[1] Wei Lei, Zhang Lei, Li Zongxuan, et al. Optimization design and test for large aspect ratio rectangular SiC space mirror[J]. Acta Photonica Sinica, 2017, 46(3): 0322003. (in Chinese)

[2] Tong Yelong, Li Yifan, Zhao Xin, et al. Thermal design and validation for spacecraft high-stability structure[J]. Spacecraft Engineering, 2018, 27(3): 61-66. (in Chinese)

[3] Zhang Liguo, Li Yudong, Liu Zexun, et al. Influence of total dose effects on TDI-CCD and corresponding test methods[J]. Optics and Precision Engineering, 2009, 17(12): 2924-2930. (in Chinese)

[4] Guan Yingjun, Xin Hongwei. Design and analysis for CCD electronic box structure of space camera[J]. Machinery Design ＆ Manufacture, 2011, 7(7): 35-37.(in Chinese)

[5] Chen Zhizhou, Cao Kaiqin, Miao Bin, et al. Thermal design of electric cabinet for space cameras[J]. Infrared Technology, 2017, 39(10): 880-883. (in Chinese)

[6] Xu Yanjun, Qi Yingchun, Ren Jianyue. Thermal analysis of space electronic sensor system[J]. Electro-Mechanical Engineering, 2009, 25(2): 12-15. (in Chinese)

[7] Li Wenhao, Liu Zhaohui, Mu You, et al. Modeling and research of infrared characteristics of space target based on radiation dissipation[J]. Infrared and Laser Engineering, 2017, 46(6): 0604003. (in Chinese)

[8] Guan Fengwei, Liu Ju. Thermal design of high power electronic control cabinet of space optical remote sensor[J]. Chinese Optics, 2013, 6(6): 919-929. (in Chinese)