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飞船环控生保系统主要故障模型分析及飞控对策

The primary malfunction model analysis and aviation countermeasure for the Environmental Control and Life Support system of manned-spacecraft

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【作者】 董文平邓一兵傅岚陈善广

【Author】 DONG Wen-ping, DENG Yi-bing, FU Lan,CHENG Shan-guang (Institute of Space Medico-Engineering ,Beijing 100094,China)

【机构】 航天医学工程研究所航天医学工程研究所 北京100094北京100094北京100094

【摘要】 研究了载人飞船环控生保系统主要故障模型及飞控对策,根据系统工作原理建立了影响飞行安全的主要故障模型,如舱体泄漏、气源消耗过量和CO2净化失效等,应用该类模型对飞行数据进行实时处理,判断或预测故障,同时给出飞控对策。该方法已成功应用于首次载人飞行。

【Abstract】 In this paper malfunction models and aviation countermeasure for the Environmental Control &Life Support System(ECLSS) of manned-spacecraft were studied. The primary malfunction models which would affect flight safety, such as chamber leakage, gas storage excessively consumed, carbon-dioxide decontamination failure, etc, were conducted from system schematic diagram, and used to analyze flight data dynamically for failure judgement, from above the countermeasure could be derived. This method was applied in the first manned-space flight successfully.

  • 【文献出处】 宇航学报 ,Journal of Astronautics , 编辑部邮箱 ,2004年04期
  • 【分类号】V444.3
  • 【被引频次】6
  • 【下载频次】206
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