一种导弹发射飞行试验系统设计与研究  

The Test System Design and Research of the Ground Launching Missile Flight

作　　者：韩颖超[1,2] 孟维晓[1] 赵琦[2] 毛友泽[2] 杜广宇 李雪飞[2] HAN Yingchao;MENG Weixiao;ZHAO Qi;MAO Youze;DU Guangyu;LI Xuefei(Harbin Institute of Technology,Harbin 150001,China;Beijing Institute of Electronic Engineering,Beijing 100854,China)

机构地区：[1]哈尔滨工业大学,哈尔滨150001 [2]北京电子工程总体研究所,北京100854

出　　处：《火力与指挥控制》2022年第7期165-167,173,共4页Fire Control & Command Control

摘　　要：设计了一种地面发射制导弹飞行试验系统,分析了试验系统的技术途径、设计原理、主要组成及连接关系。解决了制导信息传递等技术难题,对试验系统精度闭合所需的要素及参数进行分析及仿真计算,对精度链传递、系统截获精度的关键要素进行了探讨,为地面发射导弹攻击空中目标提供了一种完整、可靠、验证有效的技术选择。The flight test system of the ground launching guided missile is designed.The technical approach,design principle,the main composition and their connection relation of the text system are analyzed.The guidance information transfer and other technical problems are solved,the needed elements and parameters for testing the accuracy closure of system are analyzed and simulatively calculated,the key elements of accuracy chain transfer and system interception accuracy are explored.A complete,reliable and valid varification design mrans are provided for the ground launching missile to attack the targets in the air.

关 键 词：地面制导弹 试验系统 系统闭合分析 空中目标 

分 类 号：TJ760.1[兵器科学与技术—武器系统与运用工程]