摘要
随着新一代飞机的快速发展,机载机电系统被赋予更多的功能,其交联的设备数量与种类不断增加,进而导致机电系统管理软件规模及复杂程度也越来越高。这对新一代机载机电系统软件设计及现有机电系统能力的扩展提出了新的挑战。以特定需求以及机载设备为基础设计的软件架构,其通用化、复用性低,导致软件的综合开发成本及周期居高不下。因此必须为未来机载机电管理系统的发展开发出一种先进的软件开发架构。基于此,提出了一种开放式架构软件开发及管理方法,并开展了相关研究,该方法能够有效提高软件开发效率,进一步实现软件标准化、可拓展化,提高软件复用性。
With the rapid development of the new generation of aircraft,the electromechanical system is given more functions,the number and types of devices cross-linked by electromechanical systems are increasing.This also leads to the increasing scale and complexity of the software,which poses new challenges to the software design of the new generation airborne electromechanical system and the expansion of the existing electromechanical system capabilities.Software architecture designed based on specific requirements and airborne equipment has low universality and reusability,resulting in high comprehensive development cost and cycle of software.Therefore,an advanced software development architecture must be developed for the development of airborne electromechanical management system in the future.In this paper,an open architecture software development and management method is proposed and related research is carried out,which can effectively improve the efficiency of software development,further realize software standardization and scalability,and improve software reusability.
作者
罗德杰
蔡明
郭鑫
Luo Dejie;Cai Ming;Guo Xin(Xi’an Aeronautics Computing Technique Research Institute,AVIC,Xi’an Shaanxi 710068,China;No.6 Military Representative Office of Air Force Equipment Department in Xi’an,Xi’an Shaanxi 710068,China)
出处
《山西电子技术》
2023年第6期87-89,共3页
Shanxi Electronic Technology
关键词
开放式
软件开发
复用性
open system architecture
software development
reusability