固体火箭发动机试验综合软件系统设计  

Integral Software System for Solid Motor Test

作　　者：陈广南[1] 郭健[1] 张为华 卞晓章 周克 焦继革 

机构地区：[1]国防科技大学航天与材料工程学院,湖南长沙410073 [2]江河化工厂,湖北远安444200

出　　处：《航空动力学报》2001年第1期49-51,共3页Journal of Aerospace Power

摘　　要：介绍一种固体火箭发动机试验用综合软件系统。该软件系统除具有标定、数据采集、试验数据分析处理功能外 ,还具有固体火箭发动机性能预估、参数辨识 ,以及试验数据库管理功能。该系统能自动快捷地分析处理各类试验数据 ,有效提高了试验效率。A multifunctional software system for solid motor test is introduced,which consists of independent modules with shared data bases.This software system has functions such as calibration,experimental data acquisition,motor performance prediction,and parameter identification.The data base is used as data exchanging center between code modules,and makes whole package of different modules acting as an integrated program,and so it is convenient for function extending.This software can process automatically various tests,such as tests of real motor,standard experimental motor,thrust termination motor and igniter.The information about design parameters,results of theoretic analysis and experimental records can be managed comprehensively with the help of data base technique and will improve the efficiency for solid motor test.

关 键 词：固体推进剂火箭发动机 数据采集 试验 计算机软件 参数辨识 

分 类 号：V435.6[航空宇航科学与技术—航空宇航推进理论与工程]