Abstract
With the onset of multi- and many-core chips, the single-core market is closing down. Those chips constitute a new challenge for aerospace and safety-critical industries in general. Little is known about the certification of software running on these systems. There is therefore a strong need for developing software architectures based on multi-core architectures, yet compliant with safety-criticality constraints. This paper presents a reconfigurable multi-core architecture and the safety-criticality constraints for airborne systems. The last section uses the current certification guidance to explain how the architecture can satisfy these constraints even with dynamic features activated.
Original language | English (US) |
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Title of host publication | AIAA/IEEE Digital Avionics Systems Conference - Proceedings |
Publisher | Institute of Electrical and Electronics Engineers Inc. |
ISBN (Print) | 9781509056002 |
DOIs | |
State | Published - Dec 7 2016 |
Externally published | Yes |