2008 IEEE/AIAA 27th Digital Avionics Systems Conference 2008
DOI: 10.1109/dasc.2008.4702751
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System considerations for robust time and space partitioning in Integrated Modular Avionics

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Cited by 16 publications
(6 citation statements)
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“…It becomes much more complex when such systems deploy multi-core processors. In single-core systems temporal isolation with respect to shared resources has to be considered only if Direct Memory Access (DMA)-capable peripheral devices or interrupts are enabled [7]. By means of abstraction layers, device drivers and disabling of unpredictable interrupts it is possible to avoid any unintended parallel accesses of processing cores and peripheral devices to memory.…”
Section: Resource Capacity Enforcementmentioning
confidence: 99%
“…It becomes much more complex when such systems deploy multi-core processors. In single-core systems temporal isolation with respect to shared resources has to be considered only if Direct Memory Access (DMA)-capable peripheral devices or interrupts are enabled [7]. By means of abstraction layers, device drivers and disabling of unpredictable interrupts it is possible to avoid any unintended parallel accesses of processing cores and peripheral devices to memory.…”
Section: Resource Capacity Enforcementmentioning
confidence: 99%
“…Such mechanisms raise new issues regarding several high-level requirements including robust partitioning. Existing studies, such as [7] and [8] have identified some of those mechanisms and their related issues for multicore certification.…”
Section: Multicore Specific Issues With Robust Partitioningmentioning
confidence: 99%
“…For aircraft, only a limited number of LRUs can be added because they have space, weight, and power (SWaP) constraints. Therefore, to deal with more features in aircraft, the IMA architecture [17,18] has been proposed.…”
Section: Avionics Systemmentioning
confidence: 99%
“…However, many systems operate on one hardware backbone, and it is necessary to guarantee the execution of each system. For this, the partitioning mechanism [18] following the ARINC 653 standard [13] is applied to avionics systems. Furthermore, virtualization-based methods, such as a hypervisor, provide legacy software compatibility with integrated hardware [20,21].…”
Section: Avionics Systemmentioning
confidence: 99%