. Analysing the energy exchange relation-ship between the inside and outside of the space target in orbit, the numerical simulation method was used to simulate the temperature and infrared of a cone-shaped space target, and the influence of various parameters on the calculation results was quantitatively analysed. The results show that the angle β between sunlight and orbital plane has a significant effect on the temperature and infrared variation of space target, the calculation results are more sensitive to the change of β when β is larger. Considering the change of the earth albedo with latitude, the temperature and the infrared radiation intensity of 8–14 μm reduced by 1.73 °C and 0.27 W/sr respectively. The variation of albedo cannot be ignored when calculating the characteristics of space target accurately.
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References
Liang-chen SHI, Guo-biao CAI, Ding-qiang ZHU (2009) The simulation to infrared signatures of spacecraft. J Astronaut 30(1):229–234
John D, Mill, John T, Stair J (1997) MSX design driven by targets and backgrounds. In: Aerospace sciences meeting and exhibit
Chenxing Luo, Wen Sheng (2014) Modeling of missile wall temperature field and its infrared radiation characteristics. J Air Force Early Warn Acad 28(4):254–257
Wentao Shen, Dingqiang Zhu, Guobiao Cai (2010) Calculation of temperature field and infrared radiation characteristics of midcourse ballistic target. J Astronaut 31(9):2210–2217
Xiao Wang, Sili Gao, Fanming Li (2017) Simulation and target analysis of dual-band infrared dynamic scene in deep space. Infrared Laser Eng 47(9):1123–1127
Hongyuan Wang, Yun Chen (2016) Modeling and simulation of infrared dynamic characteristics of space-based space targets. Infrared Laser Eng 45(5):1–7
Hao ZHANG, Jianguang CAO, Jiang WANG et al (2018) Analysis of satellite’s extreme heat flow in inclined orbit. Aerosp Shanghai 35(1):36–42
Qing PAN, Pingyang WANG, Yiying BAO et al (2012) On-orbit external heat flux calculation of spacecraft based on reverse monte carlo method. J Shanghai JiaoTong Univ 46(05):750–755
Guirong MIN, Shun GUO (1998) Satellite thermal control technology. The Science Publishing House, Beijing
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Li, X., Li, J. (2020). Research on Temperature and Infrared Characteristics of Space Target. In: Liang, Q., Wang, W., Liu, X., Na, Z., Jia, M., Zhang, B. (eds) Communications, Signal Processing, and Systems. CSPS 2019. Lecture Notes in Electrical Engineering, vol 571. Springer, Singapore. https://doi.org/10.1007/978-981-13-9409-6_154
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DOI: https://doi.org/10.1007/978-981-13-9409-6_154
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