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- W2068118873 abstract "Computing systems are employed for aerospace applications with high reliability requirements. In order to provide the needed reliability, it was necessary to make use of computing systems with fault-tolerance characteristics. Traditionally, fault tolerance is achieved through the use of hardware redundance. However, fault-tolerant techniques based on suitable software design considerations have also been developed. The present paper is concerned with the major issues arising in the context of an application of fault-tolerant software techniques to dynamic systems. Attention is given to fault-tolerant flight software, software component stability, system stability with fault-tolerant software, the preservation of functional performance, N-version vs. recovery blocks in flight software, systems-based software, static and dynamic models, static and dynamic consistency tests, and recovery block initialization." @default.
- W2068118873 created "2016-06-24" @default.
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- W2068118873 date "1985-08-17" @default.
- W2068118873 modified "2023-10-09" @default.
- W2068118873 title "Systems approach to software fault tolerance" @default.
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- W2068118873 doi "https://doi.org/10.2514/6.1985-6018" @default.
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