Nöldeke et al., 2024 - Google Patents
FPGA-Based Fault Tolerance Framework for Avionics SystemsNöldeke et al., 2024
- Document ID
- 16778606304220660678
- Author
- Nöldeke P
- Lukić B
- Durak U
- Publication year
- Publication venue
- 2024 AIAA DATC/IEEE 43rd Digital Avionics Systems Conference (DASC)
External Links
Snippet
Fault tolerance is a key element in the design of safety-critical avionics systems. Thus, they must be capable of enduring a specified number of random component failures to be considered adequate for safety-critical applications. Nevertheless, the occurrence of a fault …
- 238000013461 design 0 abstract description 33
Classifications
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- G06F11/16—Error detection or correction of the data by redundancy in hardware
- G06F11/20—Error detection or correction of the data by redundancy in hardware using active fault-masking, e.g. by switching out faulty elements or by switching in spare elements
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- G06F11/0706—Error or fault processing not based on redundancy, i.e. by taking additional measures to deal with the error or fault not making use of redundancy in operation, in hardware, or in data representation the processing taking place on a specific hardware platform or in a specific software environment
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