一种基于一体化设计的通用飞机机载电子系统架构  

A Airborne System Architecture for General Aircraft Based on Integration Design

作　　者：刘文学[1] 孔德岐[1] 田莉蓉[1] 吕亚方 米耘锋 LIU Wen xue;KONG De qi;TIAN Li rong;LV Ya fang;MI Yun feng(Xi′an Aeronautics Computing Technique Research Institute,AVIC,Xi′an 710068,China)

机构地区：[1]航空工业西安航空计算技术研究所,陕西西安710068

出　　处：《航空计算技术》2018年第5期134-138,142,共6页Aeronautical Computing Technique

基　　金：航空科学基金项目资助(2016ZC31005)

摘　　要：机载电子系统是支持通用飞机实现高效操作、高安全性、低成本、自主飞行等先进能力的关键功能单元,是体现通用飞机技术发展水平的一个重要标志。目前国内面向通用飞机机载电子系统和国外差距较大,针对国内通用飞机机载电子系统所存在的问题,结合未来的技术发展,提出一种基于一体化设计的通用飞机机载电子系统架构,对架构的逻辑和物理实现进行了描述,经过实际的原理样机验证,架构具有较高的实际应用价值。Airborne electronic systems a key unit of general aircraft for support efficient operation,safety ,and low cost.It′s a sign for general aviation technology development.At present,the gap between domestic avionics system and foreign aircraft is quite large.Aiming at the problems of airborne electronic system in China ,and future development,a general aircraft airborne electronic system architecture based on integrated design is proposed.The architecture logic and physical implementation are designed,the results show that the prototype has high practical value.

关 键 词：通用飞机 机载电子系统 逻辑架构 物理架构 

分 类 号：V243[航空宇航科学与技术—飞行器设计]