首页 | 官方网站   微博 | 高级检索  
     

随机风对比例导引制导精度影响研究
引用本文:徐平,王伟,林德福.随机风对比例导引制导精度影响研究[J].兵工学报,2011,32(12):1481-1485.
作者姓名:徐平  王伟  林德福
作者单位:(北京理工大学 宇航学院, 北京 100081)
摘    要:分析了随机风对弹体产生的干扰作用,建立了引入随机风干扰的比例导引制导系统模型,并对模型进行了适当简化,运用伴随法得到了简化后比例导引制导系统的解析解,系统解析解显示随机风造成的脱靶量与随机风的标准差成正比,并随着制导时间的增加趋于一个常值.最后详细分析了未经简化的比例导引制导系统,仿真结果表明:增大比例导引系数有利于抑...

关 键 词:飞行器控制、导航技术  随机风  比例导引  制导精度  伴随法

Study on Effect of Random Wind on Proportional Navigation Guidance Precision
XU Ping , WANG Wei , LIN De-fu.Study on Effect of Random Wind on Proportional Navigation Guidance Precision[J].Acta Armamentarii,2011,32(12):1481-1485.
Authors:XU Ping  WANG Wei  LIN De-fu
Affiliation:(School of Aerospace,Beijing Institute of Technology, Beijing 100081, China)
Abstract:The disturbance effect of random wind on missile is analyzed.A proportional navigation guidance system model with random wind disturbance is built and then simplified.The analytic solution is obtained by using adjoint method.Finally,the original proportional navigation guidance system is analyzed in detail.The analytic solution of the simplified model demonstrates that the miss distance caused by random wind varies as the standard deviation of random wind velocity and trends towards a constant value with the guidance time increase.Simulation results show that the increase of proportion navigation coefficient is beneficial to inhibit the harmful influence of random wind on the guidance precision,either improving autopilot response or reducing the damping coefficient have the same effect.
Keywords:control and navigation technology of aerocraft  random wind  proportional navigation  guidance precision  adjoint method
本文献已被 CNKI 万方数据 等数据库收录!
点击此处可从《兵工学报》浏览原始摘要信息
点击此处可从《兵工学报》下载全文
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-23

京公网安备 11010802026262号