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: The book presents a historical background of past and present guided missile systems and the evolution of modern weapons,discusses the generalized missile equations of motion, aerodynamic forces and coefficients, the important subject of the various types
of tactical guidance laws and/or techniques, weapon delivery systems and techniques,strategic
missiles and cruise missile theory and
design. Platform: |
Size: 3264512 |
Author:jbarragan |
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Description: ANSYS的导弹尾翼建模及其气动分析，
是卡耐基梅隆大学网站上的一个ANSYS气动分析应用的例子，帮助理解ANSYS建模与分析，非常经典。-ANSYS modeling and aerodynamic missile fin analysis, is a Carnegie Mellon University on the website an example of application of ANSYS aerodynamic analysis to help understand the ANSYS modeling and analysis, very classic. Platform: |
Size: 319488 |
Author:jyll |
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Description: Datcom软件的GUI版，有界面 比普通的Dos操作要方便的多。用于计算气动数据！-Datcom the GUI version of the software, there are interface than the normal operation of the convenience of multi-Dos. Used to calculate the aerodynamic data! Platform: |
Size: 4474880 |
Author:ww |
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Description: 通过对MatlAB 中Designing a Guidance System in MATLAB® and Simulink® 的导弹质量特性和气动特性的改变，并由原有的3DOF扩展为6DOF，仿真导弹的弹道特性、姿态特性和过载特性。 -In Matlab Designing a Guidance System in the MATLAB ® and Simulink ® missiles quality characteristics and aerodynamic characteristics of change, expansion by existing 3DOF 6DOF simulation missile ballistic characteristics, attitude, features and characteristics of overload. Platform: |
Size: 208896 |
Author:战斗机 |
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Description: 导弹空气动力学，用于导弹计算流体力学和弹道仿真研究的参考书籍，非常系统和实用.-missile aerodynamic.This book is a good reference for CFD of missiles and Trajectory simulation. Platform: |
Size: 8304640 |
Author:Neil |
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Description: 弹道仿真matlab程序
包含了铅垂平面内弹道仿真的matlab程序（不带有气动参数，需要自己给定），含有差值，仿真的整个过程。导弹飞行动力学材料。-The trajectory simulation matlab program includes the vertical plane trajectory simulation matlab program (without the aerodynamic parameters need to given), contains the difference, the simulation of the whole process. Missile flight dynamics material. Platform: |
Size: 3072 |
Author:李志强 |
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Description: 通过导弹的空气动力系数计算导弹的之心运动方程组，并利用MATLAB进行绘图，包括轨迹，速度时间曲线等-Aerodynamic coefficients calculated by missile missile equations of motion of the heart, and using MATLAB graphics, including trajectory, velocity-time curve Platform: |
Size: 234496 |
Author:lizhili |
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Description: 通用导弹气动力计算程序,由美国空军开发，比较实用且简单易学-Common Missile aerodynamic calculation program, developed by the Air Force, more practical and easy to learn Platform: |
Size: 613376 |
Author:逍遥游 |
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Description: GUI version of missiledatcom. The aerodynamic parameters, including drag coefficient, lift coefficient and torque coefficient, can be calculated quickly by inputting missile shape parameters. Platform: |
Size: 45143987 |
Author:2239538092@qq.com |
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Search - missile aerodynamic