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摘要:
Aviation electronics (avionics) are sophisticated and distributed systems aboard an airplane. The complexity of these systems is constantly growing as an increasing amount of functionalities is realized in software. Thanks to the performance increase, a hardware unit must no longer be dedicated to a single system function. Multicore processors for example facilitate this trend as they are offering an increased system performance in a small power envelope. In avionics, several system functions could now be integrated on a single hardware unit, if all safety requirements are still satisfied. This approach allows for further optimizations of the system architecture and substantial reductions of the space, weight and power (SWaP) footprint, and thus increases the transportation capacity. However, the complexity found in current safety-critical systems requires an automated software deployment process in order to tap this potential for further SWaP reductions. This article used a realistic flight control system as an example to present a new model-based methodology to automate the software deployment process. This methodology is based on the correctness-by-construction principle and is implemented as part of a systems engineering toolset. Furthermore, metrics and optimization criteria are presented which further help in the automatic assessment and refinement of a generated deployment. A discussion regarding a tighter integration of this approach in the entire avionics systems engineering workflow concludes this article.
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篇名 Deploying Safety-Critical Applications on Complex Avionics Hardware Architectures
来源期刊 软件工程与应用(英文) 学科 工学
关键词 AVIONICS SYSTEMS Engineering SOFTWARE DEPLOYMENT SOFTWARE ARCHITECTURE Safety-Critical SYSTEMS
年,卷(期) 2013,(5) 所属期刊栏目
研究方向 页码范围 229-235
页数 7页 分类号 TP39
字数 语种
DOI
五维指标
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研究主题发展历程
节点文献
AVIONICS
SYSTEMS
Engineering
SOFTWARE
DEPLOYMENT
SOFTWARE
ARCHITECTURE
Safety-Critical
SYSTEMS
研究起点
研究来源
研究分支
研究去脉
引文网络交叉学科
相关学者/机构
期刊影响力
软件工程与应用(英文)
月刊
1945-3116
武汉市江夏区汤逊湖北路38号光谷总部空间
出版文献量(篇)
885
总下载数(次)
0
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0
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