This paper takes the tactical missile command and control system as the background , and studies the network architecture of command and control system 本文以战术导弹指挥控制系统为应用背景,对适合于指挥控制系统的网络体系结构进行研究。
Based on the small tactical missile system design , an engineering method for ram - air servo system dynamic accuracy analysis and verifying unit design is put forward 摘要从小型战术导弹总体设计的角度提出了一种继电控制冲压式伺服系统的动态精度和校正装置的工程分析和设计方法。
The judging condition is proposed concerning whether the missile will collides with launch device in launch process . at last , digital simulation system is developed to simulation the process of launch 建立了与以上发射动力学模型相应的仿真模型，并对仿真结果进行了分析，所得结论对战术导弹发射系统的设计具有一定的参考价值。
Based on existing results , this dissertation goes deep into the problem of the optimal allocation of conventional tactical missiles to targets , and the theory and the methods of optimal allocation of weapon systems to targets are consummated and developed 本文在现有成果的基础上，重点研究了常规战术导弹对目标打击的最优分配问题，完善和发展了武器系统对目标的优化分配理论与方法
3 using game theory and the three different criterions , the author investigates optimal allocation of tactical missiles between a primary target and a secondary target under the condition that the primary target is defended by the secondary target ( the defender can use either " normal " defensive mode or " cautious " defensive mode ) , presents the optimal attacking policy of the attacker and the optimal defensive policy of the defender 3利用对策理论和三个不同的准则，研究了一个主要目标在一个次要目标防卫下(次要目标采用“理智”防守模式) ，战术导弹对这两个目标打击的优化分配问题，给出了进攻方的最优进攻策略和防守方的最优防守策略。
The tactical missile seeker handover accuracy from midcourse to terminal guidance is researched . the small perturbation method is proposed to analyse error sensitivity of the seeker presetting parameters from error sources . firstly , the terminal guidance seeker presetting parameters are computed , based on the equations of a surface - to - air missile movement and a target movement . then the seeker presetting unaccuracy due to the command guidance radar measurement errors is also computed . it can be seen that the seeker presetting errors increase rapidly when the missile is close to the target , which leads to an important conclusion that the late seeker handover from midcourse to teminal guidance should be avoided 研究复合制导的战术导弹中末制导交班的导引头预定精度问题.提出用小扰动法分析导引头预定参数对误差源的误差敏感性关系.以中远程防空导弹为例，结合导弹运动方程组和目标运动模型，计算了中末制导交班的导引头预定参数，并计算了在制导站雷达测量误差下的末制导导引头预定参数的计算精度.可知，导引头定位参数的计算误差随着弹目距离的接近而显著增大，得到中末制导交班不能太晚的重要结论
The first chapter introduced the background of researching problem , presents a common process to resolve this kinds of problem and a common procedure for this method ; the second chapter briefly presented the basic thinking of equipment ils engineering and equipment technique support , discriminate between equipment ils and equipment technique support ; in chapter 3 , we studied the basic configuration of tactics ground - to - ground missile weapon system and the work content of technique support thoroughly , established the work - flow model of tactics ground - to - ground missile technique support in combat environment ; in chapter 4 , we mostly discussed the essence content of technique support evaluation , introduced the application of tradition static evaluating methods in the aspect of evaluating the capability of tactics ground - to - ground missile technique support , such as ahp , adc and synthesis fuzzy evaluation method , and put forward the method of computer dynamic simulating evaluation ; the fifth chapter particularly introduced the design thinking and realizing method of tactics ground - to - ground missile technique support evaluation by computer dynamic simulating , in the end , give an emulation realization instance 第二章对装备综合保障工程和装备技术保障基本思想进行了简要介绍，并对装备综合保障和技术保障进行了辨析。第三章对地地战术导弹武器的基本结构、技术保障工作内容进行了深入的分析研究，建立了地地战术导弹战时技术保障工作流程模型。第四章探讨了地地战术导弹技术保障评估的基本内容，详细介绍了诸如“ adc ” 、综合模糊评判等传统评估方法在地地战术导弹技术保障能力评估方面的应用，提出了计算机动态仿真评估的方法，并对地地战术导弹技术保障能力动态仿真评估进行了初步分析。
Carbon fiber reinforced plastics ( cfrp ) are widely used in aerospace , marine engineering ( such as all kinds of stratigic missile engine shells ) and various civil applications due to their exceptionally high specific strength and specific module , good high - temperature resistance , corrosion resistance and so on 碳纤维复合材料( carbonfiberreinforcedplastics , cfrp )具有比强度比模量高、耐高温抗腐蚀等优异性能,在航空航天、海洋军工(如各类战略战术导弹发动机壳体)与民用各领域具有重要和广泛的应用。
Abstract : the tactical missile seeker handover accuracy from midcourse to terminal guidance is researched . the small perturbation method is proposed to analyse error sensitivity of the seeker presetting parameters from error sources . firstly , the terminal guidance seeker presetting parameters are computed , based on the equations of a surface - to - air missile movement and a target movement . then the seeker presetting unaccuracy due to the command guidance radar measurement errors is also computed . it can be seen that the seeker presetting errors increase rapidly when the missile is close to the target , which leads to an important conclusion that the late seeker handover from midcourse to teminal guidance should be avoided 文摘:研究复合制导的战术导弹中末制导交班的导引头预定精度问题.提出用小扰动法分析导引头预定参数对误差源的误差敏感性关系.以中远程防空导弹为例，结合导弹运动方程组和目标运动模型，计算了中末制导交班的导引头预定参数，并计算了在制导站雷达测量误差下的末制导导引头预定参数的计算精度.可知，导引头定位参数的计算误差随着弹目距离的接近而显著增大，得到中末制导交班不能太晚的重要结论
With the development of science , new method is used in fighter plane and missile design , and new material is used in fighter plane and missile production , which make them have higher speed , higher maneuvering , smaller radar cross section and better jamming and anti - jamming ability . all these development is a big challenge to surface - to - air missile and makes the battlefield environment more complicated 随着科技的进步,新技术、新材料的大量应用,使作战飞机和战术导弹具有更快的飞行速度,更好的机动性能以及更小的雷达反射面积;同时,电子对抗技术的广泛使用,这些都给防空导弹带来了巨大挑战,使地面防空变得日趋复杂。
