Description: 根据导弹仿真数据，绘制可直观显示弹道特性的理想弹道曲线。给出了比例导引法的差分方程，建立了
比例导引法的三维弹道仿真模型。在对比例导引法进行三维弹道仿真的基础上，分别对增量比例导引、基于二次
型的最优制导律和考虑动态特性的二次型最优制导律进行了三维弹道仿真，绘制出了可直观显示弹道特性的理想
弹道，计算了导弹与目标的遭遇时间，并对结果进行了比较分析。最后得出考虑弹体动态特性的二次型最优制导
律具有最优性。-According to the missile simulation data, mapping can be visual display characteristics of an ideal ballistic ballistic curve. Proportional navigation law gives the differential equation, proportional navigation law established a three-dimensional trajectory simulation model. Proportional navigation in the three-dimensional trajectory simulation method, based on the respective proportion of the incremental guidance, based on quadratic optimal guidance law and consider the dynamic characteristics of quadratic optimal guidance law for a three-dimensional trajectory simulation, rendering a visual display may be the ideal ballistic trajectory characteristics, calculated the missile with the target Platform: |
Size: 189440 |
Author:特步 |
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Description: 一篇很好的文章,对学习比例导引很有帮助,其中还有用matlab对比例导引的编程,程序可以运行,本人试过-A very good article, very helpful guidance to learning proportion, including using matlab programming for proportional navigation, the program can run, I tried Platform: |
Size: 219136 |
Author:大 |
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Description: 采用比例导引法,把三维追击轨道分解到两个二维平面上分别导引,并充分考虑到目标的
机动性对弹道的影响,用MATLAB软件编写程序模拟出导弹实际追击的三维变轨弹道,绘制出分运动和合运动中各参数的
变化曲线。最后比较了不同的追击速度和不同的导引系数k对弹道特性的影响,考虑到导弹实际飞行时受需用法向过载的
制约,导出了导引系数k应满足的普遍公式,提出了对实战具有一定参考价值的建议。
-Using proportional navigation law, in pursuit of the three-dimensional orbit decomposition to two two-dimensional plane, respectively, guidance, and taking fully into account the objectives of the impact of mobility on the trajectory, using MATLAB software programming practical pursuit of missile simulated three-dimensional orbit trajectory , to map out points Movement Hop movement curve of each parameter. Finally, the pursuit of different speed and different-guided ballistic coefficient k on the characteristics of, taking into account the actual missile flight by the need to overload the use of constraints derived Seeker coefficient k should satisfy the general formula, put forward on the actual reference value has a certain proposal. Platform: |
Size: 295936 |
Author:李恒 |
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Description: 比例导引理想弹道仿真Matlab代码，给出了比例导引法的差分方程, 采用Matlab语言, 对比例导引法的导弹理想弹道进行了三维数据仿真, 绘制出三维理想弹道。随导弹与目标参数变化情况, 对理想弹道的特性进行了分析。-Ideal proportional navigation trajectory simulation Matlab code, the law gives the proportional navigation differential equations using Matlab language, the ideal ratio of ballistic missile guidance method for simulation of three-dimensional data, to map out the ideal three-dimensional trajectory
Platform: |
Size: 1024 |
Author:madier |
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Description: 导弹飞行过程中采用比例导引法，本程序对飞行轨迹就行模拟计算。-Missile flight in the proportional guidance law, the procedures of the flight path on-line simulation. Platform: |
Size: 1024 |
Author:caoyj |
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Description: 抄录的是飞行器制导与控制及其matlab仿真技术
毕开波编著p159，仿真的是二维比例导引仿真，递推采用的是龙哥库塔方法
用的不是欧拉方法
我花了很长时间才敲到电脑上，望大家给点掌声，打字员llittlebird
错误的没有，有图为证
要下载两个-Reproduces the Aircraft Guidance and Control of matlab simulation Bi Kaibo ed p159, the simulation is two-dimensional proportional navigation simulation, recursive method used in the Long Ge Kuta Euler method is not used for a long time I spent knocking to the computer, hope everyone to the point of applause, typists llittlebird mistake not, there are two photo cards to download Platform: |
Size: 4096 |
Author:zhang |
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Description: 给出了比例导引法的差分方程, 采用Matlab语言, 对比例导引法的导弹理想弹道进行了三维数据仿真, 绘制出三维理想弹道。随导弹与目标参数变化情况, 对理想弹道的特性进行了分析-Given the proportional guidance law of difference equation, based on Matlab language, for proportional guidance law missile ideal ballistic three-dimensional data simulation and rendering the three-dimensional ideal trajectory. With missiles and target parameter change, to ideal ballistic characteristic was analyzed
Platform: |
Size: 1024 |
Author:jason |
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Description: 介绍了比例导引法的导引规律，推导了基于比例导引规律的拦截弹弹道方程．给出了一种目标做正弦
机动飞行的轨道方程，并采用Matlab对拦截弹拦截目标进行了目标拦截仿真．分析了拦截弹速度和目标速度，以及导引系数对拦截弹弹道的影响，研究了导弹实际飞行中弹道曲率与法向过载的关系．-Analysis of Trajectory Simulation of Proportional Guidance Based on Matlab Platform: |
Size: 338944 |
Author:李斌 |
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Description: 比例导引算法的实现，包括两个M文件，一个主程序和一个被调用的函数文件-Proportional navigation algorithm, including two M-files, a main program and a call function files Platform: |
Size: 1024 |
Author:txp |
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Description: 利用C语言实现导弹三自由度弹道，制导采用比例导引法，适合导弹飞行力学初学者学习-Using C language to realize three degrees of freedom ballistic missile, guidance using the proportional guidance method, suitable for beginners learning missile flight mechanics Platform: |
Size: 1024 |
Author:杨哲 |
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Description: 以比例导引律为基础，用伴随矩阵的构建解释了其闭环形式的解，其中包括初始航向角误差HED的图行，便于分析-The proportional guidance law as the foundation, with the adjoint matrix construction and explains its closed form solution, which includes the initial heading angle error of HED graphics, easy analysis Platform: |
Size: 1024 |
Author:曹静 |
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Description: 比例导引法的导弹和目标之间，理想弹道模型，用于了解导弹和目前在最佳时间遭遇的图形-Proportional guidance law between missile and target, the ideal trajectory model, used to understand graphical missile and is currently experiencing in the best time. Platform: |
Size: 1024 |
Author:孙权 |
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Description: 用matlab，采用三维比例导引，引导飞机接近目标。每个函数都独立一个m文件，易于阅读，学习。-Using matlab, using three-dimensional proportional navigation guidance, guide the aircraft close to the target. Each function is independent of an m-file, easy to read and learn. Platform: |
Size: 4096 |
Author:俞吉 |
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Description: 介绍了比例导引法的导引规律，推导了基于比例导引规律的拦截弹弹道方程．给出了一种目标做正弦
机动飞行的轨道方程，并采用Matlab对拦截弹拦截目标进行了目标拦截仿真．分析了拦截弹速度和目标速度，以
及导引系数对拦截弹弹道的影响，研究了导弹实际飞行中弹道曲率与法向过载的关系．-Proportional guidance law is introduced，and trajectory equation of intercepting missile based
on proportional guidance law is deduced．A kind of orbit equation of target in sine mobility is given，and
the missile intercepting the target is simulated with Matlab．The influence of missile speed，target speed
and guidance mode on the trajectory is analyzed．The relationship between trajectory curvature and normal
over-loading is researched． Platform: |
Size: 677888 |
Author:sonheungmin |
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Description: 用Matlab编写的铅垂平面内的比例导引方案弹道程序，目标为水平面内的平动物体-Proportional navigation scheme with ballistic programs written in Matlab vertical plane, the target for the level of animal body in a horizontal plane Platform: |
Size: 111616 |
Author:宋 |
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Description: Four degree of freedom missile motion equation based on proportional navigation method，The motion equation of 4-DOF missile based on proportional guidance method is given, and the termination conditions are given Platform: |
Size: 1238 |
Author:2239538092@qq.com |
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