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Liu Qiang Zhang Zhongzhao Zhang Naitong (Communication Research Center Harbin Institute of Technology,Harbin 150001)
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Abstract: This paper first introduces the structure of space station DMS.By analysing of the fault tolerance ability and the reliability of the FDDI、IEEE802 4、MIL-STD-1553B in each case,may be obtained the reliability mathematics models with probability analysis.It also illustrates the DMS reliability variation with the variation of station's quantity and link failure probability,and this provides the foundation of the reliability design of the space station DMS.
Liu Qiang Zhang Zhongzhao Zhang Naitong (Communication Research Center Harbin Institute of Technology,Harbin 150001). Reliability Analysis of Space Station DMS Based on FDDI[J]. .
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