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Research on approach of reliability design and evaluation for space launching systems based on mission sections

机译:基于任务部分的空间发射系统可靠性设计与评估方法研究

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With the increasing of the number and type of space launch activities, the demands for space launch system also diverse from each other. In order to save the cost of space launch, it is necessary to carry out the mission based reliability analysis of space launch. The reliability of space launch based on mission section is the ability of the space launch system to fulfil the specified function in the specified mission section. It considers only the failures that affect the completion of the mission, and functions that are irrelevant with the mission are not concerned. Based on the mission reliability model, the limited human, material and financial resources can be used to fulfil the functions that are closely related with the success or failure of the mission. It is helpful to reduce the cost and the risk of space launch. In this paper, based on the fuzzy mathematics, the probability of failure mode effect is defined and given in the FMECA, and in this paper, based on Failure Mode Effects and Criticality Analysis (FMECA), introducing the fuzzy mathematics, FFMECA method is formed. Firstly, the space launch mission is analysed using the mission flow. Then, the failure modes that affect the success of the mission are distinguished in the form of quantification by the probability of failure mode effect given in the FMECA. Finally, the mission reliability is evaluated using the probability of FMECA. And the vulnerable spot of the mission can be obtained. So we can optimize the system or the flow to improve its reliability of the space launch mission. Taking a typical space launch mission for instance, by the above method, the model of reliability of the space launch mission was constructed. The quantitative and qualitative analysis of different mission sections was carried out. The result of reliability for the mission can be acquired. Application of this method can effectively guide mission and system design to improve the reliability and it is significant for the eng
机译:随着空间发射活动的数量和类型的增加,空间发射系统的需求也彼此多样化。为了节省空间推出的成本,有必要执行太空发射的基于任务的可靠性分析。基于任务部分的空间启动的可靠性是空间发射系统符合指定任务部分中指定函数的能力。它仅考虑影响特派团完成的失败,以及与使命无关的功能并不担心。基于任务可靠性模型,可以使用有限的人力,材料和金融资源来满足与使命的成功或失败密切相关的功能。降低成本和太空发射风险有助于。本文基于模糊数学,在FMECA中定义和给出了故障模式效应的概率,并在本文中,基于故障模式效应和临界分析(FMECA),引入模糊数学,形成FFMeca方法。首先,使用任务流程分析空间启动任务。然后,影响任务成功的失败模式以定量的形式以尺寸的故障模式效应在FMECA中的概率区分。最后,使用FMECA的概率来评估任务可靠性。并且可以获得任务的脆弱点。因此,我们可以优化系统或流程,以提高其空间发射任务的可靠性。例如,采用典型的空间发射使命,通过上述方法,构建了空间发射任务的可靠性模型。进行了不同任务部分的定量和定性分析。可以获得使命的可靠性的结果。这种方法的应用可以有效地指导任务和系统设计来提高可靠性,这对eng的重要性是重要的

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