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Description: 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for代表飞机发现导弹后做正弦运动试图逃跑。
小结：
追踪模型中关键是利用叠代方程 Y=Y+k*(y-Y)*dt 确定追踪者的运动坐标，这样，不
X=X+k*(x-X)*dt
论被追踪者做何种运动，都可利用该叠代方程找出追踪者的运动轨迹（注意追踪者的速度应大于被追踪者的速度）。
-one. Track model (x, y) coordinates of the aircraft representatives, representatives v the speed of aircraft; A (X, Y), on behalf of the coordinates of missile, u representative of the speed of the missile. As the aircraft missile at times, it is dY / dX = (y-Y) / (x-X) recorded k = u / sqrt ((y-Y) * (y-Y) (x-x) * (x-X) ) have curves / dt = k (y-Y) dX / dt = k (x-X) there is an iterative equation Y Y = k * (y-Y) * dt X = X * k (x-x) * dt ( proceedings t substituting dt) procedures for the first cycle of a representative aircraft fired a missile, the second for representatives of aircraft missiles found after doing sinusoidal movement to try to escape. Summary : key tracking model is to use iterative equation Y Y = k * (y-Y) * dt tracers to determine the coordinates of movement, and X = X *
Platform: |
Size: 803 |
Author: 白小欣 |
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Description: 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for代表飞机发现导弹后做正弦运动试图逃跑。
小结：
追踪模型中关键是利用叠代方程 Y=Y+k*(y-Y)*dt 确定追踪者的运动坐标，这样，不
X=X+k*(x-X)*dt
论被追踪者做何种运动，都可利用该叠代方程找出追踪者的运动轨迹（注意追踪者的速度应大于被追踪者的速度）。
-one. Track model (x, y) coordinates of the aircraft representatives, representatives v the speed of aircraft; A (X, Y), on behalf of the coordinates of missile, u representative of the speed of the missile. As the aircraft missile at times, it is dY/dX = (y-Y)/(x-X) recorded k = u/sqrt ((y-Y)* (y-Y) (x-x)* (x-X) ) have curves/dt = k (y-Y) dX/dt = k (x-X) there is an iterative equation Y Y = k* (y-Y)* dt X = X* k (x-x)* dt ( proceedings t substituting dt) procedures for the first cycle of a representative aircraft fired a missile, the second for representatives of aircraft missiles found after doing sinusoidal movement to try to escape. Summary : key tracking model is to use iterative equation Y Y = k* (y-Y)* dt tracers to determine the coordinates of movement, and X = X*
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Size: 1024 |
Author: 白小欣 |
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Description: 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
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Size: 8192 |
Author: donotspam |
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Description: Missile 子弹 跟随效果 DelphiX
用Delphi6+DelphiX刚写的子弹跟随跟踪的代码。
总感觉不太真实，请各位高手指点指点，有没有好的算法实现跟踪。-Missile follow the effects of bullets DelphiX with Delphi6+ DelphiX bullets just write the code to follow the track. Feel less true, please instruct the expert advice, is there a good tracking algorithm.
Platform: |
Size: 733184 |
Author: bme_liuwei |
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Description: 三点法跟踪运载火箭系统跟踪目标弹作匀速直线运动，拦截弹做匀速率运动。里面微分方程是用欧拉法求解的，为了提高精确度，改成四阶龙格库塔法-Tracking system to track the target missile launch vehicle for uniform linear motion, interceptor uniform rate of movement to do. Which is Euler' s method for solving differential equations, in order to improve accuracy and change into a fourth-order Runge-Kutta method
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Size: 22528 |
Author: zhxzhx |
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Description: 本实验设计了一个《导弹打飞机》的动画演示程序。建立地面坐标系，横轴x代表水平射程，纵轴y代表垂直高度，单位均为km。假设导弹的初始位置为(0，0)，飞机的初始位置为(20，0)，飞机在20km高度以1km/s的速度做水平匀速直线运动，导弹从地面发射，以2km/s的速度做等速运动，以追踪法对飞机进行打击，即导弹的速度方向始终沿着弹目视线且指向目标。-The experimental design was a " missile hit the aircraft," the animated demo. Establishment of ground coordinates, the horizontal axis x represents the level range, representative of the vertical height of the vertical axis y, units are km. Assuming the missile' s initial position is (0,0), the aircraft' s initial position (20.0), aircraft altitude at the 20km to 1km/s speed to do the level of uniform linear motion, the missile launched from the ground to 2km/s constant speed of movement to do in order to track the method of combat aircraft, the missile' s velocity is always along the direction of line of sight and the target missile to the target.
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Size: 40960 |
Author: abler |
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Description: 这是航天器轨迹优化的程序，包括深空探测，空空导弹。-This is the optimization of the spacecraft track program, including deep space exploration, an air-to-air missile.
Platform: |
Size: 33792 |
Author: 尹佳杰 |
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Description: 靶场试验航路分析与设计方法，针对靶场导弹飞行试验的特点和要求,总结提出了靶场试验航路设计的思路及航路参数的表征形式,提出了试验航路方案的设计方法,建立了试验航路方案分析方法和相应步骤,给出了试验航路方案综合评估与优化的具体方法和思路.
-Range test route analysis and design methods for the shooting range missile flight test characteristics and requirements, summarizes proposed the range test route design ideas and forms of representation of the route parameters, the proposed design of the test route program, establish a test the route program analysis method and the corresponding steps, gives a the test routes comprehensive evaluation and optimization of specific methods and ideas.
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Size: 24576 |
Author: 李亮 |
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Description: 从卫星观测的弹道导弹跟踪启动，算法是提出了在大气层外初始阶段，从一个或多个移动平台 (通常卫星) 使用视线 (LOS) 测量启动轨道弹道导弹。这一问题的主要特点是贫穷目标议案可观测性，导致出现很病态估计问题。-Ballistic Missile Track Initiation from Satellite Observations
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Size: 1382400 |
Author: xuelinger |
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Description: Missile adjust its direction to track the airplane-Including files:
1.matlab source code
2.vedio demo
Platform: |
Size: 309248 |
Author: |
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Description: 该程序建立了导弹在二维坐标系中以比例导引法追踪目标的过程。-The program established a missile at a two-dimensional coordinate system with proportional navigation method to track the target process.
Platform: |
Size: 1024 |
Author: 王海涛 |
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Description: In this paper, formation control ideas for multiple spacecraft using the virtual structure approach
are presented. If there is no formation feedback from the spacecraft to the virtual structure, the
spacecraft will get out of formation when the virtual structure moves too fast for the spacecraft to
track due to spacecraft control saturation or the total system must sacriˉce convergence speed in
order to keep the spacecraft in formation. The spacecraft may also get out of formation when the
system is a® ected by internal or external disturbances. To overcome these drawbacks, an idea of
introducing formation feedback from the spacecraft to the virtual structure is illustrated in detail.
An application of these ideas to multiple spacecraft interferometers in deep space is given.
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Size: 314368 |
Author: alkatel |
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Description: 基于LGame引擎的Android塔防游戏，Java源码下载，游戏的图片等资源用了炫光塔防的图片，Java代码中有丰富注释，便于学习理解。本款塔防游戏游戏一共有4种塔，每一种塔都可以升级，都有各自的攻击属性，也可以卖掉换钱。白色塔：射速快杀伤小；绿色塔：使敌人减速，杀伤小；红色塔：导弹能够跟踪目标。杀伤较大；蓝色塔：发出能量波，杀伤大。具体刺激程序请下载源码编译后可运行一下-Based LGame Android tower defense game engine, Java source code download, game images and other resources with the glare tower defense picture, Java code has rich notes, easy to learn to understand. This paragraph tower defense games, a total of four kinds of towers, each tower can be upgraded, have their own attacks on property, you can sell for cash. White Tower: fast rate of fire killing small Green Tower: slow down the enemy, killing small red tower: the ability to track the target missile. Killing large Blue Tower: emit energy waves, killing large. Specific stimulus program, please download the source code can be compiled to run the
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Size: 3346432 |
Author: gpudn29 |
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Description: 反直升机导弹采用比例导引法攻击目标直升机
导弹发射位置：(0,0)
导弹速度：500m/s
直升机速度：100m/s
直升机爬升角度： 8°
直升机初始位置（四个）：
（4000,1000）、（4000，-1000）
（4000,100 ）、（4000,-100）
比例导引律k=1.5（可以自行在程序中修改）-this matlab program is aimed to simulate the track of the anti-helicopter missile when using proportional navigation method
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Size: 1024 |
Author: jixing |
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Description: 一个用simulink搭建的导弹追踪系统模型，并含有追踪到目标后的所有测试函数-A tracking system model built by Simulink missile, and contains all the test function to track the target
Platform: |
Size: 25600 |
Author: wu |
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Description: 对导弹拦击目标的轨道进行了仿真,并绘制出来相应的拦击轨迹-Intercepting missile target track simulation, and drawn the appropriate volley track
Platform: |
Size: 10240 |
Author: 张海洋 |
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Description: 导弹打击目标跟踪，轨道模型优化，算法优化等等。(Missile hitting target tracking, track model optimization, algorithm optimization and so on.)
Platform: |
Size: 1024 |
Author: JackSky |
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