Architecture framework for spacecraft computer control safety system

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Abstract

We have a strong demand to design computer control safety system because crew stats to stay the international space station continuously, but there is no design framework for spacecraft computer control safety system. In this paper, we propose the architecture framework for spacecraft computer control safety system to guide a safety systems engineer to design computer controlled safety system. This framework is based on the general safety design process and NASA's computer safety requirements. The architecture framework can be proposed in accordance with the coming new IEEE1471 standard. This architecture framework can cover all design processes which are mandatory to be conducted to design system safety architecture. From this result, we suppose that this architecture framework reaches at least mandatory level.

Original languageEnglish
Title of host publication20th Annual International Symposium of the International Council on Systems Engineering, INCOSE 2010
Pages1250-1262
Number of pages13
Volume2
Publication statusPublished - 2010
Event20th Annual International Symposium of the International Council on Systems Engineering, INCOSE 2010 - Chicago, IL, United States
Duration: 2010 Jul 122010 Jul 15

Other

Other20th Annual International Symposium of the International Council on Systems Engineering, INCOSE 2010
CountryUnited States
CityChicago, IL
Period10/7/1210/7/15

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ASJC Scopus subject areas

  • Hardware and Architecture
  • Information Systems
  • Control and Systems Engineering

Cite this

Shirasaka, S. (2010). Architecture framework for spacecraft computer control safety system. In 20th Annual International Symposium of the International Council on Systems Engineering, INCOSE 2010 (Vol. 2, pp. 1250-1262)