具有安全保障的FACE环境管理程序的体系结构与应用

J. Myren, Mitch Groen
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引用次数: 0

摘要

柯林斯宇航公司认识到作战人员从减小航空电子系统的尺寸、重量和功率(SWAP)中获得的价值。作战人员还从现有航空电子设备和任务软件模块的重用中获益,这些模块在软件框架中经常变化,因此被分配到单独的处理器上。正如在商业IT行业中看到的那样,一种解决方案是使用多核处理和管理程序,允许混合框架,以最小的SWAP提供快速集成。在航空电子方面,我们必须额外提供保证。本文将探讨我们对FACE™技术标准(参考文献[1])的应用,以获得框架可变性,并与管理程序一起使用,以允许最终框架存在于单个多核处理环境中,并确保解决方案的安全。通过在同一多核处理器上运行的美国陆军和柯林斯软件的演示,验证了所提出的概念。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Architecture And Application Of Hypervisor In FACE Environment With Safety Assurance
Collins Aerospace recognizes the value the warfighter gets from reducing the Size, Weight and Power (SWAP) of the avionics systems. The war fighter also sees benefit from reuse of existing avionics and mission software modules, which frequently vary in software framework and thus are allocated to separate processors. A solution, as seen in the commercial IT industry would be the use of multi-core processing and hypervisors allowing the mixing of frameworks providing rapid integration with minimal SWAP. In avionics we must additionally provide assurance. This paper will explore our application of the FACE™ Technical Standard (Ref. [1]) to obtain framework variability, used in conjunction with a hypervisor to allow the resulting frameworks to exist in a single multi-core processing environment with safety assurance to the solution. The concept proposed was validated through demonstration of US Army and Collins software running on the same multi-core processor.
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