Introduction : a similar network now popular war game battle tanks , the player calculated wind direction , launching point for ballistic impact , quite challenging , use your brains 一款类似如今热门网络对战游戏的坦克作战，玩家需要计算风向发射角度对于弹道的影响，颇具挑战性，开动你的脑筋！
At the same time the author used the means of statistics to find out the various degrees of influence from the different initiatory kinematics parameters and gives the primary and secondary order 同时根据正交试验的思想，分析了不同的初始运动学参数对于下沉弹道的影响程度，并且给出了这些因素的主次顺序。
First , this paper will introduce the random factors affecting the trajectory , kallman filtering method , and the mathematic model that is used to process radar data processing and extrapolate the trajectory 首先介绍了影响弹道的随机因素、卡尔曼滤波方法、侦察及校射模式下雷达数据处理及弹道外推的数学模型。
Based on a ballistic model , the relationship between corrected distance and the magnitude of impulse control force is , and relationship between the miss distance and the class number of impulse control force analyzed 从弹道的角度建立弹道模型，分析了修正距离与脉冲控制力大小的关系以及脉冲发动机级数与脱靶量之间的关系。
Two new algorithms , adaptive model and adaptive interacting multiple model , are presented in this paper with respect to the maneuvering trajectory characteristics of anti - ship cruisle missiles 针对比例制导的飞航式反舰导弹弹道的特点和机动特征，提出了跟踪此类目标的两种新算法? ?基于自适应模型的算法和基于自适应交互多模型的算法。
This thesis uses fuzzy changing the gain proportion guidance to control the yaw angle v and the pitching angle , and to realize following track , with the predetermined track , which had been designed by hierarchical track planning with voronoi diagram 本文在利用voronoi图的分层航迹规划,规划出预定航迹,并利用模糊变增益比例制导律控制导弹的偏角v和弹道的倾角,实现航迹跟踪。
Then the author optimize the initiatory kinematics parameters of the segregator of the submarine launched missile carrier by the way of monte carlo and simplex . confirming the limit scope of the segregator of the submarine launched missile carrier when sinking 然后利用蒙特卡罗法和复合形方法相结合的优化方法进行了分离体初始运动学参数的优化设计，同时对分离体下沉弹道的各项指标进行了优化计算。
Integrated design of rocket - ramjet is investigated systematically in this paper . based on step optimization pattern , proper matching for missile and engine is solved satisfactorily . also the relationship between guidance system and optimal trajectory is settled 本文系统地研究了整体式冲压发动机导弹一体化设计的问题，依据分步优化模式，解决了弹体与发动机的合理匹配、控制系统与最优弹道的关系问题。
The improvement to internal ballistic calculation precision of solid rocket motor ( srm ) is important to capture target of missile . and to accomplish it ' s task . calculation of burning surface of propellant grain is essential to interinal ballistic performance calculation 提高固体火箭发动机内弹道的计算精度对导弹准确捕获目标、完成任务有着重要的作用，而发动机工作时瞬态燃面计算是内弹道性能计算的基础。
Later the author computes the underwater trajectory of the segregator of the submarine launched missile carrier , then discusses the influence to the underwater trajectory from the hydrodynamics parameters , collectivity parameters and the initiatory kinematics parameters 而后根据初始运动学参数，计算了运载器分离体的下沉弹道，并且分别讨论了分离体的总体参数、流体动力学参数和初始运动学参数对下沉弹道的影响。
