基于试验状态点矩阵的航电系统综合飞行试验设计  

Design of Integrated Flight Test for Avionics System Based on Test State Point Matrix

作　　者：李靖[1] 张兴国[1] 陈宇 LI Jing;ZHANG Xingguo;CHEN Yu(Chinese Flight Test Establishment,Xi’an 710089,China)

机构地区：[1]中国飞行试验研究院,西安710089

出　　处：《弹箭与制导学报》2020年第1期31-34,共4页Journal of Projectiles,Rockets,Missiles and Guidance

基　　金：总装和航空工业联合基金(614B05110302)资助。

摘　　要：随着装备技术的发展及实战化考核要求,航空装备飞行试验需要由单系统验证模式向综合运用条件下的系统综合验证模式转变。文中提出一种基于试验状态点矩阵的航电系统综合飞行试验设计方法,通过建立综合飞行试验约束条件,构建试验状态点的数学矩阵模型,实现航空电子系统综合验证任务辅助设计,有效提高试验任务执行效率及验证质量。With the development of avionics technology and the requirement of operational test,the flight test of avionics system needs to change from the single system verification mode to the system comprehensive verification mode under the condition of comprehensive operation.This paper presents a design method of integrated flight test for avionics system based on test state point matrix.By establishing the constraint conditions of integrated flight test and building the mathematical matrix model of test state point,the auxiliary design of avionics system integrated verification task can be realized,and the efficiency and quality of test can be effectively improved.

关 键 词：飞行试验 试验状态点 航空电子系统 

分 类 号：V217[航空宇航科学与技术—航空宇航推进理论与工程]