方位误差对自旋导弹导引性能的影响  

Effect of Direction Error on Guidance Performance of Spinning Missiles

作　　者：王宗义[1] 

机构地区：[1]哈尔滨工程大学自动化学院,黑龙江哈尔滨150001

出　　处：《弹箭与制导学报》2003年第1期5-8,共4页Journal of Projectiles,Rockets,Missiles and Guidance

摘　　要：方位误差是自旋导弹自动导引过程中较特殊的问题。文中对方位误差对自旋导弹导引性能的影响进行了理论研究和仿真分析,得出了方位误差对系统稳定性影响的公式,给出了方位误差应限定的范围。Direction error is one of the special problems during the guidance of spinning missiles. In this paper a theory and simulation analysis was made on the effect of direction error on the guidance performance of spinning missiles. The formula about the effect of direction error on the stability of guidance loop and the limit range of direction error was given.

关 键 词：方位误差 自旋导弹 模型 导引过程仿真 自动导引过程 导引回路 稳定性 

分 类 号：TJ765.33[兵器科学与技术—武器系统与运用工程] TJ765.22