[1] Jin Z, Yu X, Ma H. Resonator fiber optic gyro employing a semiconductor laser[J]. Applied Optics, 2012, 51(15): 2856-64.

[2] Jin Shi, Hu Jun，Cao Xiaotao. Design of testing system of active thermal control for space camera[J]． Chinese Journal of Optics and Applied Optic, 2010, 3(2): 126-132. (in Chinese)

[3] Wu Xuefeng, Ding Yalin, Wu Qingwen. Thermal design for near space optical remote sensor[J]． Optics and Precision Engineering, 2010, 18(5): 1159-1165. (in Chinese)

[4] Luo Zhitao, Xu Shuyan, Chen Liheng. Thermal control of high-power focal plane apparatus[J]． Optics and Precision Engineering, 2008, 16(11): 2187-2192. (in Chinese)

[5] Zi Keming, Wu Qingwen, Guo Jiang, et al. Thermal design of CCD focal plane assembly of space optical remote-sensor [J]． Optical Technique, 2008, 34(3): 401-407. (in Chinese)

[6] Li Ming, Wu Qingwen, Jiang Fan, et al. Design of thermal control system for three-linear array mapping cameras[J]． Optics and Precision Engineering, 2010, 18(6): 1367-1373. (in Chinese)

[7] Fan Hanlin, Fan Yufeng. The demand of materials in the spacecraft thermal control subsystem[J]． Spacecraft Environment Engineering, 2010, 27(2): 135-138. (in Chinese)

[8] Li Yunze, Wei Chuanfeng, Yuan Lingshuang, et al. Simulation of micro spacecraft active temperature control system using thermoelelectric cooler[J]． Chinese Journal of Mechanical Engineering, 2005, 41(10): 149-152. (in Chinese)