Infrared and Laser Engineering, Volume. 44, Issue 1, 249(2015)

Active thermal control system for space camera based on temperature level

Yu Tao*, Wang Yongcheng, Dai Shuang, Sun Liang, and Song Kefei
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    References(8)

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

    [5] [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)

    [7] [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] [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)

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    Yu Tao, Wang Yongcheng, Dai Shuang, Sun Liang, Song Kefei. Active thermal control system for space camera based on temperature level[J]. Infrared and Laser Engineering, 2015, 44(1): 249

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    Paper Information

    Category: 光电测量

    Received: May. 20, 2014

    Accepted: Jun. 22, 2014

    Published Online: Jan. 26, 2016

    The Author Email: Tao Yu (yut@ciomp.ac.cn)

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