The invention provides a lightweight spacecraft minimum safety system and an implementation method, aiming at reliable operation of a spacecraft in orbit, through configuration optimization of the minimum safety system, orderly power-up, cold and hot start and control time sequence configuration design are carried out on each component unit, and the reliability of the spacecraft is improved. The system configuration and construction method suitable for reliable operation of the lightweight spacecraft is provided, safe starting control logic and safe mode switching control logic of the spacecraft are achieved, communication of spaceflight energy flow, control flow and information flow can be ensured, the spacecraft operates orderly based on a minimum safety system, and the reliability of the spacecraft is improved. And effective support is provided for autonomous, safe and stable operation of spacecraft faults and ground emergency rescue. Through the configuration and construction method for the minimum safety system of the lightweight spacecraft, the reliability and safety of on-orbit autonomous execution of the lightweight spacecraft can be improved, and the influence of on-orbit faults on the safety of the spacecraft is reduced.
本发明提供了一种轻量化航天器最小安全系统及实现方法,针对航天器在轨的可靠性运行,通过最小安全系统配置优化,对各组成单元有序加电、冷热启动和控制时序配置设计,提出了一种适合轻量化航天器可靠运行的系统配置和构建方法,实现了航天器安全启动控制逻辑和安全模式切换控制逻辑,可确保航天能源流、控制流和信息流程的贯通,航天器基于最小安全系统的有序运行,为航天器故障自主安全稳定运行和地面应急抢救提供有效支撑。通过本发明一种轻量化航天器最小安全系统配置和构建方法,可提高轻量化航天器在轨的自主执行的可靠性、安全性,减小在轨故障对航天器安全的影响。
Lightweight spacecraft minimum safety system and implementation method
轻量化航天器最小安全系统及实现方法
10.12.2024
Patent
Elektronische Ressource
Chinesisch
IPC: | B64G Raumfahrt , COSMONAUTICS |
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