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硅微条探测器热控制系统(Tracker thermo control system,TTCS)是阿尔法磁谱仪(Alpha magnetic spectrometer,AMS)内一个重要的子系统,其主要任务是将AMS-02内部硅微条探测器产生的热量传导到辐射板以排散到太空,并维持探测器内部温度高度稳定.为提高可靠性,TTCS运行过程监控采取了结合自保护机制的分层监控实现策略.首先介绍了TTCS系统总体架构及组成;在此基础上着重描述了TTCS监控硬件平台,并分析了分层监控策略的模型结构和功能分配,硬件实现的自保护机制(Health-guard)进一步提高了系统运行安全度,最后结合地面模拟测试平台,给出了系统运行测试结果.该监控策略已成功应用在TTCS原型件设计中.

参考文献

[1] AMS Collaboration.Search for antihelium in cosmic rays[J].Phys.Lett.B,1999,461:387-396.
[2] AMS Collaboration.The alpha magnetic spectrometer (AMS) on the international space station:part Ⅰ-results from the test flight on the space shuttle[J].Phys.Rep.,2002,366(6):331-404.
[3] Ing Youn Chen,Chyu M C.Two-phase active thermal control systems for spacecrafts[C].Energy Conversion Engineering Conf.,1996,2:1488-1493.
[4] Ungar E K.Single phase vs.two-phase active thermal control systems for space applications:a trade study[C].AIAA Paper,1995,95:0634.
[5] J Van Es.Development of the tracker thermal control system of the alpha magnetic spectrometer[R].NLR-Memorandum ASSP-2004-021,2004.
[6] Wang Ping.Module design method for telemetry software of micro-satellite[J].Chinese Journal of Quantum Electronics (量子电子学报),2004,21(3):392-395 (in Chinese).
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