Design Considerations in Boeing 777 Fly-By-Wire Computers
HASE '98 The 3rd IEEE International Symposium on High-Assurance Systems Engineering
Design of self-checking software
Proceedings of the international conference on Reliable software
ACM Transactions on Computer-Human Interaction (TOCHI)
DSVIS'06 Proceedings of the 13th international conference on Interactive systems: Design, specification, and verification
Self-Checking Components for Dependable Interactive Cockpits Using Formal Description Techniques
PRDC '11 Proceedings of the 2011 IEEE 17th Pacific Rim International Symposium on Dependable Computing
Addressing dependability for interactive systems: application to interactive cockpits
Proceedings of the 5th ACM SIGCHI symposium on Engineering interactive computing systems
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The deployment of interactive facilities in avionic digital cockpits for critical applications is a challenge today. The dependability of the user interface and its related supporting software must be consistent with the criticality of the functions to be controlled. The approach proposed in this paper aims at describing how fault prevention and fault tolerance techniques can be combined to address this challenge. Following the ARINC 661 standard, a model-based development of interactive objects (namely widgets and layers) aims at providing zero-default software. Regarding remaining software faults in the underlying runtime support and also physical faults, the approach is based on fault tolerance design patterns, like self-checking components and replication techniques. The proposed solution relies on the space and time partitioning provided by the executive support following the ARINC 653 standard. Defining and designing resilient interactive cockpits is a necessity in the near future as these command and control systems provide a great opportunity to improve maintenance and evolutivity of avionic systems.