作战支援类飞机航空电子任务系统总体结构研究
收稿日期: 2013-11-20
修回日期: 2014-01-06
网络出版日期: 2014-01-13
Research on General Architecture of Avionics Mission System for Operational Support Aircraft
Received date: 2013-11-20
Revised date: 2014-01-06
Online published: 2014-01-13
在研究了几种典型的航空电子系统结构特点的基础上，分析了作战支援类飞机航空电子系统的特点和适宜的结构形式，指出了军用航空电子系统总体结构设计中容易出现的主要问题和应当遵循的设计准则。应用最新的分布式模块化电子（DME）系统技术和体系结构设计方法，建立了面向任务与操作者的作战支援类飞机航空电子系统总体结构框架。最后，指出了采用分布式模块化系统设计技术优化航空电子系统内部功能，以及采用异型智能化结构部件技术实现系统与飞机气动外形、结构总体的一体化，是军用飞机航空电子系统的未来发展趋势。
关键词： 航空电子技术; 综合模块化航空电子系统; 分布式综合模块化航空电子系统; 分布式模块化电子系统; 航空电子系统结构; 体系结构框架; 作战支援类飞机
屈也频 . 作战支援类飞机航空电子任务系统总体结构研究[J]. 航空学报, 2014 , 35(8) : 2307 -2318 . DOI: 10.7527/S1000-6893.2013.0513
On the basis of a discussion of a few classical avionics architecture types, the major problems in military avionics system structure planning are analyzed, and the characteristics of avionics and mission system for operational support aircraft and its design principles are enumerated. With the latest distributed modular electronics (DME) system technology and architecture framework design method, a tasks and users oriented military avionics architecture of the operational supporting aircraft is constructed. The paper concludes that this is one of the development trends of operational avionics in the future, which utilizes a distributed modular system design scheme to optimize avionics inner functions, and introduces intelligent abnormal structural component technology to integrate military avionics with aerodynamic and general structure design.
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