航空电子设备
计算机科学
接口(物质)
图层(电子)
基于模型的设计
系统工程
软件工程
嵌入式系统
工程类
模拟
操作系统
化学
有机化学
气泡
最大气泡压力法
航空航天工程
作者
Julian Rhein,Viktor Sinitsyn,Florian Holzapfel
标识
DOI:10.1109/dasc55683.2022.9925749
摘要
Model-based software development using design tools such as MATLAB Simulink or Ansys SCADE Suite is usually centered around the specification, simulation and code generation of application layer functions. In this article, we propose a model-based avionics systems development approach that is focused on a broader view of the entire development life-cycle including interface definition, software integration, definition of the physical system architecture, test-rig design and wire-harness manufacturing. The approach is built around a central interface data model, which captures the application layer, transport layer and physical layer interfaces within a system architecture.
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