基于卫星定位的弹道修正弹控制参数解算方法  

A Method of Solving Control Parameter for Trajectory Correction Projectiles Based on Satellite Positioning

作　　者：李元[1] 王海川[1] 

机构地区：[1]江苏自动化研究所,江苏连云港222061

出　　处：《指挥控制与仿真》2015年第3期8-12,24,共6页Command Control & Simulation

摘　　要：介绍了近年来国外基于GPS定位的弹道修正弹发展情况,分析了一维、二维弹道修正弹的技术特点,结合工程应用分别提出了一维、二维弹道修正弹求取修正控制参数的策略和方法。射击试验和仿真实验结果表明该方法具有可行性和有效性。The paper introduces the recent development of foreign trajectory correction projectiles based on GPS, analyzes the technological features of 1D and 2D trajectory correction projectiles, and then, combined with the engineering applica- tion, puts forward the strategies and methods of solving correction parameter for 1D and 2D trajectory correction projectiles separately. The results of firing test and simulation show the feasibility and effectiveness of the methods.

关 键 词：弹道修正弹 卫星定位 修正参数解算 

分 类 号：E911[军事] TJ012[兵器科学与技术—兵器发射理论与技术]