On-Line Instruction-checking in Pipelined Microprocessors

Microprocessors performances have increased by more than five orders of magnitude in the last three decades. As technology scales down, these components become inherently unreliable posing major design and test challenges. This paper proposes an instruction-checking architecture to detect erroneous instruction executions caused by both permanent and transient errors in the internal logic of a microprocessor. Monitoring the correct activation sequence of a set of predefined microprocessor control/status signals allow distinguishing between correctly and not correctly executed instruction

Cross-layer system reliability assessment framework for hardware faults

System reliability estimation during early design phases facilitates informed decisions for the integration of effective protection mechanisms against different classes of hardware faults. When not all system abstraction layers (technology, circuit, microarchitecture, software) are factored in such an estimation model, the delivered reliability reports must be excessively pessimistic and thus lead to unacceptably expensive, over-designed systems. We propose a scalable, cross-layer methodology and supporting suite of tools for accurate but fast estimations of computing systems reliability. The backbone of the methodology is a component-based Bayesian model, which effectively calculates system reliability based on the masking probabilities of individual hardware and software components considering their complex interactions. Our detailed experimental evaluation for different technologies, microarchitectures, and benchmarks demonstrates that the proposed model delivers very accurate reliability estimations (FIT rates) compared to statistically significant but slow fault injection campaigns at the microarchitecture level.Peer ReviewedPostprint (author's final draft

Statistical Reliability Estimation of Microprocessor-Based Systems

What is the probability that the execution state of a given microprocessor running a given application is correct, in a certain working environment with a given soft-error rate? Trying to answer this question using fault injection can be very expensive and time consuming. This paper proposes the baseline for a new methodology, based on microprocessor error probability profiling, that aims at estimating fault injection results without the need of a typical fault injection setup. The proposed methodology is based on two main ideas: a one-time fault-injection analysis of the microprocessor architecture to characterize the probability of successful execution of each of its instructions in presence of a soft-error, and a static and very fast analysis of the control and data flow of the target software application to compute its probability of success. The presented work goes beyond the dependability evaluation problem; it also has the potential to become the backbone for new tools able to help engineers to choose the best hardware and software architecture to structurally maximize the probability of a correct execution of the target softwar

Cross-layer reliability evaluation, moving from the hardware architecture to the system level: A CLERECO EU project overview

Advanced computing systems realized in forthcoming technologies hold the promise of a significant increase of computational capabilities. However, the same path that is leading technologies toward these remarkable achievements is also making electronic devices increasingly unreliable. Developing new methods to evaluate the reliability of these systems in an early design stage has the potential to save costs, produce optimized designs and have a positive impact on the product time-to-market. CLERECO European FP7 research project addresses early reliability evaluation with a cross-layer approach across different computing disciplines, across computing system layers and across computing market segments. The fundamental objective of the project is to investigate in depth a methodology to assess system reliability early in the design cycle of the future systems of the emerging computing continuum. This paper presents a general overview of the CLERECO project focusing on the main tools and models that are being developed that could be of interest for the research community and engineering practice

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

FIMSIM: A fault injection infrastructure for microarchitectural simulators

Fault injection is a widely used approach for experiment-based dependability evaluation in which faults can be injected to the hardware, to the simulator or to the software. Simulation based fault injection is more appealing for researchers, since it can be utilized at the early design stage of the processor. As such, it enables a preliminary analysis of the correlation between the criticality of circuit level faults and their impact on applications. However, the lack of publicly available fault injectors for microarchitecture level simulators brings extra burden of designing and implementing fault injectors to the researchers who evaluate microarchitecture dependability. In this study, we present FIMSIM, to the best of our knowledge, the first publicly available fault injection simulator at the microarchitecture level. FIMSIM is a compact tool which is capable of injecting transient, permanent, intermittent and multi-bit faults. Therefore, FIMSIM provides the opportunity to comprehensively evaluate the vulnerability of different microarchitectural structures against different fault models.Postprint (published version

Exceeding Conservative Limits: A Consolidated Analysis on Modern Hardware Margins

Modern large-scale computing systems (data centers, supercomputers, cloud and edge setups and high-end cyber-physical systems) employ heterogeneous architectures that consist of multicore CPUs, general-purpose many-core GPUs, and programmable FPGAs. The effective utilization of these architectures poses several challenges, among which a primary one is power consumption. Voltage reduction is one of the most efficient methods to reduce power consumption of a chip. With the galloping adoption of hardware accelerators (i.e., GPUs and FPGAs) in large datacenters and other large-scale computing infrastructures, a comprehensive evaluation of the safe voltage reduction levels for each different chip can be employed for efficient reduction of the total power. We present a survey of recent studies in voltage margins reduction at the system level for modern CPUs, GPUs and FPGAs. The pessimistic voltage guardbands inserted by the silicon vendors can be exploited in all devices for significant power savings. On average, voltage reduction can reach 12% in multicore CPUs, 20% in manycore GPUs and 39% in FPGAs.Comment: Accepted for publication in IEEE Transactions on Device and Materials Reliabilit