基于均匀设计的空地导弹火控精度试验技术研究  

Accuracy Test Technologies for Air-to-ground Missile Fire Control System Based on Uniform Design Method

作　　者：陈敬志[1] CHEN Jingzhi(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》2019年第5期77-80,共4页Journal of Projectiles,Rockets,Missiles and Guidance

基　　金：航空科学基金(20171330001)资助。

摘　　要：为了降低试验次数,保证试验点在试验范围内均衡分散,采用一种机载空地导弹火控系统精度试验技术,以均匀设计理论为基础,选取相对高度、目标速度等可控因素来设计精度试验。通过均匀设计仿真,得到试验剖面仿真结果,并安排动态精度试验。结果表明,该方法可降低试验次数,保证试验状态均衡分散,提高试验效率,对导弹火控系统试验设计有较高的应用价值。Aimed at reduce the number of test times, and ensure that the testing points distribute uniformly among the test area. The accuracy test technologies for airborne air-to-ground missile fire control system are used. On the based of the uniform design theory, we select controllable factors including relative altitude, target velocity to design accuracy test. Using the uniform designing simulation, the test profile simulation result was given, and arrange dynamic accuracy test. According to the results, this method can reduce the test times, ensure that the testing points distribute uniformly, and improve the test efficiency,it has a higher application worth for missile fire control system test design.

关 键 词：空地导弹 火控系统 精度试验 均匀设计 

分 类 号：V217[航空宇航科学与技术—航空宇航推进理论与工程]