下一代空间航空电子设备:高度可靠的分层系统实现

R. Black, M. Fletcher
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引用次数: 9

摘要

在过去的十年里,电子技术的进步使个人计算机系统的能力和灵活性有了很大的提高。不幸的是,目前用于空间应用的航空电子系统通常没有利用这些COTS优势。最近,出现了利用商业总线互连的趋势,主要是VME和PCI。这些并行互连的缺点是单个故障可以禁用整个冗余字符串。霍尼韦尔为航空电子系统开发了一种正在申请专利的体系结构,该体系结构结合了以前串行系统的高可靠性和直接COTS总线接口的灵活性和开放性。十年前,航空电子系统的技术水平从20世纪80年代的PAVE PILLAR系统到波音777中使用的集成模块化航空电子设备(IMA)发生了重大变化。下一代航空电子架构不是基于传统的拜占庭冗余结构,而是基于事实的方案,其中每个元素都知道何时发生内部故障并将自己从系统中移除。IMA采用锁步微处理器设计,可与COTS背板进行输入/输出通信,并与虚拟背板/sup /spl贸易//(可靠的高速串行总线,如1394或AFDX)进行系统内通信。系统功能采用arinc653时空分区操作系统实现。整个系统提供了简单系统的简单性,实现了最高级别的可靠性,为重新配置软件应用程序和硬件接口提供了完全的灵活性,允许使用低成本COTS硬件进行快速原型设计,并且很容易在初始点实现之外进行扩展。作为唯一的第五代航空电子架构,纳入霍尼韦尔IMA的概念非常适合成为星座项目下一代乘员探索飞行器的骨干。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Next generation space avionics: a highly reliable layered system implementation
Advances in electronics over the past decade have produced major improvements in the power and flexibility of personal computer systems. Unfortunately current avionics systems for space applications typically have not leveraged these COTS advantages. Recently, there has been a trend toward utilization of commercial bus interconnects, primarily VME and PCI. These parallel interconnects have the disadvantage that a single failure can disable an entire string of the redundancy. Honeywell has developed a patent pending architecture for an avionics system that combines the high reliability of previous serial systems with the flexibility and openness of direct COTS bus interface. A decade ago, the state of the art for avionics systems made a step change from the PAVE PILLAR systems of the 1980's to the integrated modular avionics (IMA) used in the Boeing 777. This next generation avionics architecture is not based upon traditional Byzantine redundancy structures, but on a truth based scheme where each element knows when an internal failure occurs and removes itself from the system. IMA utilizes a lock step microprocessor design that communicates to a COTS backplane for input/output, and to a virtual backplane/sup /spl trade// (a reliable, high-speed serial bus such as 1394 or AFDX) for intra-system communication. The system functions are implemented using an ARINC-653 time and space partitioned operating system. The entire system provides the simplicity of a simplex system, implements the highest level of reliability provides complete flexibility to reconfigure both software applications and hardware interfaces, allows for rapid prototyping using low-cost COTS hardware, and is easily expandable beyond the initial point implementation. As the only 5th generation avionics architecture, the concepts incorporated into Honeywell's IMA are ideally suited to be the backbone of the next generation Crew Exploration Vehicle for Project Constellation.
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