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[matlab] 弹道分析 DL : 1: 用matlab来编写的较复杂的程序，用来对导弹进行弹道分析-prepared using Matlab to the more complex procedures for the analysis of ballistic missile
Update : 2025-02-17 Size : 22kb Publisher : 向礼
[WEB Code] myjob DL : 1: 无控纵向导弹弹道计算。用四阶龙库、阿当姆斯积分法，运行时间短，效果好。-no control ballistic missile vertical calculation. With the four-Long, Adam Shams integral method, a short running time, the effect is good.
Update : 2025-02-17 Size : 2kb Publisher : 杨
[matlab] analysis_of_missile DL : 0: 采用Matlab编写的弹道分析算法，该算法可以模拟弹道飞行轨迹-Matlab preparation of the trajectory analysis algorithm, which can be simulated ballistic trajectory
Update : 2025-02-17 Size : 21kb Publisher : 杨向华
[File Format] OptimalReentry DL : 0: 导弹载入弹道的优化设计，主要是机动段的优化-ballistic missile printed in the optimization of the design, mainly the optimization of the mobile
Update : 2025-02-17 Size : 223kb Publisher : 何瑾
[transportation applications] Ballistics DL : 0: 在无投弹误差条件下，对制导炸弹的方案弹道方程组求解，求得炸弹落点C处的标准射程X（对应）以及主要的弹道参数-In the absence of bomb error conditions, the program of guided bombs ballistic Equations to obtain the bomb impact point C of the standard range of Office X (corresponding), as well as the main ballistic parameter
Update : 2025-02-17 Size : 356kb Publisher : duanlu
[Other] MissileGuidanceSimuDemo01 DL : 0: 本程序包为导弹追踪导引法的相对弹道簇图MATLAB仿真计算程序。关键词：导弹弹道追踪导引仿真 missile simulation guidance MATLAB -The package for the missile guidance law to track the relative ballistic cluster map MATLAB simulation program. Key words: ballistic missile tracking guided missile simulation guidance MATLAB simulation
Update : 2025-02-17 Size : 8kb Publisher : donotspam
[matlab] MATLABzaidandaofangzhendeyingyong DL : 0: 分析了弹道仿真数学模型的特点、并以滑翔增程弹为例，详细研究了在M文件、simulink工具箱以及两者交互使用环境下建立外弹道质心运动系统仿真模型的方法和优缺点。 -Analysis of the ballistic characteristics of the mathematical model simulation and Gliding Range shells as an example, a detailed study of the M paper, simulink toolbox and use both interactive environment to establish external ballistics center of mass movement system simulation model and the advantages and disadvantages.
Update : 2025-02-17 Size : 301kb Publisher : 陈大伟
[Other] Anapproacnforoptimizedtacticalballisticmissileobje DL : 1: 一篇用弹道系数识别弹道导弹目标的博士论文！这是非常难得的文章！-With a ballistic coefficient of a ballistic missile target recognition doctoral thesis! This is a very rare article!
Update : 2025-02-17 Size : 1.44mb Publisher : LIU weijian
[Graph Recognize] 1 DL : 0: matlab程序防御系统弹道导弹目标识别方面的matlab程序-matlab program of ballistic missile defense system target identification procedures matlab
Update : 2025-02-17 Size : 22kb Publisher : fangzi
[Graph Recognize] 476514886DOF DL : 0: matlab程序防御系统弹道导弹目标识别方面的matlab程序-matlab program of ballistic missile defense system target identification procedures matlab
Update : 2025-02-17 Size : 14kb Publisher : fangzi
[Graph Recognize] missilesimulation DL : 0: matlab程序防御系统弹道导弹目标识别方面的matlab程序-matlab program of ballistic missile defense system target identification procedures matlab
Update : 2025-02-17 Size : 2kb Publisher : fangzi
[ADO-ODBC] dandaofenxi DL : 0: 复杂情况下的弹道分析仿真。对于导弹专业的理论仿真很实用。-Complex case of ballistic analysis simulation. For the theoretical simulation of the missile professional practical.
Update : 2025-02-17 Size : 22kb Publisher : 风海啸
[OpenGL program] atbm DL : 0: 反战术导弹导弹比例导引律三维弹道仿真程序.-The proportion of anti-tactical ballistic missile missile guidance law of three-dimensional trajectory simulation program.
Update : 2025-02-17 Size : 1kb Publisher : stephen
[matlab] zyzd DL : 0: 最优制导律反战术弹道导弹TBM弹道仿真，matlab编写。-Optimal Guidance Law TBM anti-tactical ballistic missile trajectory simulation, matlab prepared.
Update : 2025-02-17 Size : 2kb Publisher : stephen
[OS program] trajectory1 DL : 0: C语言计算导弹弹道,C语言计算导弹弹道 -C language calculated ballistic missiles, C language calculated ballistic missile
Update : 2025-02-17 Size : 3kb Publisher : 吕君
[Applications] ProportionalNavigationGuidanceEmuator DL : 0: 用比例导引律仿真拦截器拦截来袭导弹的时间步长模拟算法,MT弹道数据，具体自己定-Proportional guidance law simulation interceptor missiles to intercept incoming time-step simulation algorithm, MT ballistic data, specific itself
Update : 2025-02-17 Size : 1kb Publisher : jintong
[Other] COM_imm DL : 1: This paper studies the problem of tracking a ballistic object in the reentry phase by processing radar measurements. A suitable (highly nonlinear) model of target motion is developed and the theoretical Cramer—Rao lower bounds (CRLB) of estimation error are derived. The estimation performance (error mean and-This paper studies the problem of tracking a ballistic object inthe reentry phase by processing radar measurements. A suitable (highly nonlinear) model of target motion is developed and thetheoretical Cramer-Rao lower bounds (CRLB) of estimationerror are derived. The estimation performance (error mean and
Update : 2025-02-17 Size : 2kb Publisher : zhangsheng
[Other] CS DL : 2: This paper studies the problem of tracking a ballistic object in the reentry phase by processing radar measurements. A suitable (highly nonlinear) model of target motion is developed and the theoretical Cramer—Rao lower bounds (CRLB) of estimation error are derived. The estimation performance (error mean and-This paper studies the problem of tracking a ballistic object inthe reentry phase by processing radar measurements. A suitable (highly nonlinear) model of target motion is developed and thetheoretical Cramer-Rao lower bounds (CRLB) of estimationerror are derived. The estimation performance (error mean and
Update : 2025-02-17 Size : 2kb Publisher : zhangsheng
[Other] EKF DL : 0: This paper studies the problem of tracking a ballistic object in the reentry phase by processing radar measurements. A suitable (highly nonlinear) model of target motion is developed and the theoretical Cramer—Rao lower bounds (CRLB) of estimation error are derived. The estimation performance (error mean and-This paper studies the problem of tracking a ballistic object inthe reentry phase by processing radar measurements. A suitable (highly nonlinear) model of target motion is developed and thetheoretical Cramer-Rao lower bounds (CRLB) of estimationerror are derived. The estimation performance (error mean and
Update : 2025-02-17 Size : 1kb Publisher : zhangsheng
[Software Engineering] Matlab_Simulink_daodan_3dof DL : 1: 提出了基于MATLAB/Simulink的导弹三通道弹道动力学模型仿真方法。分析了运动受力情况,给出导弹空间六自由度运动动力学模型,对在某初始条件下的三通道弹道进行了仿真和分析,结果很好地反映了弹道特点,证明该仿真方法有效可行。-Based on MATLAB/Simulink ballistic missile dynamic model of three-channel simulation method. Analysis of the movement by force, is given a missile in space dynamic model of six degrees of freedom movement, the initial conditions in a three-channel under the ballistic simulation and analysis, the results well reflect the ballistic characteristics of the simulation method proved effective feasible.
Update : 2025-02-17 Size : 137kb Publisher : 李恒

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