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Nöldeke et al., 2024 - Google Patents

FPGA-Based Fault Tolerance Framework for Avionics Systems

Nöldeke 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 …
Continue reading at ieeexplore.ieee.org (other versions)

Classifications

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    • G06F11/20Error 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
    • G06F11/202Error 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 where processing functionality is redundant
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    • G06F11/2097Error 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 maintaining the standby controller/processing unit updated
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