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Analyzing method and system for dangerous events of long-term on-orbit manned spacecraft

A technology for manned spacecraft and dangerous events, applied in the field of overall spacecraft design, can solve problems such as the inability to support the quantitative calculation of astronaut evacuation probability, the inability to identify and analyze hazards, and the consumption of large system resources, so as to promote safety qualitative , The system layout is simple and clear, and the effect of small system resource cost

Active Publication Date: 2019-02-12
BEIJING SPACE TECH RES & TEST CENT
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Problems solved by technology

[0004] 1. Failure to identify and analyze hazards due to on-orbit maintenance operations;
[0005] 2. It cannot support the quantitative calculation of the probability of astronauts evacuating due to failures during the long-term operation of manned spacecraft;
[0006] 3. Due to the long flight time and too many risk factors identified, a large amount of system resources are required to support safety control measures

Method used

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  • Analyzing method and system for dangerous events of long-term on-orbit manned spacecraft
  • Analyzing method and system for dangerous events of long-term on-orbit manned spacecraft

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Embodiment approach

[0043] In the present invention, based on the fault tree analysis method, the risk control is carried out for the long-term on-orbit operation of large manned spacecraft. As can be seen from the above, according to one embodiment of the present invention, the manned spacecraft long-term on-orbit dangerous event analysis method of the present invention specifically includes:

[0044] Step a: Determine the dangerous events during the manned spacecraft’s on-orbit operation, that is, determine the undesired failure consequence state during the manned spacecraft’s on-orbit operation. Then the consequence state of the dangerous event of the manned spacecraft is analyzed, and the severity level of the dangerous event is analyzed.

[0045] Step b: Carry out functional analysis of the manned spacecraft, and on the basis of the functional analysis of the manned spacecraft, classify the functions of the manned spacecraft according to dangerous events. Specifically, it is to establish a ...

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Abstract

The invention relates to a long-term on-orbit danger event analysis method of a manned spacecraft and a danger analysis system. The analysis method comprises the following steps: a, determining dangerevents in an on-orbit process of the manned spacecraft, and analyzing consequence status and severity levels of the danger events; b, carrying out function analysis on the manned spacecraft, and carrying out hierarchical division on functions of the manned spacecraft according to the danger events; c, identifying sources of danger that can lead to danger events; d, analyzing a sequence of dangerevents caused by each danger source, determining severity degrees of the danger events, and analyzing risk of fault consequences of the danger events; and e, for high-risk danger events, using fault tree analysis to fault trees in a prioritized manner for reanalysis. According to the analysis method of the invention, serious dangers which may occur in the on-orbit running process are identified, system resource cost minimization of safety control measures is ensured, and maximum efficiency is realized.

Description

technical field [0001] The invention relates to the technical field of overall design of spacecraft, in particular to a method for analyzing a manned spacecraft's long-term on-orbit dangerous event and a manned spacecraft risk analysis system. Background technique [0002] The primary task of manned spacecraft in orbit is to ensure the safety of astronauts. With the development of manned spacecraft in the direction of complexity, large-scale and long-term orbital flight, the hazards that can cause serious consequences are becoming more and more serious. If a catastrophic accident occurs, it will cause casualties and heavy property losses. In the design stage of manned spacecraft, it is necessary to carry out the analysis of hazard sources and hazardous events, and through the control and elimination of hazards, the safety of the spacecraft is guaranteed to be at an acceptable level. [0003] Since my country has no long-term experience of large-scale manned spacecraft opera...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G06F17/50
CPCG06F30/15
Inventor 杨宏李伟夏侨丽张伟李涛李志海王岩王为张健刘铭吴冰陈伯翰
Owner BEIJING SPACE TECH RES & TEST CENT
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