大气与环境光学学报 ›› 2013, Vol. 8 ›› Issue (5): 372-378.

• 光学遥感与图像处理 • 上一篇    下一篇

星载仪器温度控制电路可靠性预计

金洁, 洪津, 王羿, 邹鹏   

  1. (中国科学院安徽光学精密机械研究所中国科学院通用光学定标与表征技术重点实验室,安徽 合肥 230031)
  • 收稿日期:2013-04-09 修回日期:2013-04-25 出版日期:2013-09-28 发布日期:2013-09-06
  • 通讯作者: 金洁 (1987-),女,安徽含山人,研究生,研究方向为检测技术与自动化装置。 E-mail:jinjie@aiofm.ac.cn。
  • 作者简介:金洁 (1987-),女,安徽含山人,研究生,研究方向为检测技术与自动化装置。
  • 基金资助:

    国建自然科学基金(青年基金项目)(41201368)资助

Reliability Prediction of Spaceborne Instruments Temperature Control Circuit

JIN Jie, HONG Jin, WANG Yi, ZOU Peng   

  1. (Key Laboratory of Optical Calibration and Characterization, Anhui Institute Of Optics and Fine Mechanics, Chinese Academy of Sciences, Hefei 230031, China)
  • Received:2013-04-09 Revised:2013-04-25 Published:2013-09-28 Online:2013-09-06

摘要:

主动温度控制措施是星载仪器适应空间严酷热环境的重要手段。某星载仪器采用主动加热的的方式对温度敏感组件进行温度控制。该温控模块的可靠性直接关系到主动温控措施的效果,进而影响仪器任务的成败。本文以该温控电路为基础,通过对系统备份和单元备份两种冗余设计方案的可靠性进行了分析对比,结果表明采用系统备份方式的温控电路可靠度更高,根据该可靠性预计结果,结合该星载温度控制功能模块特点,确定了温控模块的最终实施方案。

关键词: 可靠性预计, 应力分析法, 冗余

Abstract:

Active temperature control is adapted as an important mean for the spaceborne instruments to fit the harsh thermal environment. the way of active heating is used for the spaceborne instrument to control the temperature of its temperature sensitive component. The reliability of the temperature control module is directly related to the effects of the active temperature control measures, which may affect the instrument performance. Based on the temperature control circuit, the reliability comparison between two redundant design schemes is carried out, namely the system backup and the unit backup. The results showed that the backup system has higher reliability. According to the results of the reliability prediction, in combination with the on-board temperature control function module's feature, the temperature control module was selected.

Key words: reliability prediction, stress analysis procedure, redundancy

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