航空电子系统

一种改善航空电子系统电磁兼容性的有效方法

An Effective Method to Improve the RF Signal Compatibility of Avionic Systems

基于Petri网的综合航空电子系统性能分析

Petri Nets-based Performance Analysis of Integrated Avionics System

飞行管理系统（FlightManagementSystem）是民用飞机航空电子系统的核心系统。

Flight Management System ( FMS ) is the kernel system of civil avionics .

C研究所航空电子系统集成业务发展战略研究

The Research of C Institute for Development Strategy of Avionics System Integration Business

基于UML语言的航空电子系统快速原型设计

Rapid Prototype Design Method in Avionics System Based on UML

航空电子系统设计中FPGA技术的应用

Application of FPGA Technology in Avionics System Design

为了满足新一代航空电子系统高度综合化、模块化的要求，在高安全实时操作系统中引入了分区（Partition）的概念。

In orde to satisfy Integrated Modular Avionics , partition is issued in high safe real-time o / s.

简要介绍了PI总线的特点及其在航空电子系统中的应用；

This article discusses in brief the PI Bus characteristic and its application in avionics system .

航空电子系统SCI网络可靠性建模研究

Research on the reliability model of avionics SCI network

航空电子系统FC交换式网络的可靠性研究

Study on Reliability of FC Fabric in Avionic

本文内容来源于实际工程项目，属于FPGA技术在航空电子系统中的应用范畴。

This thesis originates from a practical engineering project , which belongs to the FPGA technology application in the aviation electron system category .

针对航空电子系统中故障诊断的问题，提出一种将神经网络中的BP算法与模糊逻辑系统相结合、自动产生并自动修正模糊规则的自适应的模糊逻辑推理机。

An adaptive fuzzy logic inference machine combined fuzzy logic with BP neural network and applied in the aviation electrommunication fault diagnosis system is introduced .

光纤通道（FC）技术是未来航空电子系统互连首选协议。

Fibre Channel ( FC ) is the primary candidate protocol for the future avionics system interconnection .

而BIT（Built-inTest，简称机内测试）技术在航空电子系统中的应用解决了上述难题，并成为提高其测试性、维修性有效途径。

But BIT ( Built-in Test , in abbreviation machine tested ) the technology to solve the above difficult problem in the aviation electron system application , and became enhances its test , the Maintainability effective way .

从航空电子系统的需求出发，对可扩展一致性接口（SCI）网络的拓扑结构进行了最短路径（跳数）研究。

For the need of the avionics , the shortest average paths of some scalable coherent interface ( SCI ) network structures are studied in this paper .

美军F-22的先进航空电子系统

The Advanced Avionics System of F-22

设计了某型飞机航空电子系统的VXI检测平台并对其进行软件编程。

A VIX detection platform and the corresponding software were designed for the avionic system of a certain type of aircraft .

FC交换式网络可靠性的研究对于航空电子系统设计阶段的容错设计和拓扑选择都将起到指导作用。

The study on reliability of fabric topologies of FC has a directive effect on both fault tolerance design and topology selection in the phase of avionics system design .

基于VME总线的ARM7主控通信模块是为满足航空电子系统技术发展的需要而研制设计的，是某航电分系统的控制、处理、通信的核心。

The ARM7 control and communication module based on VME-bus is designed to meet the need of new avionics system development .

基于AADL的航空电子系统安全性分析

Security Analysis of Avionics Systems Based on AADL

对于采用FC（光纤通道）网络的航空电子系统，从FC的基本模型出发，给出了三种具有容错能力的常用拓扑结构：双环结构、双交换机结构和交换机仲裁环组合结构。

To the avionics of fibre channel ( FC ) interconnection , based on the basic FC interconnection model , three fault tolerance topologies are given : loop-to-loop , switch-to-switch and switch-loop .

航空电子系统MIL-STD-1553通信网络接口验证测试

Avionics System MIL-STD-1553 Communication Network Interface Verification Test

对于采用光纤通道（FC）互连的航空电子系统，从FC的基本模型出发，给出了由多个FC交换机组成的FC交换式网络的通信模型；

To avionics of fibre channel ( FC ) interconnection , communication model of fabric that is made up of one or more FC switches is given based on basic FC interconnection model .

LRM模块是航空电子系统结构设计的新方向。

LRM modular is a new design method of avionics system and it is the trend of avionics system package .

根据国内外电子行业及微电子IC设计行业的发展现状和军用航空电子系统的特殊性，本文提出了SOC设计构想，详细讨论了SOC设计过程。

From the development status of electronics industry and microelectronics IC design industry and the particularity of military avionics system , this paper puts forward SOC design concept , then it discusses the SOC design 's procedure in details .

MIL-STD-1553B总线在航空电子系统中应用广泛，总线监控系统可以实现总线消息实时监控。

MIL-STD-1553B bus has a wide application in airborne avionics systems , the bus monitoring systems can realize the real-time bus information monitoring .

阐述效能的基本定义及其分类，根据效能准则依照Delphi法建立了综合航空电子系统效能评估的指标体系，将系统效能分解为各个底层指标。

The basic definition and classification are expounded . Based on effectiveness rules , the index system to evaluate the effectiveness of integrated avionics system is established according to Delphi method , and the system effectiveness is converted into basic indexes .

着重探讨和分析了国外最新一代军、民用飞机上使用的航空电子系统体系结构&综合模块化航空电子系统（IMA）。

The latest generation of avionics architecture , namely Integrated Modular Architecture ( IMA ) used in the foreign military and civil aircraft is especially discussed and analyzed in this paper .

总之，FC-LP通信协议具有高可靠、高效率、低延时的特点，能满足强时性和高可靠性飞机航空电子系统通信需求。

FC-LP has characteristics of high-reliability , high-efficiency and low-latency , and can satisfy communication requirements of strong-real-time and high-reliability avionics .

这些都对进一步研究实现TCAS与S模式应答机的综合化具有一定的参考与借鉴意义，也为航空电子系统的综合化设计与实现提供了一种解决思路。

The above could provide some reference for the further study and implementation of integraed TCAS and mode S transponder and supply one thought for design and implementation of integrated avionics system .