Standart-konformes Snapshotting für SystemC Virtuelle Plattformen

The steady increase in complexity of high-end embedded systems goes along with an increasingly complex design process. We are currently still in a transition phase from Hardware-Description Language (HDL) based design towards virtual-platform-based design of embedded systems. As design complexity rises faster than developer productivity a gap forms. Restoring productivity while at the same time managing increased design complexity can also be achieved through focussing on the development of new tools and design methodologies. In most application areas, high-level modelling languages such as SystemC are used in early design phases. In modern software development Continuous Integration (CI) is used to automatically test if a submitted piece of code breaks functionality. Application of the CI concept to embedded system design and testing requires fast build and test execution times from the virtual platform framework. For this use case the ability to save a specific state of a virtual platform becomes necessary. The saving and restoring of specific states of a simulation requires the ability to serialize all data structures within the simulation models. Improving the frameworks and establishing better methods will only help to narrow the design gap, if these changes are introduced with the needs of the engineers and developers in mind. Ultimately, it is their productivity that shall be improved. The ability to save the state of a virtual platform enables developers to run longer test campaigns that can even contain randomized test stimuli. If the saved states are modifiable the developers can inject faulty states into the simulation models. This work contributes an extension to the SoCRocket virtual platform framework to enable snapshotting. The snapshotting extension can be considered a reference implementation as the utilization of current SystemC/TLM standards makes it compatible to other frameworkds. Furthermore, integrating the UVM SystemC library into the framework enables test driven development and fast validation of SystemC/TLM models using snapshots. These extensions narrow the design gap by supporting designers, testers and developers to work more efficiently.Die stetige Steigerung der Komplexität eingebetteter Systeme geht einher mit einer ebenso steigenden Komplexität des Entwurfsprozesses. Wir befinden uns momentan in der Übergangsphase vom Entwurf von eingebetteten Systemen basierend auf Hardware-Beschreibungssprachen hin zum Entwurf ebendieser basierend auf virtuellen Plattformen. Da die Entwurfskomplexität rasanter steigt als die Produktivität der Entwickler, entsteht eine Kluft. Die Produktivität wiederherzustellen und gleichzeitig die gesteigerte Entwurfskomplexität zu bewältigen, kann auch erreicht werden, indem der Fokus auf die Entwicklung neuer Werkzeuge und Entwurfsmethoden gelegt wird. In den meisten Anwendungsgebieten werden Modellierungssprachen auf hoher Ebene, wie zum Beispiel SystemC, in den frühen Entwurfsphasen benutzt. In der modernen Software-Entwicklung wird Continuous Integration (CI) benutzt um automatisiert zu überprüfen, ob eine eingespielte Änderung am Quelltext bestehende Funktionalitäten beeinträchtigt. Die Anwendung des CI-Konzepts auf den Entwurf und das Testen von eingebetteten Systemen fordert schnelle Bau- und Test-Ausführungszeiten von dem genutzten Framework für virtuelle Plattformen. Für diesen Anwendungsfall wird auch die Fähigkeit, einen bestimmten Zustand der virtuellen Plattform zu speichern, erforderlich. Das Speichern und Wiederherstellen der Zustände einer Simulation erfordert die Serialisierung aller Datenstrukturen, die sich in den Simulationsmodellen befinden. Das Verbessern von Frameworks und Etablieren besserer Methodiken hilft nur die Entwurfs-Kluft zu verringern, wenn diese Änderungen mit Berücksichtigung der Bedürfnisse der Entwickler und Ingenieure eingeführt werden. Letztendlich ist es ihre Produktivität, die gesteigert werden soll. Die Fähigkeit den Zustand einer virtuellen Plattform zu speichern, ermöglicht es den Entwicklern, längere Testkampagnen laufen zu lassen, die auch zufällig erzeugte Teststimuli beinhalten können oder, falls die gespeicherten Zustände modifizierbar sind, fehlerbehaftete Zustände in die Simulationsmodelle zu injizieren. Mein mit dieser Arbeit geleisteter Beitrag beinhaltet die Erweiterung des SoCRocket Frameworks um Checkpointing Funktionalität im Sinne einer Referenzimplementierung. Weiterhin ermöglicht die Integration der UVM SystemC Bibliothek in das Framework die Umsetzung der testgetriebenen Entwicklung und schnelle Validierung von SystemC/TLM Modellen mit Hilfe von Snapshots

Understanding Soft Errors in Uncore Components

The effects of soft errors in processor cores have been widely studied. However, little has been published about soft errors in uncore components, such as memory subsystem and I/O controllers, of a System-on-a-Chip (SoC). In this work, we study how soft errors in uncore components affect system-level behaviors. We have created a new mixed-mode simulation platform that combines simulators at two different levels of abstraction, and achieves 20,000x speedup over RTL-only simulation. Using this platform, we present the first study of the system-level impact of soft errors inside various uncore components of a large-scale, multi-core SoC using the industrial-grade, open-source OpenSPARC T2 SoC design. Our results show that soft errors in uncore components can significantly impact system-level reliability. We also demonstrate that uncore soft errors can create major challenges for traditional system-level checkpoint recovery techniques. To overcome such recovery challenges, we present a new replay recovery technique for uncore components belonging to the memory subsystem. For the L2 cache controller and the DRAM controller components of OpenSPARC T2, our new technique reduces the probability that an application run fails to produce correct results due to soft errors by more than 100x with 3.32% and 6.09% chip-level area and power impact, respectively.Comment: to be published in Proceedings of the 52nd Annual Design Automation Conferenc

Auditable Restoration of Distributed Programs

We focus on a protocol for auditable restoration of distributed systems. The need for such protocol arises due to conflicting requirements (e.g., access to the system should be restricted but emergency access should be provided). One can design such systems with a tamper detection approach (based on the intuition of "break the glass door"). However, in a distributed system, such tampering, which are denoted as auditable events, is visible only for a single node. This is unacceptable since the actions they take in these situations can be different than those in the normal mode. Moreover, eventually, the auditable event needs to be cleared so that system resumes the normal operation. With this motivation, in this paper, we present a protocol for auditable restoration, where any process can potentially identify an auditable event. Whenever a new auditable event occurs, the system must reach an "auditable state" where every process is aware of the auditable event. Only after the system reaches an auditable state, it can begin the operation of restoration. Although any process can observe an auditable event, we require that only "authorized" processes can begin the task of restoration. Moreover, these processes can begin the restoration only when the system is in an auditable state. Our protocol is self-stabilizing and has bounded state space. It can effectively handle the case where faults or auditable events occur during the restoration protocol. Moreover, it can be used to provide auditable restoration to other distributed protocol.Comment: 10 page

MPU-based incremental checkpointing for transiently-powered systems

International audienc

Configuration Interoperability of Hardware-Software-Models in SystemC

Im modernen Electronic System Level-Design wird zur Bewältigung der ständig steigenden Entwurfskomplexität auf hoher Abstraktion entwickelt. Unterstützung bieten dabei Systembeschreibungssprachen wie SystemC zusammen mit meist kommerziellen Entwicklungsumgebungen. Für eine hohe Entwurfseffizienz etwa bei der Architektur-Exploration sollten die Modelle untereinander über Herstellergrenzen und über Entwicklungsumgebungen hinweg problemlos austauschbar sein. Dafür sind Interoperabilitäts-Standards notwendig wie sie für SystemC bereits auf funktionaler Ebene existieren (TLM-2.0). Über diese den realen Teil der Modelle betreffende Interoperabilität hinaus ist die Austauschbarkeit von Modellen zwischen Entwicklungsumgebungen bisher nicht standardisiert. Die vorliegende Arbeit definiert hierfür eine Meta-Interoperabilität und beschäftigt sich intensiv mit der dort einzugliedernden Interoperabilität der Konfiguration von Modellen. Es wird ein flexibler Konfigurationsmechanismus präsentiert, der existierende Mechanismen miteinander kompatibel macht und der in den von der Open SystemC Initiative (OSCI) erarbeiteten Konfigurations-Standard einfließt. Der Konfigurationsmechanismus basiert auf einer Modell-Middleware, die auch für weitere Ziele der Meta-Interoperabilität verwendet werden kann.In today's Electronic System Level Design, rapid platform development is done on a high abstraction level. Hence the system description language SystemC is getting used more and more often. For easy and fast architectural exploration, the designers must be able to integrate (high-level) models from different IP or model vendors as well as customized models into one platform. These models need to be interoperable with low effort. Therefore we need interoperability standards, like TLM-2.0 for SystemC which defines a communication standard for functional interoperablilty. Another interoperability layer is the tool layer, which has not yet been addressed by a standard. This work defines meta interoperability and deales especially with the configuration interoperability as one part of meta interoperability. For model configuration a flexible interoperability framework is presented, which is able to connect different configuration mechanisms to each other. Additionally this work had been contributed to the upcoming configuration standard developed by Open SystemC Initiative (OSCI). Furthermore the configuration framework is based on a middleware which is applicable as a base for additional services for meta interoperability

Reproducible Host Networking Evaluation with End-to-End Simulation

Networking researchers are facing growing challenges in evaluating and reproducing results for modern network systems. As systems rely on closer integration of system components and cross-layer optimizations in the pursuit of performance and efficiency, they are also increasingly tied to specific hardware and testbed properties. Combined with a trend towards heterogeneous hardware, such as protocol offloads, SmartNICs, and in-network accelerators, researchers face the choice of either investing more and more time and resources into comparisons to prior work or, alternatively, lower the standards for evaluation. We aim to address this challenge by introducing SimBricks, a simulation framework that decouples networked systems from the physical testbed and enables reproducible end-to-end evaluation in simulation. Instead of reinventing the wheel, SimBricks is a modular framework for combining existing tried-and-true simulators for individual components, processor and memory, NIC, and network, into complete testbeds capable of running unmodified systems. In our evaluation, we reproduce key findings from prior work, including dctcp congestion control, NOPaxos in-network consensus acceleration, and the Corundum FPGA NIC.Comment: 15 pages, 10 figures, under submissio

Fault Tolerant Nanosatellite Computing on a Budget

In this contribution, we present a CubeSat-compatible on-board computer (OBC) architecture that offers strong fault tolerance to enable the use of such spacecraft in critical and long-term missions. We describe in detail the design of our OBC’s breadboard setup, and document its composition from the component-level, all the way down to the software level. Fault tolerance in this OBC is achieved without resorting to radiation hardening, just intelligent through software. The OBC ages graceful, and makes use of FPGA-reconfiguration and mixed criticality. It can dynamically adapt to changing performance requirements throughout a space mission. We developed a proof-of-concept with several Xilinx Ultrascale and Ultrascale+ FPGAs. With the smallest Kintex Ultrascale+ KU3P device, we achieve 1.94W total power consumption at 300Mhz, well within the power budget range of current 2U CubeSats. To our knowledge, this is the first scalable and COTS-based, widely reproducible OBC solution which can offer strong fault coverage even for small CubeSats. To reproduce this OBC architecture, no custom-written, proprietary, or protected IP is needed, and the needed design tools are available free-of-charge to academics. All COTS components required to construct this architecture can be purchased on the open market, and are affordable even for academic and scientific CubeSat developers

Robust and reliable hardware accelerator design through high-level synthesis

System-on-chip design is becoming increasingly complex as technology scaling enables more and more functionality on a chip. This scaling-driven complexity has resulted in a variety of reliability and validation challenges including logic bugs, hot spots, wear-out, and soft errors. To make matters worse, as we reach the limits of Dennard scaling, efforts to improve system performance and energy efficiency have resulted in the integration of a wide variety of complex hardware accelerators in SoCs. Thus the challenge is to design complex, custom hardware that is efficient, but also correct and reliable. High-level synthesis shows promise to address the problem of complex hardware design by providing a bridge from the high-productivity software domain to the hardware design process. Much research has been done on high-level synthesis efficiency optimizations. This dissertation shows that high-level synthesis also has the power to address validation and reliability challenges through three automated solutions targeting three key stages in the hardware design and use cycle: pre-silicon debugging, post-silicon validation, and post-deployment error detection. Our solution for rapid pre-silicon debugging of accelerator designs is hybrid tracing: comparing a datapath-level trace of hardware execution with a reference software implementation at a fine temporal and spatial granularity to detect logic bugs. An integrated backtrace process delivers source-code meaning to the hardware designer, pinpointing the location of bug activation and providing a strong hint for potential bug fixes. Experimental results show that we are able to detect and aid in localization of logic bugs from both C/C++ specifications as well as the high-level synthesis engine itself. A variation of this solution tailored for rapid post-silicon validation of accelerator designs is hybrid hashing: inserting signature generation logic in a hardware design to create a heavily compressed signature stream that captures the internal behavior of the design at a fine temporal and spatial granularity for comparison with a reference set of signatures generated by high-level simulation to detect bugs. Using hybrid hashing, we demonstrate an improvement in error detection latency (time elapsed from when a bug is activated to when it manifests as an observable failure) of two orders of magnitude and a threefold improvement in bug coverage compared to traditional post-silicon validation techniques. Hybrid hashing also uncovered previously unknown bugs in the CHStone benchmark suite, which is widely used by the HLS community. Hybrid hashing incurs less than 10% area overhead for the accelerator it validates with negligible performance impact, and we also introduce techniques to minimize any possible intrusiveness introduced by hybrid hashing. Finally, our solution for post-deployment error detection is modulo-3 shadow datapaths: performing lightweight shadow computations in modulo-3 space for each main computation. We leverage the binding and scheduling flexibility of high-level synthesis to detect control errors through diverse binding and minimize area cost through intelligent checkpoint scheduling and modulo-3 reducer sharing. We introduce logic and dataflow optimizations to further reduce cost. We evaluated our technique with 12 high-level synthesis benchmarks from the arithmetic-oriented PolyBench benchmark suite using FPGA emulated netlist-level error injection. We observe coverages of 99.1% for stuck-at faults, 99.5% for soft errors, and 99.6% for timing errors with a 25.7% area cost and negligible performance impact. Leveraging a mean error detection latency of 12.75 cycles (4150× faster than end result check) for soft errors, we also explore a rollback recovery method with an additional area cost of 28.0%, observing a 175× increase in reliability against soft errors. While the area cost of our modulo shadow datapaths is much better than traditional modular redundancy approaches, we want to maximize the applicability of our approach. To this end, we take a dive into gate-level architectural design for modulo arithmetic functional units. We introduce new low-cost gate-level architectures for all four key functional units in a shadow datapath: (1) a modulo reduction algorithm that generates architectures consisting entirely of full-adder standard cells; (2) minimum-area modulo adder and subtractor architectures; (3) an array-based modulo multiplier design; and (4) a modulo equality comparator that handles the residue encoding produced by the above. We compare our new functional units to the previous state-of-the-art approach, observing a 12.5% reduction in area and a 47.1% reduction in delay for a 32-bit mod-3 reducer; that our reducer costs, which tend to dominate shadow datapath costs, do not increase with larger modulo bases; and that for modulo-15 and above, all of our modulo functional units have better area and delay then their previous counterparts. We also demonstrate the practicality of our approach by designing a custom shadow datapath for error detection of a multiply accumulate functional unit, which has an area overhead of only 12% for a 32-bit main datapath and 2-bit modulo-3 shadow datapath. Taking our reliability solution further, we look at the bigger picture of modulo shadow datapaths combined with other solutions at different abstraction layers, looking to answer the following question: Given all of the existing reliability improvement techniques for application-specific hardware accelerators, what techniques or combinations of techniques are the most cost-effective? To answer this question, we consider a soft error fault model and empirically evaluate cross-layer combinations of ABFT, EDDI, and modulo shadow datapaths in the context of high-level synthesis; parity in logic synthesis; and flip-flop hardening techniques at the physical design level. We measure the reliability benefit and area, energy, and performance cost of each technique individually and for interesting technique combinations through FPGA emulated fault-injection and physical place-and-route. Our results show that a combination of parity and flip-flop hardening is the most cost-effective in general with an average 1.3% area cost and 5.7% energy cost for a 50× improvement in reliability. The addition of modulo-3 shadow datapaths to this combination provides some additional benefit for some applications, even without considering its combinational logic, stuck-at fault, and timing error protection benefits. We also observe new efficiency challenges for ABFT and EDDI when used for hardware accelerators

Fault-tolerant satellite computing with modern semiconductors

Miniaturized satellites enable a variety space missions which were in the past infeasible, impractical or uneconomical with traditionally-designed heavier spacecraft. Especially CubeSats can be launched and manufactured rapidly at low cost from commercial components, even in academic environments. However, due to their low reliability and brief lifetime, they are usually not considered suitable for life- and safety-critical services, complex multi-phased solar-system-exploration missions, and missions with a longer duration. Commercial electronics are key to satellite miniaturization, but also responsible for their low reliability: Until 2019, there existed no reliable or fault-tolerant computer architectures suitable for very small satellites. To overcome this deficit, a novel on-board-computer architecture is described in this thesis.Robustness is assured without resorting to radiation hardening, but through software measures implemented within a robust-by-design multiprocessor-system-on-chip. This fault-tolerant architecture is component-wise simple and can dynamically adapt to changing performance requirements throughout a mission. It can support graceful aging by exploiting FPGA-reconfiguration and mixed-criticality.  Experimentally, we achieve 1.94W power consumption at 300Mhz with a Xilinx Kintex Ultrascale+ proof-of-concept, which is well within the powerbudget range of current 2U CubeSats. To our knowledge, this is the first COTS-based, reproducible on-board-computer architecture that can offer strong fault coverage even for small CubeSats.European Space AgencyComputer Systems, Imagery and Medi