Description: 导弹控制系统的鲁棒控制设计实例，包括3中不同的方法，有详细的注解和最后simulink 仿真。-Missile control system design example of robust control, including 3 in different ways, have detailed comment and final simulink simulation. Platform: |
Size: 37888 |
Author:jesse |
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Description: 用Simulink工具箱,对导弹仿真模型进行了模块化设计,条理清晰,信息流流向明确,具有很好
的可视化效果,增加了模块的可移植性。最后在一定条件下仿真得出了弹道及部分参数的变化结果,结果已经得到初步验证。
-Using Simulink toolbox, the missile simulation model modular design, the clarity of the information flow the flow of clear, with good visualization to increase the portability of the module. Finally, under certain conditions, the trajectory simulation obtained and some parameters of changes in the results of preliminary verification results have been. Platform: |
Size: 242688 |
Author:李恒 |
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Description: 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. Platform: |
Size: 140288 |
Author:李恒 |
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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: 导弹的3自由度仿真层序——simulink，希望对大家有用-3 degree of freedom missile simulation sequence- simulink, hope useful for all of us Platform: |
Size: 21504 |
Author:战狼 |
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Description: 我这有几篇文章，是关于导弹建模的，主要适用simulink建模并仿真，希望对大家有所帮助。-I have several articles, on the missile model, the main application of simulink modeling and simulation, we hope to be helpful. Platform: |
Size: 4141056 |
Author:选会 |
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Description: 导弹Simulink仿真的一些步骤和体现，各位可以看看，这是我转载别人的。-Simulink simulation of missile and embody some of the steps, you can see, this is my reprint of others. Platform: |
Size: 2048 |
Author:何冰 |
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Description: 采用Creator 和Vega 平台以及Simulink仿真开发工具对空面导弹的飞行视景仿真技术进行了研究。提出了一种空面导弹飞行视景仿真系统的体系构架，利用获取的DED真实地形数据，通过Creator建立大地形三维模型；借助VC/MFC开发平台，实现了Simulink数字仿真系统与视景仿真的通信；在Vega中实现视景仿真系统的软件开发调试。仿真结果表明，该系统能够为空面武器系统研制阶段的参数优化和效能评估提供有效的验证平台。-Creator and Vega used Simulink simulation platform and development tools, face-to-air missile flight visual simulation technology was studied. A blank surface missile flight visual simulation system architecture, use the DED for real terrain data, terrain through the Creator to establish a large three-dimensional model with VC/MFC development platform, digital simulation implemented Simulink and Visual Simulation System communications in Vega to achieve visual simulation system software development and debugging. Simulation results show that the system can be empty surface weapon system development phase of the parameter optimization and performance evaluation of an effective verification platform. Platform: |
Size: 4096 |
Author:robert |
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Description: 1、利用simulink中sfunction方法建立航天器姿态动力学模型和运动学模型；
2、利用linmod对非线性模型线性化；
3、姿态模型线性化后，利用极点配置（pole）方法求取控制参数；
4、将控制参数带入非线性模型仿真控制效果。-One using simulink sfunction method to establish the dynamic model and kinematic model of the spacecraft attitude
2, the use of linmod linearization of the nonlinear model
Attitude model linearization, the use of pole configuration (pole) is used to obtain the control parameters
4, the control parameters into the nonlinear model simulation control effect. Platform: |
Size: 9216 |
Author:战斗机 |
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Description: 本文主要通过极点配置法，设计了导弹三通道的控制系统，整体性能达到了设计的基本要求，在导弹垂直上升阶段及俯仰阶段，分别选取特征点进行仿真，达到了垂直发射中姿态角控制的要求。但是，采用极点配置法设计的控制律仍存在许多不足，短时间内具有良好的性能，而某一时刻之后系统将面临着严重的振荡。可以考虑采用其它方法重新设计，或是多种控制方法的结合，扬长避短，可获得更为理想的效果。-In this paper, the pole placement method, the design of a missile three-channel control system, the overall performance of the basic requirements of the design, select the feature points to simulate the missile vertical upward phase and pitch, respectively, reached the vertical launch attitude angle controlrequirements. However, the pole assignment method designed control law there are still many deficiencies in a short period of time has a good performance, a moment after which the system will face severe oscillation. Can consider using other methods to re-design, or a combination of a variety of control methods to advantage, the availability of more desirable effect. Platform: |
Size: 64512 |
Author:战斗机 |
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Description: 最近发现有不少人需要导弹六自由度Simulink仿真模型，
而且大家好像对导弹Simulink建模比较关心，这里我就把我做的一个导弹六自由度Simulink仿真模型分享给大家以作参考。
-Recently found that many people need missile Simulink simulation model of six degrees of freedom, and everyone seems to be more concerned about the missile Simulink modeling, I put I do a six degrees of freedom Simulink simulation model of the missile to share to everyone for reference. Platform: |
Size: 22528 |
Author:jingjing |
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Description: 根据导弹相对动力学方程用m文件和simulink进行仿真计算-According to the missile with relative dynamics equation m file and simulink for simulation calculation Platform: |
Size: 14336 |
Author:郑旭 |
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Description: 用matlab/simulink搭建的六自由度无控弹道导弹模型，用来仿真在不加控制力作用下弹道导弹的飞行轨迹，simulink模型用RTW很方便转换成c/c++，适合飞行控制专业的新手学习，有问题请留言。-Using matlab/simulink to build the six degrees of freedom without controlled ballistic missile model is used to simulate the flight trajectory, in uncontrolled force of ballistic missile flight control, suitable for beginners to professional learning, have any questions please leave a message.
Platform: |
Size: 25600 |
Author:周胜俞 |
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Description: 关于导弹建模和仿真的五篇论文，基于SIMULINK的便携式红外寻的防空导弹制导控制系统仿真建模_季向东；一种在分布交互仿真系统中使用Simulink模型的方法_唐凯；基于MATLAB的导弹弹道建模与仿真_许龙；基于Matlab_Simulink的导弹六自由度弹道仿真系统设计_高胜灵-Modeling and simulation on missile five papers based on SIMULINK of portable infrared homing air defense missile guidance control system simulation modeling _ Ji Xiangdong A method for distributed interactive simulation systems using Simulink models _ Tang Kai missile based on MATLAB Trajectory modeling and simulation _ Xu Long ballistic missile six degree of freedom simulation system based Matlab_Simulink _ high spirit wins Platform: |
Size: 3347456 |
Author:li hongliang |
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Description: 这是一个最为经典的用SIMULINK进行导弹追踪，且命中目标的设计方案，可作为此类设计的一个典型案例。-This is the most classic a missile tracking and SIMULINK design scheme and shot on target, such design can be used as a typical case.
Platform: |
Size: 38912 |
Author:吴秋玲 |
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Description: 针对某些导弹在对目标进行打击时需要满足零脱靶量和攻击角度约束的要求,首先基于终端滑模控制和有限时间控制理论,改进了一种快速收敛的非奇异终端滑模函数,用于设计滑模面,结合自适应指数趋近律,提出了一种自适应非奇异终端滑模控制方法。(For some missile needs to meet the zero miss distance and attack angle constraint requirements in the attack on the target, based on the terminal sliding mode control and finite time control theory, improved non singular terminal sliding function a fast convergence, for the design of the sliding surface, combined with the self adaptation index reaching law, put forward a kind of adaptive non singular terminal sliding mode control method.) Platform: |
Size: 371712 |
Author:轻度
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