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2021 10th Latin-American Symposium on Dependable Computing (LADC)最新文献

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V-Model Adaptation for Space Systems in Light of the ECSS Standard 基于ECSS标准的空间系统v型自适应
Pub Date : 2021-11-01 DOI: 10.1109/ladc53747.2021.9672593
Regina L. O. Moraes, Tânia Basso, Eliane Martins
A challenge in the space domain is to adapt the V&V (Verification and Validation) process to answer to the growing importance of embedded software and still comply with international standards. This work presents an analysis of the ECSS (European Cooperation for Space Standardization) standard to allow the adaptation of the well-known V-Model for Cyber-Physical System (CPS), particularly for space systems. The result is a complete model capable of representing the physical and software segments, as well as positioning ECSS revisions throughout the system development and its testing/validation tasks.
空间领域的一个挑战是适应V&V(验证和验证)过程,以满足嵌入式软件日益增长的重要性,同时仍然符合国际标准。这项工作提出了对ECSS(欧洲空间标准化合作)标准的分析,以允许对众所周知的网络物理系统(CPS)的v模型进行改编,特别是对空间系统。结果是一个完整的模型,能够表示物理和软件部分,以及在整个系统开发及其测试/验证任务中定位ECSS修订。
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引用次数: 0
WSENSING: Program
Pub Date : 2021-11-01 DOI: 10.1109/ladc53747.2021.9672558
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引用次数: 0
Towards Simulation of CubeSat Operational Scenarios under a Cyber-Physical Systems View 基于信息物理系统的立方体卫星运行场景模拟
Pub Date : 2021-11-01 DOI: 10.1109/ladc53747.2021.9672594
Danilo Pallamin de Almeida, Bence Graics, R. Chagas, F. Sousa, Fátima Mattiello-Francisco
In the development of academic CubeSat-based space missions, it is common to skip or rush many practices of the Systems Engineering Process due to time and cost constraints, which may lead to issues later on in the mission and failures. Mission concept analyses are often in these practices, including the analysis of the in-orbit behavior of the satellite with respects to power consumption and data generation. With the purpose of supporting these analyses, this article introduces a workflow based on a Cyber-Physical abstraction of CubeSat mission operation scenarios, which uses architectural models based on SysML Class Diagrams and automatic model transformation to support the simulation of these operational scenarios in an open source Model-Based System Engineering (MBSE) tool. These simulations can be used in mission concept analyses in Phase-0 studies to verify initial operations requirements and drive further design implementations.
在基于立方体卫星的学术空间任务的发展中,由于时间和成本的限制,跳过或匆忙进行系统工程过程的许多实践是很常见的,这可能导致任务后期的问题和失败。任务概念分析经常在这些实践中进行,包括对卫星在轨行为的功耗和数据生成的分析。为了支持这些分析,本文介绍了一个基于CubeSat任务操作场景的网络物理抽象的工作流,它使用基于SysML类图的体系结构模型和自动模型转换来支持开源的基于模型的系统工程(MBSE)工具中这些操作场景的仿真。这些模拟可用于0阶段研究的任务概念分析,以验证初始操作需求并推动进一步的设计实现。
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引用次数: 1
Revocation Mechanisms for Blockchain Applications: A Review 区块链应用程序的撤销机制:综述
Pub Date : 2021-11-01 DOI: 10.1109/ladc53747.2021.9672577
F. Vidal, N. Ivaki, N. Laranjeiro
Nowadays, blockchain has been adopted by applications that are beyond cryptocurrencies. In such applications, the data generated or transactions executed are likely to be altered (revoked) due to several reasons, including business requests, legislation, or the existence of bugs. In addition, most of the data are being created by smart contracts, which, in many cases, are built by developers with non-sophisticated development tools or lacking expertise, leading to code holding residual bugs. In blockchain systems, in which immutability is one of the most critical characteristics, implementing reliable, secure, and efficient (i.e., in terms of time) revocation is a difficult challenge. This paper reviews 8 revocation mechanisms identified in current literature and discusses the applicability of each solution and associated challenges. We expect that our analysis contributes to the definition of new or improved mechanisms for transaction and data revocation in blockchain systems.
如今,区块链已被加密货币以外的应用程序所采用。在这样的应用程序中,生成的数据或执行的事务可能会由于多种原因而被更改(撤销),包括业务请求、立法或存在错误。此外,大多数数据都是由智能合约创建的,在许多情况下,智能合约是由使用非复杂开发工具或缺乏专业知识的开发人员构建的,导致代码中存在残留的错误。在区块链系统中,不变性是最关键的特征之一,实现可靠、安全和有效(即在时间方面)的撤销是一项艰巨的挑战。本文回顾了当前文献中确定的8种撤销机制,并讨论了每种解决方案的适用性和相关挑战。我们期望我们的分析有助于定义区块链系统中新的或改进的事务和数据撤销机制。
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引用次数: 1
Towards the Formal Semantics of Scenario Tests for Autonomous Vehicles 自动驾驶汽车场景测试的形式语义研究
Pub Date : 2021-11-01 DOI: 10.1109/ladc53747.2021.9672554
László Kovács, Oszkár Semeráth
Testing self-driving components in autonomous vehicles is a challenging task. Such components need to interact with a complex and continuously changing environment, making traditional software testing approaches ineffective or impractical. Scenario-based testing approaches aim to define various traffic situations to support this testing of autonomous components by providing sensor inputs for them while monitoring the output of the actuators. However, we need a formal description of traffic scenarios to measure some coverage metrics or synthesize traffic scenarios. This paper proposes mathematically precise behavior formalization to achieve this by using graph transformation rules. We show that our formalization can cover existing scenario specification implementation, such as Scenic.
在自动驾驶汽车中测试自动驾驶组件是一项具有挑战性的任务。这些组件需要与复杂且不断变化的环境交互,这使得传统的软件测试方法无效或不切实际。基于场景的测试方法旨在定义各种交通情况,通过为自动驾驶组件提供传感器输入,同时监控执行器的输出,从而支持自动驾驶组件的测试。然而,我们需要流量场景的正式描述来度量一些覆盖度量或综合流量场景。本文提出了用图变换规则实现数学上精确的行为形式化。我们展示了我们的形式化可以覆盖现有的场景规范实现,比如Scenic。
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引用次数: 0
Impact Assessment of IT Security Breaches in Cyber-Physical Systems: Short paper 网络物理系统中IT安全漏洞的影响评估:短文
Pub Date : 2021-11-01 DOI: 10.1109/ladc53747.2021.9672582
András Földvári, G. Biczók, I. Kocsis, László Gönczy, A. Pataricza
The increased cyber-attack surface in cyber-physical systems, the close coupling to vulnerable physical processes, and the potential for human casualties necessitate a careful extension of traditional safety methodologies, e.g., error propagation analysis (EPA), with cybersecurity capabilities. We propose a model-driven Information Technology/Operational Technology impact analysis method that supports identifying vulnerabilities, most critical attack strategies, and most dangerous threat actors by analyzing attack scenarios on an abstract functional model of the system. Our solution extends EPA, initially developed for dependability and safety analysis, with cybersecurity aspects to explore the safety impact of a cyber attack on a cyber-physical system. The paper presents the impact analysis workflow, the threat model, the pilot analysis tool, and a case study.
网络物理系统中不断增加的网络攻击面,与脆弱物理过程的紧密耦合,以及潜在的人员伤亡,都需要谨慎地扩展传统的安全方法,例如错误传播分析(EPA),并具有网络安全功能。我们提出了一种模型驱动的信息技术/操作技术影响分析方法,该方法通过分析系统抽象功能模型上的攻击场景,支持识别漏洞、最关键的攻击策略和最危险的威胁参与者。我们的解决方案扩展了EPA,最初是为可靠性和安全性分析而开发的,具有网络安全方面,以探索网络攻击对网络物理系统的安全影响。本文介绍了影响分析工作流程、威胁模型、试点分析工具和案例分析。
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引用次数: 2
Fault injection platform for affordable verification and validation of CubeSats software 用于负担得起的CubeSats软件验证和验证的故障注入平台
Pub Date : 2021-11-01 DOI: 10.1109/ladc53747.2021.9672584
David Paiva, José Marcelo Duarte, R. Lima, Manoel Carvalho, Fátima Mattiello-Francisco, H. Madeira
CubeSats and very small satellites represent an emergent trend in the space industry. These satellites use commercial off-the-shelf (COTS) components to reduce cost and take advantage of the performance/power consumption ratio of COTS, which is an order of magnitude better than the equivalent radiation hardened space grade components. Unfortunately, COTS components are susceptible to Single Event Upsets (SEU), which are transient errors caused by space radiation. This makes the study of the impact of faults caused by space radiation a mandatory step in the development of CubSats, in order to carefully evaluate weak points that must be strengthened through the use of specific software fault tolerance techniques. The fact that the impact of faults is strongly dependent on the software running on the COTS hardware indicates that the study of the impact of radiation faults must be carried out every time the CubeSat software has a major change, or even a minor update. This paper proposes CubeSatFI, a fault injection platform for CubeSats meant to facilitate the incorporation of this extra step in the Verification and Validation of CubeSats software. CubeSatFI allows the easy definition of fault injection campaigns that emulate the effects of space radiation. SEU are emulated realistically through bit-flip faults injected in the processor registers and in other locations of the CubeSat boards that can be reached by boundary-scan, which is available in CubeSat boards through JTAG Test Access Port. The execution of the fault injection campaigns is controlled by the CubeSatFI platform in a fully automated mode. The paper describes the architecture of the CubeSatFI platform, the fault models, and the general fault injection process. Additionally, the use of the CubeSatFI platform is demonstrated with a fault injection campaign for the EDC (Environment Data Collection), a payload system that will be used in a constellation of satellite from the Brazilian National Institute for Space Research (Instituto Nacional de Pesquisas Espaciais - INPE), providing a first realistic insight on the impact of faults in the EDC software.
立方体卫星和非常小的卫星代表了航天工业的一个新兴趋势。这些卫星使用商用现货(COTS)组件来降低成本,并利用COTS的性能/功耗比,这比等效的辐射硬化空间级组件好一个数量级。不幸的是,COTS组件容易受到单事件扰动(SEU)的影响,这是由空间辐射引起的瞬态误差。这使得研究空间辐射引起的故障的影响成为开发CubSats的一个强制性步骤,以便仔细评估必须通过使用特定软件容错技术来加强的弱点。故障的影响很大程度上取决于运行在COTS硬件上的软件,这表明每次CubeSat软件发生重大变化,甚至是小的更新时,都必须进行辐射故障影响的研究。本文提出了CubeSatFI,这是一个立方体卫星的故障注入平台,旨在促进在立方体卫星软件的验证和验证中加入这一额外步骤。CubeSatFI可以轻松定义模拟空间辐射影响的断层注入活动。通过注入到处理器寄存器和CubeSat板的其他位置的位翻转故障,可以通过边界扫描(通过JTAG测试访问端口在CubeSat板中提供)来真实地模拟SEU。故障注入作业的执行由CubeSatFI平台以全自动模式控制。本文介绍了CubeSatFI平台的体系结构、故障模型和故障注入的一般流程。此外,CubeSatFI平台通过EDC(环境数据收集)的故障注入活动进行了演示,EDC(环境数据收集)是一个有效载荷系统,将用于巴西国家空间研究所(INPE)的一个卫星星座,首次提供了对EDC软件故障影响的现实见解。
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引用次数: 2
A Systemic Approach to Aircraft System Supportability 飞机系统可保障性的系统方法
Pub Date : 2021-11-01 DOI: 10.1109/ladc53747.2021.9672564
C. Silva, Claudio Medrado Filho, Alexandre Magno Pinto
This paper explores supportability of an aircraft system aiming to proactively incorporate it in concept definition in the Systems Engineering Processes. System-Theoretic Accident Model and Process (STAMP) approach provided the foundation for the analysis conducted herein, strengthening the perspective on how to avoid value losses related to support activities. Results bring important life cycle concerns into consideration for a “design-in” perspective for an aircraft system in conceptual studies.
本文探讨了飞机系统的可支持性,旨在将其积极地纳入系统工程过程中的概念定义。系统理论事故模型和过程(STAMP)方法为本文的分析提供了基础,加强了如何避免与支持活动相关的价值损失的视角。研究结果将重要的生命周期问题纳入概念研究中飞机系统的“设计”视角。
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引用次数: 0
Towards Testing the UML PSSM Test Suite 面向UML PSSM测试套件的测试
Pub Date : 2021-11-01 DOI: 10.1109/ladc53747.2021.9672570
Márton Elekes, Zoltán Micskei
In model-based engineering approaches, models are executable artefacts used for simulation, generation and verification. The Executable UML specifications enriched the well-known UML language with precisely defined semantics. The Precise Semantics of UML State Machines (PSSM) specification defined an operational semantics for state machines. Moreover, the specification contains a detailed test suite that illustrates the semantics and can be used to check the conformance of model execution tools. However, as the test suite itself is a complex engineering effort, it could contain errors. To the best of our knowledge, this is the first paper to test and verify the PSSM test suite. We report on typical errors and issues found by reviewing the specification and executing it in one of the supporting tools. Finally, we collect recommendations for such test suites that could enhance future modelling language specifications.
在基于模型的工程方法中,模型是用于仿真、生成和验证的可执行工件。可执行UML规范用精确定义的语义丰富了众所周知的UML语言。UML状态机的精确语义(PSSM)规范定义了状态机的操作语义。此外,该规范包含详细的测试套件,用于说明语义,并可用于检查模型执行工具的一致性。然而,由于测试套件本身是一项复杂的工程工作,它可能包含错误。据我们所知,这是第一篇测试和验证PSSM测试套件的论文。我们通过审查规范并在一个支持工具中执行它来报告发现的典型错误和问题。最后,我们收集了这些测试套件的建议,这些测试套件可以增强未来的建模语言规范。
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引用次数: 1
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Pub Date : 2021-11-01 DOI: 10.1109/ladc53747.2021.9672585
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引用次数: 0
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2021 10th Latin-American Symposium on Dependable Computing (LADC)
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