OLT(RE)2: an On-Line on-demand Testing approach for permanent Radiation Effects in REconfigurable systems

Reconfigurable systems gained great interest in a wide range of application fields, including aerospace, where electronic devices are exposed to a very harsh working environment. Commercial SRAM-based FPGA devices represent an extremely interesting hardware platform for this kind of systems since they combine low cost with the possibility to utilize state-of-the-art processing power as well as the flexibility of reconfigurable hardware. In this paper we present OLT(RE)2: an on-line on-demand approach to test permanent faults induced by radiation in reconfigurable systems used in space missions. The proposed approach relies on a test circuit and on custom place-and-route algorithms. OLT(RE)2 exploits partial dynamic reconfigurability offered by today’s SRAM-based FPGAs to place the test circuits at run-time. The goal of OLT(RE)2 is to test unprogrammed areas of the FPGA before using them, thus preventing functional modules of the reconfigurable system to be placed on areas with faulty resources. Experimental results have shown that (i) it is possible to generate, place and route the test circuits needed to detect on average more than 99 % of the physical wires and on average about 97 % of the programmable interconnection points of an arbitrary large region of the FPGA in a reasonable time and that (ii) it is possible to download and run the whole test suite on the target device without interfering with the normal functioning of the system

Design and implementation of a routing algorithm to maximize test coverage of permanent faults in FPGAs

Nowadays electronic devices are used in a huge number of applications, from entertainment market to military equipment, from mobile phones to satellites. Each application has its own requirements and constraints depending on its purpose. One particular kind of applications is the one called mission critical that is characterized by a large amount of money that could be lost if something goes wrong. As an example this is the case of satellites that cannot be repaired or returned for maintenance if some parts stop working. When electronic device, and in particular FPGAs, are used in mission critical applications their reliability requires a special attention, therefore a key aspect of them is the capability to tolerate faults. When FPGAs operate in harsh environment, like in space, both temporary and permanent faults can occur due to radiation. The on-line testing technique involves a testing circuit that is capable to test its own used resources. In this work a design and implementation of a routing algorithm to maximize fault coverage of permanent faults is presented

Characterisation and mitigation of long-term degradation effects in programmable logic

Reliability has always been an issue in silicon device engineering, but until now it has been managed by the carefully tuned fabrication process. In the future the underlying physical limitations of silicon-based electronics, plus the practical challenges of manufacturing with such complexity at such a small scale, will lead to a crunch point where transistor-level reliability must be forfeited to continue achieving better productivity. Field-programmable gate arrays (FPGAs) are built on state-of-the-art silicon processes, but it has been recognised for some time that their distinctive characteristics put them in a favourable position over application-specific integrated circuits in the face of the reliability challenge. The literature shows how a regular structure, interchangeable resources and an ability to reconfigure can all be exploited to detect, locate, and overcome degradation and keep an FPGA application running. To fully exploit these characteristics, a better understanding is needed of the behavioural changes that are seen in the resources that make up an FPGA under ageing. Modelling is an attractive approach to this and in this thesis the causes and effects are explored of three important degradation mechanisms. All are shown to have an adverse affect on FPGA operation, but their characteristics show novel opportunities for ageing mitigation. Any modelling exercise is built on assumptions and so an empirical method is developed for investigating ageing on hardware with an accelerated-life test. Here, experiments show that timing degradation due to negative-bias temperature instability is the dominant process in the technology considered. Building on simulated and experimental results, this work also demonstrates a variety of methods for increasing the lifetime of FPGA lookup tables. The pre-emptive measure of wear-levelling is investigated in particular detail, and it is shown by experiment how di fferent reconfiguration algorithms can result in a significant reduction to the rate of degradation

Characterization of Interconnection Delays in FPGAS Due to Single Event Upsets and Mitigation

RÉSUMÉ L’utilisation incessante de composants électroniques à géométrie toujours plus faible a engendré de nouveaux défis au fil des ans. Par exemple, des semi-conducteurs à mémoire et à microprocesseur plus avancés sont utilisés dans les systèmes avioniques qui présentent une susceptibilité importante aux phénomènes de rayonnement cosmique. L'une des principales implications des rayons cosmiques, observée principalement dans les satellites en orbite, est l'effet d'événements singuliers (SEE). Le rayonnement atmosphérique suscite plusieurs préoccupations concernant la sécurité et la fiabilité de l'équipement avionique, en particulier pour les systèmes qui impliquent des réseaux de portes programmables (FPGA). Les FPGA à base de cellules de mémoire statique (SRAM) présentent une solution attrayante pour mettre en oeuvre des systèmes complexes dans le domaine de l’avionique. Les expériences de rayonnement réalisées sur les FPGA ont dévoilé la vulnérabilité de ces dispositifs contre un type particulier de SEE, à savoir, les événements singuliers de changement d’état (SEU). Un SEU est considérée comme le changement de l'état d'un élément bistable (c'est-à-dire, un bit-flip) dû à l'effet d'un ion, d'un proton ou d’un neutron énergétique. Cet effet est non destructif et peut être corrigé en réécrivant la partie de la SRAM affectée. Les changements de délai (DC) potentiels dus aux SEU affectant la mémoire de configuration de routage ont été récemment confirmés. Un des objectifs de cette thèse consiste à caractériser plus précisément les DC dans les FPGA causés par les SEU. Les DC observés expérimentalement sont présentés et la modélisation au niveau circuit de ces DC est proposée. Les circuits impliqués dans la propagation du délai sont validés en effectuant une modélisation précise des blocs internes à l'intérieur du FPGA et en exécutant des simulations. Les résultats montrent l’origine des DC qui sont en accord avec les mesures expérimentales de délais. Les modèles proposés au niveau circuit sont, aux meilleures de notre connaissance, le premier travail qui confirme et explique les délais combinatoires dans les FPGA. La conception d'un circuit moniteur de délai pour la détection des DC a été faite dans la deuxième partie de cette thèse. Ce moniteur permet de détecter un changement de délai sur les sections critiques du circuit et de prévenir les pannes de synchronisation engendrées par les SEU sans utiliser la redondance modulaire triple (TMR).----------ABSTRACT The unrelenting demand for electronic components with ever diminishing feature size have emerged new challenges over the years. Among them, more advanced memory and microprocessor semiconductors are being used in avionic systems that exhibit a substantial susceptibility to cosmic radiation phenomena. One of the main implications of cosmic rays, which was primarily observed in orbiting satellites, is single-event effect (SEE). Atmospheric radiation causes several concerns regarding the safety and reliability of avionics equipment, particularly for systems that involve field programmable gate arrays (FPGA). SRAM-based FPGAs, as an attractive solution to implement systems in aeronautic sector, are very susceptible to SEEs in particular Single Event Upset (SEU). An SEU is considered as the change of the state of a bistable element (i.e., bit-flip) due to the effect of an energetic ion or proton. This effect is non-destructive and may be fixed by rewriting the affected part. Sensitivity evaluation of SRAM-based FPGAs to a physical impact such as potential delay changes (DC) has not been addressed thus far in the literature. DCs induced by SEU can affect the functionality of the logic circuits by disturbing the race condition on critical paths. The objective of this thesis is toward the characterization of DCs in SRAM-based FPGAs due to transient ionizing radiation. The DCs observed experimentally are presented and the circuit-level modeling of those DCs is proposed. Circuits involved in delay propagation are reverse-engineered by performing precise modeling of internal blocks inside the FPGA and executing simulations. The results show the root cause of DCs that are in good agreement with experimental delay measurements. The proposed circuit level models are, to the best of our knowledge, the first work on modeling of combinational delays in FPGAs.In addition, the design of a delay monitor circuit for DC detection is investigated in the second part of this thesis. This monitor allowed to show experimentally cumulative DCs on interconnects in FPGA. To this end, by avoiding the use of triple modular redundancy (TMR), a mitigation technique for DCs is proposed and the system downtime is minimized. A method is also proposed to decrease the clock frequency after DC detection without interrupting the process