APPLICATION OF THE FAULT-TOLERANT DEADLINE MECHANISM TO A SATELLITE ON-BOARD COMPUTER SYSTEM.

Anthony Y. Wei, Kenji Hiraishi, Ray Cheng, Roy H. Campbell

Research output: Contribution to conferencePaper

Abstract

Application of the fault-tolerant deadline mechanism to a satellite on-board computer system is described using extended Path Pascal as a vehicle. The MMS (Multimission Modular Spacecraft), a satellite designed by NASA for the 1980s, is used as a model. The results of the research demonstrate the potential of the deadline mechanism for programming fault-tolerant real-time processes.

Original languageEnglish (US)
Pages107-109
Number of pages3
StatePublished - Jan 1 1980
Externally publishedYes
EventDig Pap FTCS 10, Int Symp on Fault-Tolerant Comput, 10th - Kyoto, Jpn
Duration: Oct 1 1980Oct 3 1980

Conference

ConferenceDig Pap FTCS 10, Int Symp on Fault-Tolerant Comput, 10th
CityKyoto, Jpn
Period10/1/8010/3/80

ASJC Scopus subject areas

  • Engineering(all)

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  • Cite this

    Wei, A. Y., Hiraishi, K., Cheng, R., & Campbell, R. H. (1980). APPLICATION OF THE FAULT-TOLERANT DEADLINE MECHANISM TO A SATELLITE ON-BOARD COMPUTER SYSTEM.. 107-109. Paper presented at Dig Pap FTCS 10, Int Symp on Fault-Tolerant Comput, 10th, Kyoto, Jpn, .