The invention relates to a safety state monitoring system for a manned spacecraft in long-term in-orbit operation. The system comprises a telemetry data receiving module, a dangerous event monitoring module and a dangerous source state monitoring module, the telemetry data receiving module is used for receiving downlink telemetry parameters of the manned spacecraft running in orbit; the dangerous event monitoring module is used for judging whether a dangerous event occurs or not according to environment monitoring telemetry parameters, corresponding to the dangerous event, of the manned spacecraft, and sending a dangerous event judgment result to the comprehensive evaluation module; the danger source state monitoring module is used for judging the safety state of the danger source according to whether the telemetering parameters of the danger source are within a preset value range or not; and the comprehensive evaluation module is used for judging whether the manned spacecraft is in a safe state or not according to the dangerous event judgment result, the consequence severity degree of the dangerous source and the safe state of the dangerous source.
本发明涉及一种长期在轨运行载人航天器安全状态监控系统,该系统包括遥测数据接收模块、危险事件监控模块、危险源状态监控模块;遥测数据接收模块,用于接收在轨运行的载人航天器下行遥测参数;危险事件监控模块,根据载人航天器与危险事件相应的环境监测遥测参数,判断是否发生危险事件,将危险事件判断结果发送给综合评定模块;危险源状态监控模块,根据危险源的遥测参数是否在预设的取值范围之内,判定危险源的安全状态;综合评定模块,根据危险事件判断结果、危险源的后果严重程度、危险源的安全状态,判定载人航天器是否为安全状态。
Long-term on-orbit operation manned spacecraft safety state monitoring system
一种长期在轨运行载人航天器安全状态监控系统
2025-03-07
Patent
Electronic Resource
Chinese
IPC: | B64G Raumfahrt , COSMONAUTICS |
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