High-Assurance Separation Kernels: a Survey on Formal Methods
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Software Model Checking of ARINC-653 Flight Code with MCP Sarah J
Software Model Checking of ARINC-653 Flight Code with MCP Sarah J. Thompson Guillaume Brat SGT Inc., NASA Ames Research Center CMU, NASA Ames Research Center MS269-1, Moffett Field, California MS-269-1, Moffett Field, California [email protected] [email protected] Arnaud Venet SGT Inc., NASA Ames Research Center MS269-1, Moffett Field, California [email protected] Abstract The ARINC-653 standard defines a common interface for Integrated Modular Avionics (IMA) code. In particular, ARINC-653 Part 1 specifies a process- and partition-management API that is analogous to POSIX threads, but with certain extensions and restrictions intended to support the implementation of high reliability flight code. MCP is a software model checker, developed at NASA Ames, that provides capabilities for model checking C and C++ source code. In this paper, we present recent work aimed at implementing extensions to MCP that support ARINC-653, and we discuss the challenges and opportunities that consequentially arise. Providing support for ARINC-653’s time and space partitioning is nontrivial, though there are implicit benefits for partial order reduction possible as a consequence of the API’s strict interprocess communication policy. 1 Introduction NASA missions are becoming increasingly complex, and, more and more of this complexity is imple- mented in software. In 1977, the flight software for the Voyager mission amounted to only 3000 lines. Twenty years later, the software for Cassini had grown by a factor of ten, and more strikingly, the soft- ware for the Mars Path Finder mission amounted to 160 KLOCs (thousands of lines of code). -
Communications for Integrated Modular Avionics
Communications for Integrated Modular Avionics Richard L. Alena [email protected] John P. Ossenfort IV, SAIC Kenneth I. Laws, QSS Andre Goforth NASA Ames Research Center Moffett Field, CA 94035 Fernando Figueroa, NASA Stennis Space Center TABLE OF CONTENTS Abstract—The aerospace industry has been adopting avionics architectures to take advantage of advances in computer engineering. Integrated Modular Avionics (IMA), 1. INTRODUCTION ..................................................... 1 as described in ARINC 653, distributes functional modules 2. INTEGRATED MODULAR AVIONICS...................... 2 into a robust configuration interconnected with a “virtual 3. NETWORKS FOR AEROSPACE ............................... 4 backplane” data communications network. Each avionics 4. MISSION COMPUTER DESIGN............................... 8 module’s function is defined in software compliant with the 5. LAB EVALUATION............................................... 12 APEX Application Program Interface. The Avionics Full- 6. CONCLUSIONS..................................................... 16 Duplex Ethernet (AFDX) network replaces the point-to- REFERENCES........................................................... 17 point connections used in previous distributed systems with BIOGRAPHY ............................................................ 18 “virtual links”. This network creates a command and data path between avionics modules with the software and 1. INTRODUCTION network defining the active virtual links over an integrated physical network. -
Avionics Applications on a Time-Predictable Chip-Multiprocessor
Avionics Applications on a Time-predictable Chip-Multiprocessor Andre´ Rocha and Claudio´ Silva Rasmus Bo Sørensen, Jens Sparsø, and Martin Schoeberl GMV Department of Applied Mathematics and Computer Science Lisbon, Portugal Technical University of Denmark Email: [andre.rocha, claudio.silva]@gmv.com Email: [rboso, jspa, masca]@dtu.dk Abstract—Avionics applications need to be certified for The demonstrators were ported to the T-CREST platform the highest criticality standard. This certification includes using its compiler tool-chain and analysis tools. The demon- schedulability analysis and worst-case execution time (WCET) strators validate the T-CREST platform. Part of the exercise, analysis. WCET analysis is only possible when the software is written to be WCET analyzable and when the platform is however, is to evaluate the added value of the platform. The time-predictable. In this paper we present prototype avionics platform shall enable application developers to determine the applications that have been ported to the time-predictable WCET of their applications more precisely or more easily. T-CREST platform. The applications are WCET analyzable, Therefore, we compare the T-CREST platform with a well- and T-CREST is supported by the aiT WCET analyzer. This established platform in the avionics domain. combination allows us to provide WCET bounds of avionic tasks, even when executing on a multicore processor. The T-CREST platform was evaluated with the aid of the following three real-world avionic applications: (1) an Airlines Operational Centre (AOC), (2) a Crew Alerting I. INTRODUCTION System (CAS), and (3) an I/O Partition (IOP). We chose The mission of the T-CREST project [1], [2] is to develop T-CREST as platform for avionics applications as this is and build a multicore processor that is time-predictable and currently the only multicore processor where static WCET easy to analyze for the worst-case execution time (WCET). -
Lynuxworks Lynxsecure Embedded Hypervisor and Separation
Operating systems: RTOS and tools Software LynuxWorks, Inc. 855 Embedded Way • San Jose, CA 95138 800-255-5969 www.lynuxworks.com LynxSecure Embedded Hypervisor and Separation Kernel With the introduction of the new LynxSecure separation kernel and embedded hypervisor, LynuxWorks once again raises the bar when it comes to superior embedded software security and safety. LynxSecure has been built from the ground up as a real-time separa- tion kernel able to run different operating systems and applications in their own secure partitions. The LynxSecure separation kernel is a virtual machine monitor that is certifi able to (a) Common Criteria EAL 7 (Evaluated Assurance Level 7) security certifi cation, a level of certifi cation unattained by any known operating system to date; and (b) DO-178B Level A, the highest level of FAA certifi cation for safety-critical avionics applications. LynxSecure conforms to the Multiple Independent Levels of Security/ Safety (MILS) architecture. The embedded hypervisor component of LynxSecure allows multiple “guest” operating systems to run in their own secure partitions. These can be run in either paravirtual- ized or fully virtualized modes, helping preserve legacy applications and operating systems in systems that now have a security require- FEATURES ment. Guest operating systems include the LynxOS family, Linux and › Optimal security and safety – the only operating system designed to Windows. support CC EAL 7 and DO-178B Level A › Real time – time-space partitioned RTOS for superior determinism and performance -
Cloud Computing Bible Is a Wide-Ranging and Complete Reference
A thorough, down-to-earth look Barrie Sosinsky Cloud Computing Barrie Sosinsky is a veteran computer book writer at cloud computing specializing in network systems, databases, design, development, The chance to lower IT costs makes cloud computing a and testing. Among his 35 technical books have been Wiley’s Networking hot topic, and it’s getting hotter all the time. If you want Bible and many others on operating a terra firma take on everything you should know about systems, Web topics, storage, and the cloud, this book is it. Starting with a clear definition of application software. He has written nearly 500 articles for computer what cloud computing is, why it is, and its pros and cons, magazines and Web sites. Cloud Cloud Computing Bible is a wide-ranging and complete reference. You’ll get thoroughly up to speed on cloud platforms, infrastructure, services and applications, security, and much more. Computing • Learn what cloud computing is and what it is not • Assess the value of cloud computing, including licensing models, ROI, and more • Understand abstraction, partitioning, virtualization, capacity planning, and various programming solutions • See how to use Google®, Amazon®, and Microsoft® Web services effectively ® ™ • Explore cloud communication methods — IM, Twitter , Google Buzz , Explore the cloud with Facebook®, and others • Discover how cloud services are changing mobile phones — and vice versa this complete guide Understand all platforms and technologies www.wiley.com/compbooks Shelving Category: Use Google, Amazon, or -
WIND RIVER Vxworks 653 PLATFORM 2.4 and 2.5
WIND RIVER VxWORKS 653 PLATFORM 2.4 AND 2.5 TABLE OF CONTENTS RTCA DO-178C Certification Evidence .......................................... 2 VxWorks 653 Platform Benefits ................................................. 2 VxWorks 653 Runtime Components ............................................ 3 VxWorks 653 Module OS ................................................... 4 Partition Management ..................................................... 4 Partition Scheduling ....................................................... 4 Partition Operating System ................................................. 4 COIL .................................................................... 5 APEX Application Support .................................................. 5 FACE Technical Reference 2.0 and 2.1 Support ................................ 5 Inter-partition Communication ............................................... 6 Intra-partition Communication ............................................... 6 Health Monitor ........................................................... 6 Wind River Workbench ..................................................... 7 Included Runtime Products .................................................. 12 Wind River DO-178C Network Stack ......................................... 12 Wind River Highly Reliable File System ....................................... 12 Technical Specifications ..................................................... 12 Supported Target Architectures ........................................... -
Towards a Real-Time Component Framework for Software Health Management
Institute for Software Integrated Systems Vanderbilt University Nashville, Tennessee, 37203 Towards a Real-time Component Framework for Software Health Management Abhishek Dubey , Gabor Karsai , Robert Kereskenyi , Nagabhushan Mahadevan TECHNICAL REPORT ISIS-09-111 November, 2009 Towards a Real-time Component Framework for Software Health Management Abhishek Dubey Gabor Karsai Robert Kereskenyi Nagabhushan Mahadevan Institute for Software Integrated Systems, Vanderbilt University, Nashville, TN 37203, USA Abstract— The complexity of software in systems like aerospace industry, that deals with detecting anomalies, di- aerospace vehicles has reached the point where new techniques agnosing failure sources, and prognosticating future failures are needed to ensure system dependability. Such techniques in complex systems, like aerospace vehicles. While System include a novel direction called ‘Software Health Management’ (SHM) that extends classic software fault tolerance with tech- Health Management has been developed for physical (hard- niques borrowed from System Health Management. In this ware) systems, it provides interesting systems engineering paper the initial steps towards building a SHM approach are techniques for other fields like embedded software systems. described that combine component-based software construction The use of System Health Management techniques for with hard real-time operating system platforms. Specifically, embedded software systems points beyond the capabilities the paper discusses how the CORBA Component Model could be combined with the ARINC-653 platform services and the provided by the SFT techniques and can potentially in- lessons learned from this experiment. The results point towards crease a system’s dependability. This new direction is called both extending the CCM as well as revising the ARINC-653. Software Health Management (SHM) [4]. -
(DBATU Iope) Question Bank (MCQ) Cloud Computing Elective II
Diploma in Computer Engineering (DBATU IoPE) Question Bank (MCQ) Cloud Computing Elective II (DCE3204A) Summer 2020 Exam (To be held in October 2020 - Online) Prepared by Prof. S.M. Sabale Head of Computer Engineering Institute of Petrochemical Engineering, Lonere Id 1 Question Following are the features of cloud computing: (CO1) A Reliability B Centralized computing C Location dependency D No need of internet connection Answer Marks 2 Unit I Id 2 Question Which is the property that enables a system to continue operating properly in the event of the failure of some of its components? (CO1) A Availability B Fault-tolerance C Scalability D System Security Answer Marks 2 Unit I Id 3 Question A _____________ is a contract between a network service provider and a customer that specifies, usually in measurable terms (QoS), what services the network service provider will furnish (CO1) A service-level agreement B service-level specifications C document D agreement Answer Marks 2 Unit I Id 4 Question The degree to which a system, subsystem, or equipment is in a specified operable and committable state at the start of a mission, when the mission is called for at an unknown time is called as _________ (CO1) A reliability B Scalability C Availability D system resilience Answer Marks 2 Unit I Id 5 Question Google Apps is an example of (CO1) A IaaS B SaaS C PaaS D Both PaaS and SaaS Answer Marks 2 Unit I Id 6 Question Separation of a personal computer desktop environment from a physical machine through the client server model of computing is known as __________. -
ARINC-653 Inter-Partition Communications and the Ravenscar Profile
ARINC-653 Inter-partition Communications and the Ravenscar Profile Jorge Garrido Juan Zamorano Juan A. de la Puente Abstract The ARINC-653 standard is often used to build mixed-criticality systems, using a partitioned archi tecture. Inter-partition communication is carried out by means of a message-passing mechanism based on ports. The standard includes an API for Ada, but the implementation semantics of operation ports is not fully defined. Furthermore, the API was defined for the Ada 95 standard, and therefore does not take into account the enhancements to the real-time features of the language that have been incorporated in the 2005 and 2013 standards, most notably the Ravenscar profile. This paper is aimed at clarifying the implementation of ARINC communication ports in Ada and the Ravenscar profile. ARINC communi cation ports are analysed, and their compatibility with the Ravenscar profile is assessed. A new API that can be used with the profile is defined, and a pilot implementation is introduced. 1 Introduction Partitioning is a convenient approach for developing mixed-criticality systems on a single hardware plat form. Under this approach, a system is divided into a set of logical partitions, which are isolated from each other both in the temporal and spatial domains. Subsystems with different levels of criticaliry are allocated to different partitions, and failures in low-criticality components cannot propagate to high-criticality ones. Critical subsystems can thus be certified in isolation to the required level, provided that the partitioning ker nel is also certified to that level, but the validation of lower-criticality subsystems can be greatly simplified. -
ARINC-653 Inter-Partition Communications and the Ravenscar Profile∗
ARINC-653 Inter-partition Communications and the Ravenscar Profile∗ Jorge Garrido Juan Zamorano Juan A. de la Puente [email protected] jzamora@datsi.fi.upm.es [email protected] Universidad Politecnica´ de Madrid (UPM), Spain Abstract The ARINC-653 standard is often used to build mixed-criticality systems, using a partitioned archi- tecture. Inter-partition communication is carried out by means of a message-passing mechanism based on ports. The standard includes an API for Ada, but the implementation semantics of operation ports is not fully defined. Furthermore, the API was defined for the Ada 95 standard, and therefore does not take into account the enhancements to the real-time features of the language that have been incorporated in the 2005 and 2013 standards, most notably the Ravenscar profile. This paper is aimed at clarifying the implementation of ARINC communication ports in Ada and the Ravenscar profile. ARINC communi- cation ports are analysed, and their compatibility with the Ravenscar profile is assessed. A new API that can be used with the profile is defined, and a pilot implementation is introduced. 1 Introduction Partitioning is a convenient approach for developing mixed-criticality systems on a single hardware plat- form. Under this approach, a system is divided into a set of logical partitions, which are isolated from each other both in the temporal and spatial domains. Subsystems with different levels of criticality are allocated to different partitions, and failures in low-criticality components cannot propagate to high-criticality ones. Critical subsystems can thus be certified in isolation to the required level, provided that the partitioning ker- nel is also certified to that level, but the validation of lower-criticality subsystems can be greatly simplified. -
And Space-Partitioned Architecture for the Next Generation of Space Vehicle Avionics
Building a Time- and Space-Partitioned Architecture for the Next Generation of Space Vehicle Avionics Jos´e Rufino, Jo˜ao Craveiro, and Paulo Verissimo University of Lisbon, Faculty of Sciences, LaSIGE [email protected], [email protected], [email protected] Abstract. Future space systems require innovative computing system architectures, on account of their size, weight, power consumption, cost, safety and maintainability requisites. The AIR (ARINC 653 in Space Real-Time Operating System) architecture answers the interest of the space industry, especially the European Space Agency, in transitioning to the flexible and safe approach of having onboard functions of different criticalities share hardware resources, while being functionally separated in logical containers (partitions). Partitions are separated in the time and space domains. In this paper we present the evolution of the AIR architecture, from its initial ideas to the current state of the art. We describe the research we are currently performing on AIR, which aims to obtain an industrial-grade product for future space systems, and lay the foundations for further work. 1 Introduction Space systems of the future demand for innovative embedded computing system architectures, meeting requirements of different natures. These systems must obey to strict dependability and real-time requirements. Reduced size, weight and power consumption (SWaP), along with low wiring complexity, are also crucial requirements both for safety reasons and to decrease the overall cost of a mission. A modular approach to software enabling component reuse among the different space missions also benefits the cost factor. At the same time, such an approach allows independent validation and verification of components, thus easing the software certification process. -
Model-Based Development of ARINC 653 Using UML and Sysml Andreas Korff, Atego – OMG RT Workshop, Paris, 18.04.2012
Model-based development of ARINC 653 using UML and SysML Andreas Korff, Atego – OMG RT Workshop, Paris, 18.04.2012 © 2011 Atego. All Rights Reserved. 1 Agenda Motivation of Integrated Modular Systems Modelling Notation Standards UML and SysML Applying UML and SysML to IMS ARINC 653 Using Models to support ARINC 653 Conclusion © 2011 Atego. All Rights Reserved. 2 Motivation of Integrated Modular Systems Integrated Modular Systems (or IMA) aim to Minimize Life Cycle Costs Enhance Mission and Operational Performance Allow greater flexibility and re-use in Development and Maintenance Existing standards for IMS ARINC 653 – for implementing IMS concepts onto RTOSes Stanag 4626/EN 4660 – to de-couple Avionics HW and SW © 2011 Atego . All Rights Reserved. 3 Federated Architectures (shown with UML) Broad range of possible problems: Any failure effects everything Scheduling sensitive to any change Difficult to maintain: Obsolecence One change effects again everything Re-Use? © 2011 Atego. All Rights Reserved. 4 A closer Look on Federated Architectures On Closer inspection, logical ‘wrappers’ appear that perform specific functions. These can be interpreted as ‘layers’ in a Federated Architecture Physical Interface Layer Central Data Formatting Layer Controller Data Processing Layer © 2011 Atego. All Rights Reserved. 5 From Federated to a Layered Architecture In an IMS layered architecture each layer has a clearly defined responsibility, interface and is as important as each of the other layers Federated Architecture Stanag 4626/EN 4660 (ASAAC) {maps for logic} Data Processing Layer Application Layer {maps for scheduling} {maps} Data Formating Layer Operating System Layer Physical Interface Lacer Module Support Layer © 2011 Atego.