Description: 微分的数值计算综合了算法在导弹中的应用，很有用-Differential synthesis of the numerical calculation algorithm in a missile application, very useful Platform: |
Size: 1024 |
Author:zhangjianqi |
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Description: 利用四阶runge-kutta法，计算铅垂面内导弹弹道轨迹的一个例子。-Using fourth-order runge-kutta method, calculation of vertical-plane trajectory of the missile an example Platform: |
Size: 1024 |
Author:赌挖宝 |
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Description: 本程序的开发环境为MATLAB6.5版本，所编程序须在此环境下运行。由于气动模型的离散性，且采用了许多工程计算经验公式和实验数据，所以在编程时会比较繁杂，为了使程序读起来方便清晰，在编制程序时采用了如下的思路：
考虑到程序的一般结构，这里将气动计算系统分为三大模块：输入模块、气动计算模块以及结果输出模块。考虑到本系统的特殊性，又将输入模块划分为初始数据输入模块、导弹外形参数模块以及插值数据库模块，并采用M文件格式编制；气动计算模块则采用了子系统的结构形式，并用Simulink 模块编制；结果输出模块则是采用M文件的形式将气动计算模块得到的结果输出到工作区间并将数据结果绘制成曲线。最后，为了运行的方便，编制了一个名为Start_file.m的M文件，按流程依次调用编写的所有程序，在运行此程序时，只需将所有程序加载于“Current Directory”指定的文件夹中（即路径的设定），并在“Command Window”中输入“Start_file”即可。
(导弹气动计算程序)-This procedure for the development environment MATLAB6.5 version, the proceedings shall be made to run in this environment. Due to the discreteness of the aerodynamic model, and used a lot of experience in engineering calculation formula and experimental data, it would be more complicated programming, in order to facilitate a clear reading procedure, the procedure used in the preparation of the following ideas:
Procedures, taking into account the general structure of computing systems here will be divided into three pneumatic modules: input module, pneumatic calculation module, as well as the results of the output module. Taking into account the specificity of the system, will enter the module is divided into the initial data input module, the missile shape parameter interpolation module and database module, and the use of M file format aerodynamic calculation module uses the structure subsystem, and the preparation of Simulink module the results of output module is used in the for Platform: |
Size: 102400 |
Author:刘成 |
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Description: 据说某岛国J 开放了一种导弹防御系统，它的第一发能拦截任意高度的导弹，但
是以后的每一发不能超过前一发的高度。拦截导弹时候按导弹到来的顺序进行拦
截，不能先拦截后面的再拦截前面的导弹。请计算最多能拦截多少导弹。
输入：第一行为敌国N 国发来的导弹数目k（k<=25），第二行为k 个正整数，
依次表示k 枚导弹的高度-A certain island J is said to open a missile defense system, its first hair can intercept any height of the missile, but
The height of each hair must not exceed the former situation. When the interceptor missile intercept the missile arrival of the order
Cut-off can not be the first interception behind the missile to intercept the front. Calculation can intercept missiles.
Input: N State s of the first acts of an enemy missile number k (k <= 25), the second behavior k positive integers,
In turn, said the height of k missiles Platform: |
Size: 2004992 |
Author:Arvin |
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Description: 弹道导弹射程计算中的微分误差计算方法，英文原版，好文章-Ballistic missile range of the calculation of the differential error calculation method, the original English, good article Platform: |
Size: 561152 |
Author:baofeihu |
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Description: 通用弹道仿真计算程序V1.0
本程序包为vxLand提供的经典版的通用导弹、炮弹、火箭弹等的弹道仿真计算程序，适用于无控弹药，(General ballistic simulation calculation program V1.0
This package provides vxLand classic version of the general missile, shells, rockets and other ballistic simulation procedures, applicable to non controlled ammunition,
The user can modify and expand the corresponding simulation trajectory of control and guidance according to the three point method and proportional navigation) Platform: |
Size: 1024 |
Author:小花猫
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