COTS-Based Fault Tolerance in Deep Space: Qualitative and Quantitative Analyses of a Bus Network Architecture
نویسندگان
چکیده
Among the COTS applications in the X2000 architecture for deep-space missions, the use of commercial bus standards is the highest-payoff COTS application since a bus interface has a global impact and enabling effect on system cost and capability, respectively. While COTS bus standards enable significant cost reductions, it is a great challenge for us to deliver a highly-reliable long-term survivable system employing COTS standards that are not developed for mission-critical applications. The spirit of our solution to the problem is to exploit the pertinent standard features of a COTS product to circumvent its shortcomings, though these standard features may not be originally designed for highly reliable systems. In this paper, we discuss our experiences and findings on the design and assessment of an IEEE 1394 compliant fault-tolerant bus architecture. We first derive and qualitatively analyze a “stack-tree topology” that not only complies with IEEE 1394 but also enables the implementation of a fault-tolerant bus architecture without node redundancy. We then present a quantitative evaluation that demonstrates significant reliability improvement from the COTS-based fault tolerance.
منابع مشابه
The Design of a Fault-Tolerant COTS-Based Bus Architecture for Space Applications*
The high-performance, scalability and miniaturization requirements together with the power, mass and cost constraints mandate the use of commercial-off-the-shelf (COTS) components and standards in the X2000 avionics system architecture for deep-space missions. In this paper, we report our experiences and findings on the design of an IEEE 1394 compliant fault-tolerant COTS-based bus architecture...
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