| Citation: | Ma Yingjian, Jian Hongqing, Shi Duoet al. Temperature dynamic characteristics analysis and control of optic-fiber light source[J]. Journal of Beijing University of Aeronautics and Astronautics, 2006, 32(03): 324-327. (in Chinese)
|
|
[1] Lefever H.The fiber-optic gyroscope[M].USA:Artech House,1993 [2] 尹世刚,舒晓武,宫兆涛,等.光纤陀螺用SLD光源的光功率稳定性研究 .光学仪器,2003,25(4):20~25 Yin Shigang,Shu Xiaowu,Gong Zhaotao,et al. Study on stability of output power of SLD used for FOG[J]. Optical Instruments,2003,25(4):20~25(in Chinese) [3] 张 ,王 妍,张春熹,等.光纤陀螺光源驱动技术[J].北京航空航天大学学报,2002,28(3):298~300 Zhang Xi,Wang Yan,Zhang Chunxi,et al. Driving technology of the light source of FOG[J]. Journal of Beijing University of Aeronautics and Astronautics,2002,28(3):298~300(in Chinese) [4] 卢希红,李茂德,潘葆炯.半导体制冷器温度场的数值分析[J].能源研究与信息,2001,17(1):18~21 Lu Xihong,Li Maode,Pan Baojiong. Numerical study on the temperature field in a semiconductor refrigeration device[J]. Energy Research and Information,2001,17(1):18~21(in Chinese) [5] 刘繁明,赵亚凤.一种新型的基于TEC的精密温控器设计[J].中国惯性技术学报,2004,12(6):61~64 Liu Fanming,Zhao Yafeng. Design of a new TEC-based accurate incubator[J]. Chinese Journal of Inertia Technology, 2004,12(6):61~64(in Chinese) [6] 覃喜庆,曾详鸿,董 静,等.基于ADN8830的高性能TEC控制电路[J].光学与光电技术,2004,2(1):20~22 Qin Xiqing,Zeng Xianghong,Dong Jing,et al. A high performance TEC controller circuit based on ADN8830[J]. Optics & Optoelectronic Technology, 2004,2(1):20~22(in Chinese) [7] 张 华,龚义建.一种微型高精度PWM温度控制器的设计[J].光学与光电技术,2004,2(2):29~31 Zhang Hua,Gong Yijian. Design for high precision miniature PWM temperature controller[J]. Optics & Optoelectronic Technology, 2004, 2(2):29~31(in Chinese)
|
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