[1] Li Ming, Wu Qingwen, Yu Fei. Optimization of optical window glass thickness based on the thermal optical analysis [J]. Acta Optica Sinica, 2010, 30(1): 210-213.

[2] Shi Jinfeng, Wu Qingwen, Zhang Jianping, et al.. Thermal-optical analysis for optical window of high-altitude and high-speed aerial camera [J]. Acta Optica Sinica, 2012, 32(4): 210-213.

[3] Luo Chuanwei, Chang Weijun, Qiang Hua, et al.. Analysis of aerodynamic pressure loading for supersonic aircraft optical window[J]. Infrared and Laser Engineering, 2011,40(4):664-667.

[4] Li Yanwei, Yang Hongbo, Cheng Zhifeng, et al.. Thermal/structural/optical integrated design for optical window in aerial remote sensor [J]. Infrared and Laser Engineering, 2012, 41(8): 2012-2106.

[5] Li Yanwei, Zhang Hongwen, Yuan Guoqin, et al.. Design of protector for altitude sub-assembled Optical window [J]. Optics and Precision Engineering, 2014, 22(3): 664-669.

[6] Ding Yalin, Zhong Chongliang, Fu Jinbao. Mathematical model of optical window under high-mach flight condition [J]. Infrared and Laser Engineering, 2013, 42(3): 747-751.

[7] Wang Wei, Dong Jihong, Meng Qingyu. Current status and developing tendency of visible spectral remote sensing camera for mars observation [J]. Chinese Optics, 2014, 7(2): 208-214.

[8] Yang Weifan, Xu Shuyan, Cao Xiaotao. Design of scanning control system for space optical remote sensor [J]. Optics and Precision Engineering, 2014, 22(2): 397-405.

[9] E R Fuller Jr, S W Freiman, J B Quinn, et al.. Fracture mechanics approach to the design of glass aircraft windows: a case study [C].SPIE, 1994, 2286: 419-430.

[10] John W Pepi. Fail-safe design of an all BK-7 glass aircraft window [C]. SPIE, 1994, 2286: 431-443.