火箭炮随动系统静态精度测量方法研究  

Research on Measurement Methods for Static Accuracy of Rocket Launcher Follower System

作　　者：刘威 LIU Wei(No.710 R&D Institute,CSIC,Yichang 443003,Hubei,China)

机构地区：[1]中国船舶重工集团有限公司第七一〇研究所,湖北宜昌443003

出　　处：《工程与试验》2025年第1期6-8,37,共4页Engineering and Test

摘　　要：火箭炮随动系统静态精度是影响火箭炮武器系统发射密集度的重要因素。通过某火箭炮随动系统静态精度3种测量方法分析,建立3种测量方法数学模型,并开展了测量精度研究。对比分析结果表明,双经纬仪测试法是3种方法中的最优方法,可用于验证角度传感器的准确性。The static accuracy of rocket launcher follower system is an important factor affecting the launch density of rocket weapon systems.According to the analysis of three measurement methods for the static accuracy of a rocket launcher follower system,the mathematical models for the three measurement methods are established,and the measurement accuracy is studied.The comparative analysis results show that the double theodolite test method is the optimal method among the three methods,which can be used to verify the accuracy of angle sensors.

关 键 词：火箭炮 双经纬仪测试法 静态精度 数学模型 

分 类 号：TJ306[兵器科学与技术—火炮、自动武器与弹药工程]