航天器ORU模块热插拔检测方法

Cai Yaxing, W. Tao, Ma Pingxin
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引用次数: 0

摘要

对于传统航天器的ORU模块在轨更换,需要在更换操作前将待更换模块设置为关机禁用状态。模块的相关事务长期中断,极大地影响了航天器的正常工作。提出了一种ORU模块在轨热插拔检测方法。从通信链路和电气方面描述了热插拔检测过程。该方法实现了航天器内ORU模块的热插拔和即插即用,缩短了模块业务中断时间,为即插即用航天器的研制提供了一种新的即插即用检测方法。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
A hot swap detection method for ORU modules of spacecraft
For on-orbit replacement of ORU module of traditional spacecraft, it is necessary to set the module to be replaced to the state of power off and disabled before replacement operation. The related transactions of module have been interrupted for a long time, and the normal function of spacecraft has been greatly affected. This paper presents an on-orbit hot swap detection method for ORU modules. The hot swap detection process is described from both communication links and electrical aspects. The method is used to realize live hot swap and plug-and-play of ORU modules in spacecraft, shorten the interruption time of module services, and provide a new plug-and-play detection method for the development of plug-and-play spacecraft.
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