综合核心处理机架构分析与设计  

Analysis and Design of Integrated Core Processor Architecture

作　　者：汤艳飞 张伟栋[1] TANG Yan-fei;ZHANG Wei-dong(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》2020年第4期101-105,共5页Aeronautical Computing Technique

基　　金：航空科学基金项目资助(2016ZC31005)。

摘　　要：航空电子系统技术发展至今,经历了分立式、联合式、综合化和先进综合化4个阶段。介绍了先进战斗机F-35的综合模块化航电系统,从综合核心处理机的系统需求出发,给出了其系统结构,以及ASAAC标准对核心处理机中功能模块的要求,分析了系统架构设计要求,提出了系统设计技术,总结出具有通用化、综合化的通用处理模块单元,给出了综合核心处理机架构设计方法。The development of avionics system technology has gone through four stages:vertical,joint,integrated and advanced integrated.Firstly,this paper introduces the integrated modular avionics system of F-35.Starting from the system requirements of the integrated core processor,the system structure of the integrated core processor and the requirements of ASAAC standard for the functional modules in the core processor are given.The system architecture design requirements of the integrated core processor are proposed,the system design technology is proposed,the general processing module unit with generalization and integration is summarized,and the architecture design method of the integrated core processor is given.

关 键 词：航电系统 综合模块化 ASAAC 通用处理 

分 类 号：V243[航空宇航科学与技术—飞行器设计]