A commercial off-the-shelf based replacement strategy for aging avionics computers

J. Luke, J.W. Bittorie, W. Cannon, D. Haldeman
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引用次数: 5

Abstract

With decreasing defense dollars available to purchase new military aircraft, the inventory of existing aircraft will have to last many more years than originally anticipated. As the avionics computers on these aging aircraft get older, they become more expensive to maintain due to parts obsolescence. In addition, expanding missions and changing requirements lead to growth in the embedded software which, in turn, requires additional processing and memory capacity. Both factors, parts obsolescence and new processing capacity, result in the need to replace the old computer hardware with newer, more capable microprocessor technology. New microprocessors, however, are not compatible with the older computer instruction set architectures. This generally requires the embedded software in these computers to be rewritten. A significant savings-estimated in the billions of dollars-could be achieved in these upgrades if the new computers could execute the old embedded code along with any new code to be added. This paper describes a commercial-off-the-shelf (COTS) based form, fit, function, and interface (F/sup 3/I) replacement strategy for legacy avionics computers that can reuse existing avionics code "as is" while providing a flexible framework for incremental upgrades and managed change. It is based on a real-time embedded software technology that executes legacy binary code on the latest generation COTS microprocessors. This technology, developed by TRW and being applied under the sponsorship of the Air Force Research Lab (AFRL), promises performance improvements of 5-10 times that of the legacy avionics computer that it replaces. It also promises a 4X decrease in cost and schedule over rewriting the code and provides a "known good" starting point for incremental upgrades of the embedded flight software. Code revalidation cost and risk are minimized since the structure of the embedded code is not changed, allowing the replacement computer to be retested at the "blackbox" level using existing qualification tests.
一种商用的现成的基于老化航空电子计算机的替换策略
随着可用于购买新军用飞机的国防资金的减少,现有飞机的库存将不得不比原先预期的持续更长时间。随着这些老旧飞机上的航空电子计算机越来越老,由于零件过时,它们的维护成本也越来越高。此外,任务的扩展和需求的变化导致嵌入式软件的增长,这反过来又需要额外的处理和内存容量。零件过时和新的处理能力这两个因素导致需要用更新、更强大的微处理器技术取代旧的计算机硬件。然而,新的微处理器与旧的计算机指令集体系结构不兼容。这通常需要重写这些计算机中的嵌入式软件。如果新计算机能够在执行旧的嵌入式代码的同时添加任何新代码,那么在这些升级中就可以节省大量的费用,估计可以节省数十亿美元。本文描述了一种基于商用现货(COTS)的形式、配合、功能和接口(F/sup 3/I)的替代策略,该策略可以“按原样”重用现有的航空电子设备代码,同时为增量升级和管理变更提供灵活的框架。它基于实时嵌入式软件技术,在最新一代COTS微处理器上执行遗留二进制代码。该技术由TRW开发,并在空军研究实验室(AFRL)的赞助下得到应用,承诺其取代的传统航空电子计算机的性能提高5-10倍。它还承诺将重写代码的成本和进度降低4倍,并为嵌入式飞行软件的增量升级提供了一个“已知的良好”起点。代码重新验证的成本和风险降到最低,因为嵌入式代码的结构没有改变,允许使用现有的资格测试在"黑箱"一级对替换的计算机进行重新测试。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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