A study of monitoring and reconfiguration electronics design in space computer unit

위성컴퓨터의 감시 및 재구성 회로 설계에 관한 연구

  • Published : 2009.07.14

Abstract

This paper describes an MRE(Monitoring and Reconfiguration Electronics) which is in charge of SCU(Spacecraft Computer Unit) hardware failure monitoring as well as of protecting the satellite against system failures. To achieve it, MRE is designed that it is an independent function with respect to the rest of the SCU, that is, care is taken into account in order to minimize the interface(the failure propagation) between the MRE and the other SCU functions.

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