Toward Fault-Tolerant Applications on Reconfigurable Systems-on-Chip

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Cross layer reliability estimation for digital systems

Forthcoming manufacturing technologies hold the promise to increase multifuctional computing systems performance and functionality thanks to a remarkable growth of the device integration density. Despite the benefits introduced by this technology improvements, reliability is becoming a key challenge for the semiconductor industry. With transistor size reaching the atomic dimensions, vulnerability to unavoidable fluctuations in the manufacturing process and environmental stress rise dramatically. Failing to meet a reliability requirement may add excessive re-design cost to recover and may have severe consequences on the success of a product. %Worst-case design with large margins to guarantee reliable operation has been employed for long time. However, it is reaching a limit that makes it economically unsustainable due to its performance, area, and power cost. One of the open challenges for future technologies is building ``dependable'' systems on top of unreliable components, which will degrade and even fail during normal lifetime of the chip. Conventional design techniques are highly inefficient. They expend significant amount of energy to tolerate the device unpredictability by adding safety margins to a circuit's operating voltage, clock frequency or charge stored per bit. Unfortunately, the additional cost introduced to compensate unreliability are rapidly becoming unacceptable in today's environment where power consumption is often the limiting factor for integrated circuit performance, and energy efficiency is a top concern. Attention should be payed to tailor techniques to improve the reliability of a system on the basis of its requirements, ending up with cost-effective solutions favoring the success of the product on the market. Cross-layer reliability is one of the most promising approaches to achieve this goal. Cross-layer reliability techniques take into account the interactions between the layers composing a complex system (i.e., technology, hardware and software layers) to implement efficient cross-layer fault mitigation mechanisms. Fault tolerance mechanism are carefully implemented at different layers starting from the technology up to the software layer to carefully optimize the system by exploiting the inner capability of each layer to mask lower level faults. For this purpose, cross-layer reliability design techniques need to be complemented with cross-layer reliability evaluation tools, able to precisely assess the reliability level of a selected design early in the design cycle. Accurate and early reliability estimates would enable the exploration of the system design space and the optimization of multiple constraints such as performance, power consumption, cost and reliability. This Ph.D. thesis is devoted to the development of new methodologies and tools to evaluate and optimize the reliability of complex digital systems during the early design stages. More specifically, techniques addressing hardware accelerators (i.e., FPGAs and GPUs), microprocessors and full systems are discussed. All developed methodologies are presented in conjunction with their application to real-world use cases belonging to different computational domains

Error Detection and Diagnosis for System-on-Chip in Space Applications

Tesis por compendio de publicacionesLos componentes electrónicos comerciales, comúnmente llamados componentes Commercial-Off-The-Shelf (COTS) están presentes en multitud de dispositivos habituales en nuestro día a día. Particularmente, el uso de microprocesadores y sistemas en chip (SoC) altamente integrados ha favorecido la aparición de dispositivos electrónicos cada vez más inteligentes que sostienen el estilo de vida y el avance de la sociedad moderna. Su uso se ha generalizado incluso en aquellos sistemas que se consideran críticos para la seguridad, como vehículos, aviones, armamento, dispositivos médicos, implantes o centrales eléctricas. En cualquiera de ellos, un fallo podría tener graves consecuencias humanas o económicas. Sin embargo, todos los sistemas electrónicos conviven constantemente con factores internos y externos que pueden provocar fallos en su funcionamiento. La capacidad de un sistema para funcionar correctamente en presencia de fallos se denomina tolerancia a fallos, y es un requisito en el diseño y operación de sistemas críticos. Los vehículos espaciales como satélites o naves espaciales también hacen uso de microprocesadores para operar de forma autónoma o semi autónoma durante su vida útil, con la dificultad añadida de que no pueden ser reparados en órbita, por lo que se consideran sistemas críticos. Además, las duras condiciones existentes en el espacio, y en particular los efectos de la radiación, suponen un gran desafío para el correcto funcionamiento de los dispositivos electrónicos. Concretamente, los fallos transitorios provocados por radiación (conocidos como soft errors) tienen el potencial de ser una de las mayores amenazas para la fiabilidad de un sistema en el espacio. Las misiones espaciales de gran envergadura, típicamente financiadas públicamente como en el caso de la NASA o la Agencia Espacial Europea (ESA), han tenido históricamente como requisito evitar el riesgo a toda costa por encima de cualquier restricción de coste o plazo. Por ello, la selección de componentes resistentes a la radiación (rad-hard) específicamente diseñados para su uso en el espacio ha sido la metodología imperante en el paradigma que hoy podemos denominar industria espacial tradicional, u Old Space. Sin embargo, los componentes rad-hard tienen habitualmente un coste mucho más alto y unas prestaciones mucho menores que otros componentes COTS equivalentes. De hecho, los componentes COTS ya han sido utilizados satisfactoriamente en misiones de la NASA o la ESA cuando las prestaciones requeridas por la misión no podían ser cubiertas por ningún componente rad-hard existente. En los últimos años, el acceso al espacio se está facilitando debido en gran parte a la entrada de empresas privadas en la industria espacial. Estas empresas no siempre buscan evitar el riesgo a toda costa, sino que deben perseguir una rentabilidad económica, por lo que hacen un balance entre riesgo, coste y plazo mediante gestión del riesgo en un paradigma denominado Nuevo Espacio o New Space. Estas empresas a menudo están interesadas en entregar servicios basados en el espacio con las máximas prestaciones y el mayor beneficio posibles, para lo cual los componentes rad-hard son menos atractivos debido a su mayor coste y menores prestaciones que los componentes COTS existentes. Sin embargo, los componentes COTS no han sido específicamente diseñados para su uso en el espacio y típicamente no incluyen técnicas específicas para evitar que los efectos de la radiación afecten su funcionamiento. Los componentes COTS se comercializan tal cual son, y habitualmente no es posible modificarlos para mejorar su resistencia a la radiación. Además, los elevados niveles de integración de los sistemas en chip (SoC) complejos de altas prestaciones dificultan su observación y la aplicación de técnicas de tolerancia a fallos. Este problema es especialmente relevante en el caso de los microprocesadores. Por tanto, existe un gran interés en el desarrollo de técnicas que permitan conocer y mejorar el comportamiento de los microprocesadores COTS bajo radiación sin modificar su arquitectura y sin interferir en su funcionamiento para facilitar su uso en el espacio y con ello maximizar las prestaciones de las misiones espaciales presentes y futuras. En esta Tesis se han desarrollado técnicas novedosas para detectar, diagnosticar y mitigar los errores producidos por radiación en microprocesadores y sistemas en chip (SoC) comerciales, utilizando la interfaz de traza como punto de observación. La interfaz de traza es un recurso habitual en los microprocesadores modernos, principalmente enfocado a soportar las tareas de desarrollo y depuración del software durante la fase de diseño. Sin embargo, una vez el desarrollo ha concluido, la interfaz de traza típicamente no se utiliza durante la fase operativa del sistema, por lo que puede ser reutilizada sin coste. La interfaz de traza constituye un punto de conexión viable para observar el comportamiento de un microprocesador de forma no intrusiva y sin interferir en su funcionamiento. Como resultado de esta Tesis se ha desarrollado un módulo IP capaz de recabar y decodificar la información de traza de un microprocesador COTS moderno de altas prestaciones. El IP es altamente configurable y personalizable para adaptarse a diferentes aplicaciones y tipos de procesadores. Ha sido diseñado y validado utilizando el dispositivo Zynq-7000 de Xilinx como plataforma de desarrollo, que constituye un dispositivo COTS de interés en la industria espacial. Este dispositivo incluye un procesador ARM Cortex-A9 de doble núcleo, que es representativo del conjunto de microprocesadores hard-core modernos de altas prestaciones. El IP resultante es compatible con la tecnología ARM CoreSight, que proporciona acceso a información de traza en los microprocesadores ARM. El IP incorpora técnicas para detectar errores en el flujo de ejecución y en los datos de la aplicación ejecutada utilizando la información de traza, en tiempo real y con muy baja latencia. El IP se ha validado en campañas de inyección de fallos y también en radiación con protones y neutrones en instalaciones especializadas. También se ha combinado con otras técnicas de tolerancia a fallos para construir técnicas híbridas de mitigación de errores. Los resultados experimentales obtenidos demuestran su alta capacidad de detección y potencialidad en el diagnóstico de errores producidos por radiación. El resultado de esta Tesis, desarrollada en el marco de un Doctorado Industrial entre la Universidad Carlos III de Madrid (UC3M) y la empresa Arquimea, se ha transferido satisfactoriamente al entorno empresarial en forma de un proyecto financiado por la Agencia Espacial Europea para continuar su desarrollo y posterior explotación.Commercial electronic components, also known as Commercial-Off-The-Shelf (COTS), are present in a wide variety of devices commonly used in our daily life. Particularly, the use of microprocessors and highly integrated System-on-Chip (SoC) devices has fostered the advent of increasingly intelligent electronic devices which sustain the lifestyles and the progress of modern society. Microprocessors are present even in safety-critical systems, such as vehicles, planes, weapons, medical devices, implants, or power plants. In any of these cases, a fault could involve severe human or economic consequences. However, every electronic system deals continuously with internal and external factors that could provoke faults in its operation. The capacity of a system to operate correctly in presence of faults is known as fault-tolerance, and it becomes a requirement in the design and operation of critical systems. Space vehicles such as satellites or spacecraft also incorporate microprocessors to operate autonomously or semi-autonomously during their service life, with the additional difficulty that they cannot be repaired once in-orbit, so they are considered critical systems. In addition, the harsh conditions in space, and specifically radiation effects, involve a big challenge for the correct operation of electronic devices. In particular, radiation-induced soft errors have the potential to become one of the major risks for the reliability of systems in space. Large space missions, typically publicly funded as in the case of NASA or European Space Agency (ESA), have followed historically the requirement to avoid the risk at any expense, regardless of any cost or schedule restriction. Because of that, the selection of radiation-resistant components (known as rad-hard) specifically designed to be used in space has been the dominant methodology in the paradigm of traditional space industry, also known as “Old Space”. However, rad-hard components have commonly a much higher associated cost and much lower performance that other equivalent COTS devices. In fact, COTS components have already been used successfully by NASA and ESA in missions that requested such high performance that could not be satisfied by any available rad-hard component. In the recent years, the access to space is being facilitated in part due to the irruption of private companies in the space industry. Such companies do not always seek to avoid the risk at any cost, but they must pursue profitability, so they perform a trade-off between risk, cost, and schedule through risk management in a paradigm known as “New Space”. Private companies are often interested in deliver space-based services with the maximum performance and maximum benefit as possible. With such objective, rad-hard components are less attractive than COTS due to their higher cost and lower performance. However, COTS components have not been specifically designed to be used in space and typically they do not include specific techniques to avoid or mitigate the radiation effects in their operation. COTS components are commercialized “as is”, so it is not possible to modify them to improve their susceptibility to radiation effects. Moreover, the high levels of integration of complex, high-performance SoC devices hinder their observability and the application of fault-tolerance techniques. This problem is especially relevant in the case of microprocessors. Thus, there is a growing interest in the development of techniques allowing to understand and improve the behavior of COTS microprocessors under radiation without modifying their architecture and without interfering with their operation. Such techniques may facilitate the use of COTS components in space and maximize the performance of present and future space missions. In this Thesis, novel techniques have been developed to detect, diagnose, and mitigate radiation-induced errors in COTS microprocessors and SoCs using the trace interface as an observation point. The trace interface is a resource commonly found in modern microprocessors, mainly intended to support software development and debugging activities during the design phase. However, it is commonly left unused during the operational phase of the system, so it can be reused with no cost. The trace interface constitutes a feasible connection point to observe microprocessor behavior in a non-intrusive manner and without disturbing processor operation. As a result of this Thesis, an IP module has been developed capable to gather and decode the trace information of a modern, high-end, COTS microprocessor. The IP is highly configurable and customizable to support different applications and processor types. The IP has been designed and validated using the Xilinx Zynq-7000 device as a development platform, which is an interesting COTS device for the space industry. This device features a dual-core ARM Cortex-A9 processor, which is a good representative of modern, high-end, hard-core microprocessors. The resulting IP is compatible with the ARM CoreSight technology, which enables access to trace information in ARM microprocessors. The IP is able to detect errors in the execution flow of the microprocessor and in the application data using trace information, in real time and with very low latency. The IP has been validated in fault injection campaigns and also under proton and neutron irradiation campaigns in specialized facilities. It has also been combined with other fault-tolerance techniques to build hybrid error mitigation approaches. Experimental results demonstrate its high detection capabilities and high potential for the diagnosis of radiation-induced errors. The result of this Thesis, developed in the framework of an Industrial Ph.D. between the University Carlos III of Madrid (UC3M) and the company Arquimea, has been successfully transferred to the company business as a project sponsored by European Space Agency to continue its development and subsequent commercialization.Programa de Doctorado en Ingeniería Eléctrica, Electrónica y Automática por la Universidad Carlos III de MadridPresidenta: María Luisa López Vallejo.- Secretario: Enrique San Millán Heredia.- Vocal: Luigi Di Lill

Developing a multi-level fault injection environment

textDependability and fault tolerance are important aspects of modern computer systems. Particle strikes or electromagnetic interference can cause internal state of the system to change, which might cause errors to the system with non-negligible probability. Such errors are termed "soft errors". Bit flips in the design are good way to model these soft-errors. These bit-flips due to soft errors are random and transient in a design, making their analysis more difficult than simple stuck-at faults. Interestingly only a few of the flops which are affected by radiation cause soft errors, due to different propagation paths and functional impact of the flops. In order to improve the dependability of a system with reasonable overhead, the flops in a design which are most vulnerable to soft errors need to be protected. Each application case can potentially expose a slightly different set of flip-flops as vulnerable. Hence different tools are required to confidently analyse soft errors for evaluating the fault tolerance. As part of the thesis, I have developed a suite of tools for analyzing soft errors. The multi-level tools are necessary for complete fault tolerance analysis and identifying the most vulnerable flip-flops in a specific processor. The first part of the thesis describes the FPGA development framework for a specific processor. Simulation based fault injection techniques are described in the later sections. The final parts cover analysis techniques and applications that can benefit from such systems.Electrical and Computer Engineerin

Optimizing Scrubbing by Netlist Analysis for FPGA Configuration Bit Classification and Floorplanning

Existing scrubbing techniques for SEU mitigation on FPGAs do not guarantee an error-free operation after SEU recovering if the affected configuration bits do belong to feedback loops of the implemented circuits. In this paper, we a) provide a netlist-based circuit analysis technique to distinguish so-called critical configuration bits from essential bits in order to identify configuration bits which will need also state-restoring actions after a recovered SEU and which not. Furthermore, b) an alternative classification approach using fault injection is developed in order to compare both classification techniques. Moreover, c) we will propose a floorplanning approach for reducing the effective number of scrubbed frames and d), experimental results will give evidence that our optimization methodology not only allows to detect errors earlier but also to minimize the Mean-Time-To-Repair (MTTR) of a circuit considerably. In particular, we show that by using our approach, the MTTR for datapath-intensive circuits can be reduced by up to 48.5% in comparison to standard approaches

New Design Techniques for Dynamic Reconfigurable Architectures

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INVESTIGATING THE EFFECTS OF SINGLE-EVENT UPSETS IN STATIC AND DYNAMIC REGISTERS

Radiation-induced single-event upsets (SEUs) pose a serious threat to the reliability of registers. The existing SEU analyses for static CMOS registers focus on the circuit-level impact and may underestimate the pertinent SEU information provided through node analysis. This thesis proposes SEU node analysis to evaluate the sensitivity of static registers and apply the obtained node information to improve the robustness of the register through selective node hardening (SNH) technique. Unlike previous hardening techniques such as the Triple Modular Redundancy (TMR) and the Dual Interlocked Cell (DICE) latch, the SNH method does not introduce larger area overhead. Moreover, this thesis also explores the impact of SEUs in dynamic flip-flops, which are appealing for the design of high-performance microprocessors. Previous work either uses the approaches for static flip-flops to evaluate SEU effects in dynamic flip-flops or overlook the SEU injected during the precharge phase. In this thesis, possible SEU sensitive nodes in dynamic flip-flops are re-examined and their window of vulnerability (WOV) is extended. Simulation results for SEU analysis in non-hardened dynamic flip-flops reveal that the last 55.3 % of the precharge time and a 100% evaluation time are affected by SEUs