基于组件的可靠分布式可重构航天器机载计算机中间件

T. Peng, Kilian Hoflinger, B. Weps, O. Maibaum, K. Schwenk, D. Lüdtke, A. Gerndt
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引用次数: 6

摘要

空间任务的新兴应用要求机载计算机提高处理性能。DLR的“下一代机载计算机”(OBC-NG)项目开发了一种分布式、可重构的计算机体系结构,以提供更高的性能,同时保持经典航天器计算机体系结构的高可靠性。不断增长的系统复杂性需要先进的板载中间件来处理分布式(实时)应用程序,并通过重新配置来减少错误。OBC-NG中间件遵循基于组件的软件工程(CBSE)方法。使用组合组件,应用程序和管理任务可以很容易地分布和重新定位到网络的处理节点上。此外,还为今后的特派团重新使用组件提供便利。本文介绍了OBC-NG的灵活中间件体系结构、组合组件框架、中间件服务和模型驱动的应用程序编程接口(API)设计。通过测试验证了中间件的概念,并研究了系统的重构效率和可靠性。一个相关的用例显示了CBSE在开发分布式可重构板载软件方面的优势。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
A Component-Based Middleware for a Reliable Distributed and Reconfigurable Spacecraft Onboard Computer
Emerging applications for space missions require increasing processing performance from the onboard computers. DLR's project "Onboard Computer - Next Generation" (OBC-NG) develops a distributed, reconfigurable computer architecture to provide increased performance while maintaining the high reliability of classical spacecraft computer architectures. Growing system complexity requires an advanced onboard middleware, handling distributed (real-time) applications and error mitigation by reconfiguration. The OBC-NG middleware follows the Component-Based Software Engineering (CBSE) approach. Using composite components, applications and management tasks can easily be distributed and relocated on the processing nodes of the network. Additionally, reuse of components for future missions is facilitated. This paper presents the flexible middleware architecture, the composite component framework, the middleware services and the model-driven Application Programming Interface (API) design of OBC-NG. Tests are conducted to validate the middleware concept and to investigate the reconfiguration efficiency as well as the reliability of the system. A relevant use case shows the advantages of CBSE for the development of distributed reconfigurable onboard software.
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