摘要
目前飞机结构疲劳试验过程中,载荷设计存在一种基于C语言的遗存系统。该系统程序布局分散,操作过程僵化,数据断点较多,人机交互界面较复杂,从而导致试验准备工作的效率不高、周期较长、较难维护的问题。为了解决这些问题,本文采用构建一套基于Microservices的载荷设计系统的解决方案,使其具有"松耦合、高内聚"的软件架构特点,实现独立部署、重用性较高的柔性研发模式,从而提高试验的设计水平。
At present,in the process of fatigue test of aircraft structure,there exists a legacy system of load design based on C language.There are some problems in the system,such as scattered program layout,rigid operation process,more data breakpoints and complex man-machine interface,which lead to inefficient test preparation,long cycle and difficult maintenance.In order to solve these problems,a load design system based on Microservices is adopted in this paper,which has the characteristics of "loose coupling,high cohesion" software architecture,and achieves a flexible R&D mode with independent deployment and high reusability,so as to improve the design level of the test.
作者
刘思扬
Liu Siyang(Aircraft Strength Research Institute of China,Key Laboratory of Aeronautical Science and Technology for Static/Fatigue of Full-Scale Aircraft Structures,Xi’an Shaanxi 710065,China)
出处
《工程与试验》
2019年第3期108-110,共3页
Engineering and Test
关键词
微服务
载荷处理
飞机结构
疲劳试验
microservices
load processing
aircraft structural
fatigue test
