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 language | English (US) |
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Pages | 107-109 |
Number of pages | 3 |
State | Published - 1980 |
Externally published | Yes |
Event | Dig Pap FTCS 10, Int Symp on Fault-Tolerant Comput, 10th - Kyoto, Jpn Duration: Oct 1 1980 → Oct 3 1980 |
Conference
Conference | Dig Pap FTCS 10, Int Symp on Fault-Tolerant Comput, 10th |
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City | Kyoto, Jpn |
Period | 10/1/80 → 10/3/80 |
ASJC Scopus subject areas
- General Engineering