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kitty
- 一. 追踪模型 以(x , y)代表飞机的坐标,v代表飞机的速度;以(X ,Y)代表导弹的坐标,u代表导弹的速度。 由于导弹时刻指向飞机,故有 dY/dX=(y-Y)/(x-X) 记k=u/sqrt((y-Y)*(y-Y)+(x-X)*(x-X)) 则有 dY/dt=k(y-Y) dX/dt=k(x-X) 故有叠代方程 Y=Y+k*(y-Y)*dt X=X+k*(x-X)*dt (程序中以t代dt) 程序中第一个for循环代表发射导弹打飞机,第二个
ParameterizedDesignForBBTMissilesControlSystem
- BTT导弹控制技术是当今导弹控制的一项新技术,相对于STT导弹控制技术来说,BTT有很多的优点。本论文基于线性控制系统理论中的特征结构配置和模型跟踪方法,提出了路棒控制的方法和可抑制抖动的多模型切换控制方法。有很好的借鉴意义。-BTT missile control technology is today's missile control of a new technology, Comparing with STT missile control technology, BTT ma
6DOF
- 导弹六自由度仿真模型,并且仿真了导弹攻击一个匀速直线运动的目标的过程-missile six degree-of-freedom simulation model and simulation of a missile attack on a uniform linear motion of the target
missile Guidance And Control
- 对于导弹控制的入门者,这是本很好的工具书。该书详细地描述了导弹的模型的建立,制导方式和控制原理等等。-For the missile control entry, which is a good instrument of this book. The book describes in detail the model set up of missiles, guided mode and control theory and so on.
daodandandaoyouhua
- 针对助推- 滑翔导弹的弹道优化问题,给出了一种求解其最大射程弹道的分段优化方法,建立了其 纵平面运动模型和弹道优化模型。在考虑攻角绝对值、攻角变化率、法向过载、分离点攻角衔接及落地条件等约束 下,应用序列二次规划法求解了其最大射程弹道。分析表明,助推- 滑翔导弹比传统弹道导弹射程显著提高,其最 优弹道的起伏有助于增大射程和提高突防能力-For booster- Optimize glider ballistic missile problem, give a maximum rang
Aero dynamic missile program
- 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
simulink
- 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.
Proportional navigation method
- 用比例导引法进行拦截弹针对机动目标的弹道仿真,仿真是基于三维模型。-Proportional navigation method used to intercept ballistic missile targets for motor simulation, simulation is based on three-dimensional model.
Six Degrees of Missile Simulation
- 基于matlab的simlink的导弹六自由度数学模型的飞行仿真程序-Based on matlab' s simlink six degrees of freedom mathematical model of the missile flight simulation program
Missile-Attitude-control
- 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,
Matlab missile gongji
- 利用simulink建立导弹三自由度运动模型,可以用来分析导弹运动-Simulink to build a missile three-DOF motion model can be used to analyze the missile movement.
missile-model--skp-file
- 导弹的三维模型 需要专门的googlesketchup软件打开 可以转换成3DS文件使用-The three-dimensional model of the missile googlesketchup requires specialized software to open 3DS files can be converted to use
simulation-of-6DOFmissile
- 自己用m文件建立的六自由度导弹模型,仿真导弹打击静止或运动目标(只需更改目标运动速度即可),有问题可以留言。-Six degree of freedom missile model using m file created, simulation of missile attacking stationary or moving targets (simply change the target velocity can be), messages can be a problem.
non-controlled--missile-Simulation
- 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
btt6dof
- 用matlab/simulink搭建的六自由度有控导弹模型,模型很全面,仿真比较真实,包括导弹弹体模型,目标模型,导引规律模型,控制器模型,舵机模型,有兴趣的可以下载,有问题请留言。-Using matlab/simulink to design six degree of freedom control missile model, the model is very comprehensive, comparative simulation real, including missile m
BTT-missile-6DOF-model-MATLAB
- 在matlab中编出的BTT导弹六自由度模型,可以参考-BTT six-DOF missile model
Real-time-display-of-dynamic-terrain
- 实现读取DEM数据来绘制地形,同时实现对地形的漫游,地形漫游是通过一个3D导弹模型作为标准来进行实现的-DEM data to achieve the terrain to draw, while the terrain of the roaming, terrain roaming through a 3D missile model as a standard to achieve
6 Degree Missile trajectory Simulation
- 基于MATLAB平台开发的导弹六自由度弹道仿真模型(Six degree of freedom simulation model of Missile Based on MATLAB platform)
新建文件夹
- 建立导弹的运动学与动力学模型,作用于导弹上的力、力矩及加速度、速度、位置、姿态等运动参数之间关系都由该模型定义,模拟导弹反导轨迹。(The kinematic and dynamic model of the missile is established, and the relation between the force, torque and acceleration, velocity, position and attitude on the missile is defined by
dandaoyouhua
- 建立导弹三自由度模型,对上升弹道轨迹进行优化。使用四阶龙格库塔方法进行解算。(A three-degree-of-freedom missile model was established to optimize the trajectory of the rising trajectory. Use the fourth-order Runge-Kutta method for solving.)