An adaptable software architecture for integrated avionics

Will Tracz, L. Coglianese
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引用次数: 15

Abstract

This paper outlines the process, challenges, and preliminary results of developing a software architecture for navigation, guidance and flight director. These critical real-time functions were chosen because they represent the essential features of integrated avionics systems. The authors propose that adaptable software architectures coupled with parameterized components, tools, and processes can greatly improve the quality and maintainability of flight systems. The results discussed in this paper are based on the results of the first of four year's work performed at IBM's Federal System Company, Owego, NY as part of the Defense Advanced Projects Research Agency's (DARPA) Domain-Specific Software Architectures (DSSA) program. The goal of this research is to engineer an architecture and environment that enables the rapid development of avionics requirements and software. In addition, this research focuses on making architectures extendible to permit the addition of evolutionary hardware and software technologies.<>
一种集成航空电子设备的适应性软件体系结构
本文概述了开发导航、制导和飞行指挥软件体系结构的过程、挑战和初步结果。之所以选择这些关键的实时功能,是因为它们代表了综合航空电子系统的基本特征。作者提出,与参数化组件、工具和过程相结合的适应性软件体系结构可以极大地提高飞行系统的质量和可维护性。本文中讨论的结果是基于IBM的联邦系统公司,纽约州Owego,作为国防高级项目研究局(DARPA)领域特定软件体系结构(DSSA)计划的一部分,进行的四年工作的第一阶段的结果。这项研究的目标是设计一个架构和环境,使航空电子需求和软件的快速发展。此外,本研究着重于使体系结构具有可扩展性,以允许添加进化的硬件和软件技术。
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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