复杂航空电子系统软件产品线的实现

F. Dordowsky, R. Bridges, Holger Tschöpe
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引用次数: 26

摘要

越来越多的客户和他们对NH90的特定应用领域导致了越来越多的功能不同的直升机改型。为了应对大量的软件变体,NH90软件团队开发了基于软件产品线(SPL)原则的软件体系结构。军用航空电子系统受到许多因素的制约,这些因素限制了SPL实施技术的选择,最突出的是对产品、工具和过程的严格安全规定。该领域的许多SPL计划还面临着已经存在的设计以及大型代码库。NH90软件团队已经定义了SPL应该遵循的体系结构原则,以便满足这些限制。NH90 SPL试图遵循这些原则。它的实现依赖于三个支柱:嵌入式实时框架、广泛的代码生成和一组设计和编码模式。本文描述了这些决定NH90 SPL体系结构的原则、用于代码生成的技术,以及设计和编码模式的选择,作为航空电子领域内实际项目中的软件产品线实现示例。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Implementing a Software Product Line for a Complex Avionics System
The growing number of customers and their specific application domains for the NH90 has led to an increasing number of functionally different helicopter variants. In order to cope with the high number of software variants, the NH90 software team has developed a software architecture that is based on Software Product Line (SPL) principles. Military avionics systems are constrained by many factors that limit the selection of SPL implementation technologies, most prominently the strict safety regulations on product, tools and processes. Many SPL initiatives in this domain also face an already existing design together with a large code base. The NH90 software team has defined architectural principles that an SPL should follow in order to meet theses restrictions. The NH90 SPL attempts to follow these principles. Its implementation relies on three pillars: an embedded real-time framework, extensive code generation and a set of design and coding patterns. This article describes these principles that determine the NH90 SPL architecture, the techniques used for code generation, and a selection of the design and coding patterns, as an example of a software product line implementation in a real project within the avionics domain.
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