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航天相机主动热控测试系统设计
引用本文:金实,胡君,曹小涛. 航天相机主动热控测试系统设计[J]. 中国光学与应用光学文摘, 2010, 0(2)
作者姓名:金实  胡君  曹小涛
作者单位:中国科学院长春光学精密机械与物理研究所;中国科学院研究生院;
摘    要:为了检测航天相机主动热控系统的功能、性能及可靠性,设计了主动热控仿真测试系统。依据传热学基本定律、航天器轨道理论和热控策略,给出了计算航天相机温度场的热网络数学模型,使主动热控系统能在模拟的空间热环境中连续工作,实现了对主动热控系统的闭环仿真测试。采用两个数字电位器相串联的方法模拟温度传感器的走势,得到的最大阻值为100 kΩ,精度达到10Ω,符合设计中对总电阻和电阻变化率的需求,实现了对主动热控系统的功能、性能以及可靠性的仿真测试。

关 键 词:航天相机  主动热控  PCI总线  闭环控制  数字电位器  

Design of testing system of active thermal control for space camera
JIN Shi,,HU Jun,Cao Xiao-tao. Design of testing system of active thermal control for space camera[J]. Chinese Optics and Applied Optics Abstracts, 2010, 0(2)
Authors:JIN Shi    HU Jun  Cao Xiao-tao
Affiliation:JIN Shi1,2,HU Jun1,Cao Xiao-tao1 (1.Changchun Institute of Optics,Fine Mechanics , Physics,Chinese Academy of Sciences,Changchun 130033,China,2.Graduate University of Chinese Academy of Sciences,Beijing 100039,China)
Abstract:In order to detect the function,performance and reliability of active thermal control system of a space camera,a simulation testing system to detect the active thermal control system was designed.The thermal-net mathematical model to calculate the temperature field of camera was established based on the basic law of heat transfer,orbital theory of spacecraft and the thermal control strategy,so that the active thermal control circuit could work in a simulated thermal space environment continuously,and the cl...
Keywords:space camera  active thermal control  PCI bus  closed-loop control  digital potentiometers  
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