Model-based adaptation of flight-critical systems

S. Ray, G. Karsai, K. Mcneill
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引用次数: 6

Abstract

In this paper we describe our experience applying the Producible Adaptive Model-based Software (PAMS) technology to the development of safety critical flight control software. PAMS is based on the state of the art Model Integrated Computing (MIC) environment from Vanderbilt University and represents a highly evolvable model-based software development methodology and tool suite that is revolutionary in its ability to address software adaptation. In particular, PAMS is an adaptation framework that introduces support for model transformations, co-evolution of models and modeling tools, and self-adaptation of systems. Analogous to delayed binding in compiler technology, PAMS enables binding software updates statically at design-time, on a configuration basis at load-time, and dynamically at run-time. The focus of this paper will be the application of PAMS to designtime evolution.
基于模型的飞行关键系统自适应
本文介绍了我们将基于可生产自适应模型的软件(PAMS)技术应用于安全关键型飞控软件开发的经验。PAMS基于范德比尔特大学最先进的模型集成计算(MIC)环境,代表了一种高度可进化的基于模型的软件开发方法和工具套件,在解决软件适应性方面具有革命性的能力。特别是,PAMS是一个适应框架,它引入了对模型转换、模型和建模工具的共同进化以及系统自适应的支持。与编译器技术中的延迟绑定类似,PAMS支持在设计时静态绑定软件更新,在加载时基于配置绑定软件更新,在运行时动态绑定软件更新。本文将重点讨论PAMS在设计时演化中的应用。
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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