高空舱飞行环境模拟控制系统通用软件模块设计  

General software module design for flight environment simulation control system of the simulated altitude test facility

作　　者：董满收 黄凯 邝文 陈小丽 DONG Man-shou;HUANG Kai;KUANG Wen;CHEN Xiao-li(AECC Sichuan Gas Turbine Establishment,Mianyang 621700,China)

机构地区：[1]中国航发四川燃气涡轮研究院,四川绵阳621700

出　　处：《燃气涡轮试验与研究》2021年第6期22-25,共4页Gas Turbine Experiment and Research

摘　　要：为提高高空舱飞行环境模拟控制系统控制程序的设计效率,开发了一套通用软件框架和模块。该套模块使用结构化文本语言编写,具有高内聚、低耦合的特点,方便用户反复调用,具体包括信号滤波与报警、设定值输入、阀门自动控制以及一些特殊功能模块等。实际使用表明,该套通用软件框架和模块可大幅缩减设计控制程序所需时间,极大地提高编程效率,为高空舱飞行环境模拟控制系统的调试、运行和维护提供了有力帮助。A set of standard soft module and framework was designed to improve design efficiency for con⁃trol program of flight environment simulation control system of the simulated altitude test facility.This set of modules was written in Structured Text,with high cohesion and low coupling qualities.Customers could call these modules conveniently and repeatedly.These modules included signal filter and alarm,set-point in⁃put,valve automatic control,special function modules and so on.Practice shows that,by using these mature software modules,customers can significantly reduce the time required to design control program,greatly improve the quality and efficiency of programming,which provide powerful help for debugging,operating and maintenance of flight environment simulation control system.

关 键 词：航空发动机 高空舱 飞行环境模拟 控制系统 模块化设计 控制程序 

分 类 号：V263.47[航空宇航科学与技术—航空宇航制造工程]