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基于OBDD的可修航天测控系统任务可靠性分析

孟礼 武小悦

孟礼, 武小悦. 基于OBDD的可修航天测控系统任务可靠性分析[J]. 航空动力学报, 2016, 31(5): 1065-1072. doi: 10.13224/j.cnki.jasp.2016.05.006
引用本文: 孟礼, 武小悦. 基于OBDD的可修航天测控系统任务可靠性分析[J]. 航空动力学报, 2016, 31(5): 1065-1072. doi: 10.13224/j.cnki.jasp.2016.05.006
MENG Li, WU Xiao-yue. Mission reliability analysis of repairable space TT&C system based on OBDD[J]. Journal of Aerospace Power, 2016, 31(5): 1065-1072. doi: 10.13224/j.cnki.jasp.2016.05.006
Citation: MENG Li, WU Xiao-yue. Mission reliability analysis of repairable space TT&C system based on OBDD[J]. Journal of Aerospace Power, 2016, 31(5): 1065-1072. doi: 10.13224/j.cnki.jasp.2016.05.006

基于OBDD的可修航天测控系统任务可靠性分析

doi: 10.13224/j.cnki.jasp.2016.05.006
详细信息
    作者简介:

    孟礼(1986-),男,辽宁凌海人,博士生,主要从事装备系统分析与管理决策研究.

  • 中图分类号: V57

Mission reliability analysis of repairable space TT&C system based on OBDD

  • 摘要: 基于顺序二元决策图(OBDD)理论,针对航天测控系统(TT&C系统)特点定义了新的OBDD数据结构,提出了一种考虑设备可修的TT&C系统任务可靠性分析方法.通过将各测控站的时间窗口划分为不同阶段,分析各阶段内设备逻辑关系并构建阶段OBDD模型,然后将所有阶段OBDD模型合并为最终的任务OBDD模型.采用连续时间Markov链(CTMC)分析可修设备的状态转移行为,基于新的OBDD数据结构给出了任务可靠性计算算法.与Markov方法和仿真方法的对比分析结果表明:所提出的方法能够精确计算设备可修的TT&C系统任务可靠性,设备数量多于30个时算法效率高于Markov方法.

     

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出版历程
  • 收稿日期:  2015-10-10
  • 刊出日期:  2016-05-28

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