首页 | 本学科首页   官方微博 | 高级检索  
     检索      

逐步回归法在反舰导弹火控建模中的应用
引用本文:李相民,张安,史建国.逐步回归法在反舰导弹火控建模中的应用[J].飞行力学,2003,21(4):65-68.
作者姓名:李相民  张安  史建国
作者单位:西北工业大学,605教研室,陕西,西安,710072
摘    要:用均匀试验设计方法布点,计算了反舰导弹的标准弹道,根据获得的弹道数据,用逐步回归分析方法建立了各种发射条件下预报弹道坐标的预报模型,该模型计算简单、精度高。此建模方法也可应用于其他领域。

关 键 词:逐步回归法  反舰导弹  火力控制  建模  均匀设计
文章编号:1002-0853(2003)04-0065-04
修稿时间:2002年11月29

Application of Stepwise Regression to Fire Modeling of an Anti-Ship Missile
LI Xiang-min,ZHANG An,SHI Jian-guo.Application of Stepwise Regression to Fire Modeling of an Anti-Ship Missile[J].Flight Dynamics,2003,21(4):65-68.
Authors:LI Xiang-min  ZHANG An  SHI Jian-guo
Abstract:The forecast of the end-point position for uniform experimental design is very important because it is the precondition to control the missile to hit the target. In this paper, the normal trajectories of the anti-ship missile are calculated with the use of uniform experimental design. Based on the trajectory data, the models to forecast the trajectory coordinates in various launching conditions are established by use of stepwise regression. The models are simple and high precision. This modeling technique can also be used in other fields.
Keywords:anti-ship missile  normal trajectory  forecast model  uniform design  stepwise regression  
本文献已被 CNKI 维普 万方数据 等数据库收录!
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号