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追踪法推广的数学建模与仿真
引用本文:强胜,龙汉,申镇,易东云.追踪法推广的数学建模与仿真[J].兵工学报,2009,30(1):56-62.
作者姓名:强胜  龙汉  申镇  易东云
作者单位:国防科学技术大学,理学院,湖南,长沙,410073;国防科学技术大学,理学院,湖南,长沙,410073;国防科学技术大学,理学院,湖南,长沙,410073;国防科学技术大学,理学院,湖南,长沙,410073
摘    要:本文首先引入侧面拦截,扩大对追踪法的讨论;并从理论上给出了追踪法对弹道影响的分析证明;其次结合推广的比例导引法,构建了三维立体组合导引法,使导引方案更加灵活、有效。最后对拦截过程进行了相应的仿真,实验结果说明此方法形式简单、方便,具有实用价值。

关 键 词:飞行器控制、导航技术  追踪法  推广的比例导引法  复合导引法  过载  动能拦截器

Generalized Mathematical Modelings and Simulations of Pursuit Guidance Method
QIANG Sheng,LONG Han,SHEN Zhen,YI Dong-yun.Generalized Mathematical Modelings and Simulations of Pursuit Guidance Method[J].Acta Armamentarii,2009,30(1):56-62.
Authors:QIANG Sheng  LONG Han  SHEN Zhen  YI Dong-yun
Affiliation:School of Science, National University of Defense Technology, Changsha 410073,Hunan, China
Abstract:The lateral intercept was proposed to extend a discussion on a pursuit navigation method;the analysis and proof of influence of the pursuit navigation method on the trajectory were theoretically given;3D solid combined navigation method was established by the generalized proportional navigation method and the pursuit navigation one to make the navigation scheme more flexible and effective.The intercept process was simulated by the combined navigation method.The simulated results show that the method is simp...
Keywords:control and navigation technology of aerocraft  pursuer guidance  generalized proportional navigation trajectory  combined navigation guidance  overload  kinetic kill vehicle  
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