1,128 research outputs found

    Partial TMR in FPGAs Using Approximate Logic Circuits

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    TMR is a very effective technique to mitigate SEU effects in FPGAs, but it is often expensive in terms of FPGA resource utilization and power consumption. For certain applications, Partial TMR can be used to trade off the reliability with the cost of mitigation. In this work we propose a new approach to build Partial TMR circuits for FPGAs using approximate logic circuits. This approach is scalable, with a fine granularity, and can provide a flexible balance between reliability and overheads. The proposed approach has been validated by the results of fault injection experiments and proton irradiation campaigns.This work was supported in part by the Spanish Ministry of Economy and Competitiveness under contract ESP2015-68245-C4-1-P

    Autonomous Recovery Of Reconfigurable Logic Devices Using Priority Escalation Of Slack

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    Field Programmable Gate Array (FPGA) devices offer a suitable platform for survivable hardware architectures in mission-critical systems. In this dissertation, active dynamic redundancy-based fault-handling techniques are proposed which exploit the dynamic partial reconfiguration capability of SRAM-based FPGAs. Self-adaptation is realized by employing reconfiguration in detection, diagnosis, and recovery phases. To extend these concepts to semiconductor aging and process variation in the deep submicron era, resilient adaptable processing systems are sought to maintain quality and throughput requirements despite the vulnerabilities of the underlying computational devices. A new approach to autonomous fault-handling which addresses these goals is developed using only a uniplex hardware arrangement. It operates by observing a health metric to achieve Fault Demotion using Recon- figurable Slack (FaDReS). Here an autonomous fault isolation scheme is employed which neither requires test vectors nor suspends the computational throughput, but instead observes the value of a health metric based on runtime input. The deterministic flow of the fault isolation scheme guarantees success in a bounded number of reconfigurations of the FPGA fabric. FaDReS is then extended to the Priority Using Resource Escalation (PURE) online redundancy scheme which considers fault-isolation latency and throughput trade-offs under a dynamic spare arrangement. While deep-submicron designs introduce new challenges, use of adaptive techniques are seen to provide several promising avenues for improving resilience. The scheme developed is demonstrated by hardware design of various signal processing circuits and their implementation on a Xilinx Virtex-4 FPGA device. These include a Discrete Cosine Transform (DCT) core, Motion Estimation (ME) engine, Finite Impulse Response (FIR) Filter, Support Vector Machine (SVM), and Advanced Encryption Standard (AES) blocks in addition to MCNC benchmark circuits. A iii significant reduction in power consumption is achieved ranging from 83% for low motion-activity scenes to 12.5% for high motion activity video scenes in a novel ME engine configuration. For a typical benchmark video sequence, PURE is shown to maintain a PSNR baseline near 32dB. The diagnosability, reconfiguration latency, and resource overhead of each approach is analyzed. Compared to previous alternatives, PURE maintains a PSNR within a difference of 4.02dB to 6.67dB from the fault-free baseline by escalating healthy resources to higher-priority signal processing functions. The results indicate the benefits of priority-aware resiliency over conventional redundancy approaches in terms of fault-recovery, power consumption, and resource-area requirements. Together, these provide a broad range of strategies to achieve autonomous recovery of reconfigurable logic devices under a variety of constraints, operating conditions, and optimization criteria

    Dependability-driven Strategies to Improve the Design and Verification of Safety-Critical HDL-based Embedded Systems

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    [ES] La utilización de sistemas empotrados en cada vez más ámbitos de aplicación está llevando a que su diseño deba enfrentarse a mayores requisitos de rendimiento, consumo de energía y área (PPA). Asimismo, su utilización en aplicaciones críticas provoca que deban cumplir con estrictos requisitos de confiabilidad para garantizar su correcto funcionamiento durante períodos prolongados de tiempo. En particular, el uso de dispositivos lógicos programables de tipo FPGA es un gran desafío desde la perspectiva de la confiabilidad, ya que estos dispositivos son muy sensibles a la radiación. Por todo ello, la confiabilidad debe considerarse como uno de los criterios principales para la toma de decisiones a lo largo del todo flujo de diseño, que debe complementarse con diversos procesos que permitan alcanzar estrictos requisitos de confiabilidad. Primero, la evaluación de la robustez del diseño permite identificar sus puntos débiles, guiando así la definición de mecanismos de tolerancia a fallos. Segundo, la eficacia de los mecanismos definidos debe validarse experimentalmente. Tercero, la evaluación comparativa de la confiabilidad permite a los diseñadores seleccionar los componentes prediseñados (IP), las tecnologías de implementación y las herramientas de diseño (EDA) más adecuadas desde la perspectiva de la confiabilidad. Por último, la exploración del espacio de diseño (DSE) permite configurar de manera óptima los componentes y las herramientas seleccionados, mejorando así la confiabilidad y las métricas PPA de la implementación resultante. Todos los procesos anteriormente mencionados se basan en técnicas de inyección de fallos para evaluar la robustez del sistema diseñado. A pesar de que existe una amplia variedad de técnicas de inyección de fallos, varias problemas aún deben abordarse para cubrir las necesidades planteadas en el flujo de diseño. Aquellas soluciones basadas en simulación (SBFI) deben adaptarse a los modelos de nivel de implementación, teniendo en cuenta la arquitectura de los diversos componentes de la tecnología utilizada. Las técnicas de inyección de fallos basadas en FPGAs (FFI) deben abordar problemas relacionados con la granularidad del análisis para poder localizar los puntos débiles del diseño. Otro desafío es la reducción del coste temporal de los experimentos de inyección de fallos. Debido a la alta complejidad de los diseños actuales, el tiempo experimental dedicado a la evaluación de la confiabilidad puede ser excesivo incluso en aquellos escenarios más simples, mientras que puede ser inviable en aquellos procesos relacionados con la evaluación de múltiples configuraciones alternativas del diseño. Por último, estos procesos orientados a la confiabilidad carecen de un soporte instrumental que permita cubrir el flujo de diseño con toda su variedad de lenguajes de descripción de hardware, tecnologías de implementación y herramientas de diseño. Esta tesis aborda los retos anteriormente mencionados con el fin de integrar, de manera eficaz, estos procesos orientados a la confiabilidad en el flujo de diseño. Primeramente, se proponen nuevos métodos de inyección de fallos que permiten una evaluación de la confiabilidad, precisa y detallada, en diferentes niveles del flujo de diseño. Segundo, se definen nuevas técnicas para la aceleración de los experimentos de inyección que mejoran su coste temporal. Tercero, se define dos estrategias DSE que permiten configurar de manera óptima (desde la perspectiva de la confiabilidad) los componentes IP y las herramientas EDA, con un coste experimental mínimo. Cuarto, se propone un kit de herramientas que automatiza e incorpora con eficacia los procesos orientados a la confiabilidad en el flujo de diseño semicustom. Finalmente, se demuestra la utilidad y eficacia de las propuestas mediante un caso de estudio en el que se implementan tres procesadores empotrados en un FPGA de Xilinx serie 7.[CA] La utilització de sistemes encastats en cada vegada més àmbits d'aplicació està portant al fet que el seu disseny haja d'enfrontar-se a majors requisits de rendiment, consum d'energia i àrea (PPA). Així mateix, la seua utilització en aplicacions crítiques provoca que hagen de complir amb estrictes requisits de confiabilitat per a garantir el seu correcte funcionament durant períodes prolongats de temps. En particular, l'ús de dispositius lògics programables de tipus FPGA és un gran desafiament des de la perspectiva de la confiabilitat, ja que aquests dispositius són molt sensibles a la radiació. Per tot això, la confiabilitat ha de considerar-se com un dels criteris principals per a la presa de decisions al llarg del tot flux de disseny, que ha de complementar-se amb diversos processos que permeten aconseguir estrictes requisits de confiabilitat. Primer, l'avaluació de la robustesa del disseny permet identificar els seus punts febles, guiant així la definició de mecanismes de tolerància a fallades. Segon, l'eficàcia dels mecanismes definits ha de validar-se experimentalment. Tercer, l'avaluació comparativa de la confiabilitat permet als dissenyadors seleccionar els components predissenyats (IP), les tecnologies d'implementació i les eines de disseny (EDA) més adequades des de la perspectiva de la confiabilitat. Finalment, l'exploració de l'espai de disseny (DSE) permet configurar de manera òptima els components i les eines seleccionats, millorant així la confiabilitat i les mètriques PPA de la implementació resultant. Tots els processos anteriorment esmentats es basen en tècniques d'injecció de fallades per a poder avaluar la robustesa del sistema dissenyat. A pesar que existeix una àmplia varietat de tècniques d'injecció de fallades, diverses problemes encara han d'abordar-se per a cobrir les necessitats plantejades en el flux de disseny. Aquelles solucions basades en simulació (SBFI) han d'adaptar-se als models de nivell d'implementació, tenint en compte l'arquitectura dels diversos components de la tecnologia utilitzada. Les tècniques d'injecció de fallades basades en FPGAs (FFI) han d'abordar problemes relacionats amb la granularitat de l'anàlisi per a poder localitzar els punts febles del disseny. Un altre desafiament és la reducció del cost temporal dels experiments d'injecció de fallades. A causa de l'alta complexitat dels dissenys actuals, el temps experimental dedicat a l'avaluació de la confiabilitat pot ser excessiu fins i tot en aquells escenaris més simples, mentre que pot ser inviable en aquells processos relacionats amb l'avaluació de múltiples configuracions alternatives del disseny. Finalment, aquests processos orientats a la confiabilitat manquen d'un suport instrumental que permeta cobrir el flux de disseny amb tota la seua varietat de llenguatges de descripció de maquinari, tecnologies d'implementació i eines de disseny. Aquesta tesi aborda els reptes anteriorment esmentats amb la finalitat d'integrar, de manera eficaç, aquests processos orientats a la confiabilitat en el flux de disseny. Primerament, es proposen nous mètodes d'injecció de fallades que permeten una avaluació de la confiabilitat, precisa i detallada, en diferents nivells del flux de disseny. Segon, es defineixen noves tècniques per a l'acceleració dels experiments d'injecció que milloren el seu cost temporal. Tercer, es defineix dues estratègies DSE que permeten configurar de manera òptima (des de la perspectiva de la confiabilitat) els components IP i les eines EDA, amb un cost experimental mínim. Quart, es proposa un kit d'eines (DAVOS) que automatitza i incorpora amb eficàcia els processos orientats a la confiabilitat en el flux de disseny semicustom. Finalment, es demostra la utilitat i eficàcia de les propostes mitjançant un cas d'estudi en el qual s'implementen tres processadors encastats en un FPGA de Xilinx serie 7.[EN] Embedded systems are steadily extending their application areas, dealing with increasing requirements in performance, power consumption, and area (PPA). Whenever embedded systems are used in safety-critical applications, they must also meet rigorous dependability requirements to guarantee their correct operation during an extended period of time. Meeting these requirements is especially challenging for those systems that are based on Field Programmable Gate Arrays (FPGAs), since they are very susceptible to Single Event Upsets. This leads to increased dependability threats, especially in harsh environments. In such a way, dependability should be considered as one of the primary criteria for decision making throughout the whole design flow, which should be complemented by several dependability-driven processes. First, dependability assessment quantifies the robustness of hardware designs against faults and identifies their weak points. Second, dependability-driven verification ensures the correctness and efficiency of fault mitigation mechanisms. Third, dependability benchmarking allows designers to select (from a dependability perspective) the most suitable IP cores, implementation technologies, and electronic design automation (EDA) tools. Finally, dependability-aware design space exploration (DSE) allows to optimally configure the selected IP cores and EDA tools to improve as much as possible the dependability and PPA features of resulting implementations. The aforementioned processes rely on fault injection testing to quantify the robustness of the designed systems. Despite nowadays there exists a wide variety of fault injection solutions, several important problems still should be addressed to better cover the needs of a dependability-driven design flow. In particular, simulation-based fault injection (SBFI) should be adapted to implementation-level HDL models to take into account the architecture of diverse logic primitives, while keeping the injection procedures generic and low-intrusive. Likewise, the granularity of FPGA-based fault injection (FFI) should be refined to the enable accurate identification of weak points in FPGA-based designs. Another important challenge, that dependability-driven processes face in practice, is the reduction of SBFI and FFI experimental effort. The high complexity of modern designs raises the experimental effort beyond the available time budgets, even in simple dependability assessment scenarios, and it becomes prohibitive in presence of alternative design configurations. Finally, dependability-driven processes lack an instrumental support covering the semicustom design flow in all its variety of description languages, implementation technologies, and EDA tools. Existing fault injection tools only partially cover the individual stages of the design flow, being usually specific to a particular design representation level and implementation technology. This work addresses the aforementioned challenges by efficiently integrating dependability-driven processes into the design flow. First, it proposes new SBFI and FFI approaches that enable an accurate and detailed dependability assessment at different levels of the design flow. Second, it improves the performance of dependability-driven processes by defining new techniques for accelerating SBFI and FFI experiments. Third, it defines two DSE strategies that enable the optimal dependability-aware tuning of IP cores and EDA tools, while reducing as much as possible the robustness evaluation effort. Fourth, it proposes a new toolkit (DAVOS) that automates and seamlessly integrates the aforementioned dependability-driven processes into the semicustom design flow. Finally, it illustrates the usefulness and efficiency of these proposals through a case study consisting of three soft-core embedded processors implemented on a Xilinx 7-series SoC FPGA.Tuzov, I. (2020). Dependability-driven Strategies to Improve the Design and Verification of Safety-Critical HDL-based Embedded Systems [Tesis doctoral]. Universitat Politècnica de València. https://doi.org/10.4995/Thesis/10251/159883TESI

    Using embedded hardware monitor cores in critical computer systems

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    The integration of FPGA devices in many different architectures and services makes monitoring and real time detection of errors an important concern in FPGA system design. A monitor is a tool, or a set of tools, that facilitate analytic measurements in observing a given system. The goal of these observations is usually the performance analysis and optimisation, or the surveillance of the system. However, System-on-Chip (SoC) based designs leave few points to attach external tools such as logic analysers. Thus, an embedded error detection core that allows observation of critical system nodes (such as processor cores and buses) should enforce the operation of the FPGA-based system, in order to prevent system failures. The core should not interfere with system performance and must ensure timely detection of errors. This thesis is an investigation onto how a robust hardware-monitoring module can be efficiently integrated in a target PCI board (with FPGA-based application processing features) which is part of a critical computing system. [Continues.

    Hardware morphogenetic developmental system

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    Indirect genotype to phenotype mappings in the form of developmental systems may allow better scalability to larger phenotypes in evolvable hardware. This report reviews developmental systems used in evolvable hardware and it proposes a new classifications based on hardware characteristics. It then describes a genetic encoding and developmental system called the morphogenetic system which has been designed for multi-cellular circuits. This morphogenetic system is inspired upon gene expression and cell differentiation but it focuses on efficient hardware implementation. An hardware implementation on the dynamically reconfigurable POEtic circuit is described. It uses serial arithmetics and time-multiplexing to minimize ressource use

    High-performance hardware accelerators for image processing in space applications

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    Mars is a hard place to reach. While there have been many notable success stories in getting probes to the Red Planet, the historical record is full of bad news. The success rate for actually landing on the Martian surface is even worse, roughly 30%. This low success rate must be mainly credited to the Mars environment characteristics. In the Mars atmosphere strong winds frequently breath. This phenomena usually modifies the lander descending trajectory diverging it from the target one. Moreover, the Mars surface is not the best place where performing a safe land. It is pitched by many and close craters and huge stones, and characterized by huge mountains and hills (e.g., Olympus Mons is 648 km in diameter and 27 km tall). For these reasons a mission failure due to a landing in huge craters, on big stones or on part of the surface characterized by a high slope is highly probable. In the last years, all space agencies have increased their research efforts in order to enhance the success rate of Mars missions. In particular, the two hottest research topics are: the active debris removal and the guided landing on Mars. The former aims at finding new methods to remove space debris exploiting unmanned spacecrafts. These must be able to autonomously: detect a debris, analyses it, in order to extract its characteristics in terms of weight, speed and dimension, and, eventually, rendezvous with it. In order to perform these tasks, the spacecraft must have high vision capabilities. In other words, it must be able to take pictures and process them with very complex image processing algorithms in order to detect, track and analyse the debris. The latter aims at increasing the landing point precision (i.e., landing ellipse) on Mars. Future space-missions will increasingly adopt Video Based Navigation systems to assist the entry, descent and landing (EDL) phase of space modules (e.g., spacecrafts), enhancing the precision of automatic EDL navigation systems. For instance, recent space exploration missions, e.g., Spirity, Oppurtunity, and Curiosity, made use of an EDL procedure aiming at following a fixed and precomputed descending trajectory to reach a precise landing point. This approach guarantees a maximum landing point precision of 20 km. By comparing this data with the Mars environment characteristics, it is possible to understand how the mission failure probability still remains really high. A very challenging problem is to design an autonomous-guided EDL system able to even more reduce the landing ellipse, guaranteeing to avoid the landing in dangerous area of Mars surface (e.g., huge craters or big stones) that could lead to the mission failure. The autonomous behaviour of the system is mandatory since a manual driven approach is not feasible due to the distance between Earth and Mars. Since this distance varies from 56 to 100 million of km approximately due to the orbit eccentricity, even if a signal transmission at the light speed could be possible, in the best case the transmission time would be around 31 minutes, exceeding so the overall duration of the EDL phase. In both applications, algorithms must guarantee self-adaptability to the environmental conditions. Since the Mars (and in general the space) harsh conditions are difficult to be predicted at design time, these algorithms must be able to automatically tune the internal parameters depending on the current conditions. Moreover, real-time performances are another key factor. Since a software implementation of these computational intensive tasks cannot reach the required performances, these algorithms must be accelerated via hardware. For this reasons, this thesis presents my research work done on advanced image processing algorithms for space applications and the associated hardware accelerators. My research activity has been focused on both the algorithm and their hardware implementations. Concerning the first aspect, I mainly focused my research effort to integrate self-adaptability features in the existing algorithms. While concerning the second, I studied and validated a methodology to efficiently develop, verify and validate hardware components aimed at accelerating video-based applications. This approach allowed me to develop and test high performance hardware accelerators that strongly overcome the performances of the actual state-of-the-art implementations. The thesis is organized in four main chapters. Chapter 2 starts with a brief introduction about the story of digital image processing. The main content of this chapter is the description of space missions in which digital image processing has a key role. A major effort has been spent on the missions in which my research activity has a substantial impact. In particular, for these missions, this chapter deeply analizes and evaluates the state-of-the-art approaches and algorithms. Chapter 3 analyzes and compares the two technologies used to implement high performances hardware accelerators, i.e., Application Specific Integrated Circuits (ASICs) and Field Programmable Gate Arrays (FPGAs). Thanks to this information the reader may understand the main reasons behind the decision of space agencies to exploit FPGAs instead of ASICs for high-performance hardware accelerators in space missions, even if FPGAs are more sensible to Single Event Upsets (i.e., transient error induced on hardware component by alpha particles and solar radiation in space). Moreover, this chapter deeply describes the three available space-grade FPGA technologies (i.e., One-time Programmable, Flash-based, and SRAM-based), and the main fault-mitigation techniques against SEUs that are mandatory for employing space-grade FPGAs in actual missions. Chapter 4 describes one of the main contribution of my research work: a library of high-performance hardware accelerators for image processing in space applications. The basic idea behind this library is to offer to designers a set of validated hardware components able to strongly speed up the basic image processing operations commonly used in an image processing chain. In other words, these components can be directly used as elementary building blocks to easily create a complex image processing system, without wasting time in the debug and validation phase. This library groups the proposed hardware accelerators in IP-core families. The components contained in a same family share the same provided functionality and input/output interface. This harmonization in the I/O interface enables to substitute, inside a complex image processing system, components of the same family without requiring modifications to the system communication infrastructure. In addition to the analysis of the internal architecture of the proposed components, another important aspect of this chapter is the methodology used to develop, verify and validate the proposed high performance image processing hardware accelerators. This methodology involves the usage of different programming and hardware description languages in order to support the designer from the algorithm modelling up to the hardware implementation and validation. Chapter 5 presents the proposed complex image processing systems. In particular, it exploits a set of actual case studies, associated with the most recent space agency needs, to show how the hardware accelerator components can be assembled to build a complex image processing system. In addition to the hardware accelerators contained in the library, the described complex system embeds innovative ad-hoc hardware components and software routines able to provide high performance and self-adaptable image processing functionalities. To prove the benefits of the proposed methodology, each case study is concluded with a comparison with the current state-of-the-art implementations, highlighting the benefits in terms of performances and self-adaptability to the environmental conditions

    Robust fault tolerant control of induction motor system

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    Research into fault tolerant control (FTC, a set of techniques that are developed to increase plant availability and reduce the risk of safety hazards) for induction motors is motivated by practical concerns including the need for enhanced reliability, improved maintenance operations and reduced cost. Its aim is to prevent that simple faults develop into serious failure. Although, the subject of induction motor control is well known, the main topics in the literature are concerned with scalar and vector control and structural stability. However, induction machines experience various fault scenarios and to meet the above requirements FTC strategies based on existing or more advanced control methods become desirable. Some earlier studies on FTC have addressed particular problems of 3-phase sensor current/voltage FTC, torque FTC, etc. However, the development of these methods lacks a more general understanding of the overall problem of FTC for an induction motor based on a true fault classification of possible fault types.In order to develop a more general approach to FTC for induction motors, i.e. not just designing specific control approaches for individual induction motor fault scenarios, this thesis has carried out a systematic research on induction motor systems considering the various faults that can typically be present, having either “additive” fault or “multiplicative” effects on the system dynamics, according to whether the faults are sensor or actuator (additive fault) types or component or motor faults (multiplicative fault) types.To achieve the required objectives, an active approach to FTC is used, making use of fault estimation (FE, an approach that determine the magnitude of a fault signal online) and fault compensation. This approach of FTC/FE considers an integration of the electrical and mechanical dynamics, initially using adaptive and/or sliding mode observers, Linear Parameter Varying (LPV, in which nonlinear systems are locally decomposed into several linear systems scheduled by varying parameters) and then using back-stepping control combined with observer/estimation methods for handling certain forms of nonlinearity.In conclusion, the thesis proposed an integrated research of induction motor FTC/FE with the consideration of different types of faults and different types of uncertainties, and validated the approaches through simulations and experiments

    New Fault Detection, Mitigation and Injection Strategies for Current and Forthcoming Challenges of HW Embedded Designs

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    Tesis por compendio[EN] Relevance of electronics towards safety of common devices has only been growing, as an ever growing stake of the functionality is assigned to them. But of course, this comes along the constant need for higher performances to fulfill such functionality requirements, while keeping power and budget low. In this scenario, industry is struggling to provide a technology which meets all the performance, power and price specifications, at the cost of an increased vulnerability to several types of known faults or the appearance of new ones. To provide a solution for the new and growing faults in the systems, designers have been using traditional techniques from safety-critical applications, which offer in general suboptimal results. In fact, modern embedded architectures offer the possibility of optimizing the dependability properties by enabling the interaction of hardware, firmware and software levels in the process. However, that point is not yet successfully achieved. Advances in every level towards that direction are much needed if flexible, robust, resilient and cost effective fault tolerance is desired. The work presented here focuses on the hardware level, with the background consideration of a potential integration into a holistic approach. The efforts in this thesis have focused several issues: (i) to introduce additional fault models as required for adequate representativity of physical effects blooming in modern manufacturing technologies, (ii) to provide tools and methods to efficiently inject both the proposed models and classical ones, (iii) to analyze the optimum method for assessing the robustness of the systems by using extensive fault injection and later correlation with higher level layers in an effort to cut development time and cost, (iv) to provide new detection methodologies to cope with challenges modeled by proposed fault models, (v) to propose mitigation strategies focused towards tackling such new threat scenarios and (vi) to devise an automated methodology for the deployment of many fault tolerance mechanisms in a systematic robust way. The outcomes of the thesis constitute a suite of tools and methods to help the designer of critical systems in his task to develop robust, validated, and on-time designs tailored to his application.[ES] La relevancia que la electrónica adquiere en la seguridad de los productos ha crecido inexorablemente, puesto que cada vez ésta copa una mayor influencia en la funcionalidad de los mismos. Pero, por supuesto, este hecho viene acompañado de una necesidad constante de mayores prestaciones para cumplir con los requerimientos funcionales, al tiempo que se mantienen los costes y el consumo en unos niveles reducidos. En este escenario, la industria está realizando esfuerzos para proveer una tecnología que cumpla con todas las especificaciones de potencia, consumo y precio, a costa de un incremento en la vulnerabilidad a múltiples tipos de fallos conocidos o la introducción de nuevos. Para ofrecer una solución a los fallos nuevos y crecientes en los sistemas, los diseñadores han recurrido a técnicas tradicionalmente asociadas a sistemas críticos para la seguridad, que ofrecen en general resultados sub-óptimos. De hecho, las arquitecturas empotradas modernas ofrecen la posibilidad de optimizar las propiedades de confiabilidad al habilitar la interacción de los niveles de hardware, firmware y software en el proceso. No obstante, ese punto no está resulto todavía. Se necesitan avances en todos los niveles en la mencionada dirección para poder alcanzar los objetivos de una tolerancia a fallos flexible, robusta, resiliente y a bajo coste. El trabajo presentado aquí se centra en el nivel de hardware, con la consideración de fondo de una potencial integración en una estrategia holística. Los esfuerzos de esta tesis se han centrado en los siguientes aspectos: (i) la introducción de modelos de fallo adicionales requeridos para la representación adecuada de efectos físicos surgentes en las tecnologías de manufactura actuales, (ii) la provisión de herramientas y métodos para la inyección eficiente de los modelos propuestos y de los clásicos, (iii) el análisis del método óptimo para estudiar la robustez de sistemas mediante el uso de inyección de fallos extensiva, y la posterior correlación con capas de más alto nivel en un esfuerzo por recortar el tiempo y coste de desarrollo, (iv) la provisión de nuevos métodos de detección para cubrir los retos planteados por los modelos de fallo propuestos, (v) la propuesta de estrategias de mitigación enfocadas hacia el tratamiento de dichos escenarios de amenaza y (vi) la introducción de una metodología automatizada de despliegue de diversos mecanismos de tolerancia a fallos de forma robusta y sistemática. Los resultados de la presente tesis constituyen un conjunto de herramientas y métodos para ayudar al diseñador de sistemas críticos en su tarea de desarrollo de diseños robustos, validados y en tiempo adaptados a su aplicación.[CA] La rellevància que l'electrònica adquireix en la seguretat dels productes ha crescut inexorablement, puix cada volta més aquesta abasta una major influència en la funcionalitat dels mateixos. Però, per descomptat, aquest fet ve acompanyat d'un constant necessitat de majors prestacions per acomplir els requeriments funcionals, mentre es mantenen els costos i consums en uns nivells reduïts. Donat aquest escenari, la indústria està fent esforços per proveir una tecnologia que complisca amb totes les especificacions de potència, consum i preu, tot a costa d'un increment en la vulnerabilitat a diversos tipus de fallades conegudes, i a la introducció de nous tipus. Per oferir una solució a les noves i creixents fallades als sistemes, els dissenyadors han recorregut a tècniques tradicionalment associades a sistemes crítics per a la seguretat, que en general oferixen resultats sub-òptims. De fet, les arquitectures empotrades modernes oferixen la possibilitat d'optimitzar les propietats de confiabilitat en habilitar la interacció dels nivells de hardware, firmware i software en el procés. Tot i això eixe punt no està resolt encara. Es necessiten avanços a tots els nivells en l'esmentada direcció per poder assolir els objectius d'una tolerància a fallades flexible, robusta, resilient i a baix cost. El treball ací presentat se centra en el nivell de hardware, amb la consideració de fons d'una potencial integració en una estratègia holística. Els esforços d'esta tesi s'han centrat en els següents aspectes: (i) la introducció de models de fallada addicionals requerits per a la representació adequada d'efectes físics que apareixen en les tecnologies de fabricació actuals, (ii) la provisió de ferramentes i mètodes per a la injecció eficient del models proposats i dels clàssics, (iii) l'anàlisi del mètode òptim per estudiar la robustesa de sistemes mitjançant l'ús d'injecció de fallades extensiva, i la posterior correlació amb capes de més alt nivell en un esforç per retallar el temps i cost de desenvolupament, (iv) la provisió de nous mètodes de detecció per cobrir els reptes plantejats pels models de fallades proposats, (v) la proposta d'estratègies de mitigació enfocades cap al tractament dels esmentats escenaris d'amenaça i (vi) la introducció d'una metodologia automatitzada de desplegament de diversos mecanismes de tolerància a fallades de forma robusta i sistemàtica. Els resultats de la present tesi constitueixen un conjunt de ferramentes i mètodes per ajudar el dissenyador de sistemes crítics en la seua tasca de desenvolupament de dissenys robustos, validats i a temps adaptats a la seua aplicació.Espinosa García, J. (2016). New Fault Detection, Mitigation and Injection Strategies for Current and Forthcoming Challenges of HW Embedded Designs [Tesis doctoral no publicada]. Universitat Politècnica de València. https://doi.org/10.4995/Thesis/10251/73146TESISCompendi
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