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以比例导引制导律为基础，用matlab语言描写了脱靶量同目标机动性能之间的关系-In order to proportional navigation guidance law as the foundation, the relationship between miss distance with the target maneuver performance are described using MATLAB language
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比例导引法的几个matlab程序，根据绝对弹道进行编程设计-Proportional navigation law matlab program, according to the absolute ballistic Programming
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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-Proportional navigation law gives the differential equations, using Matlab language, the ideal proportional navigation law missile trajectory simulation of three
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自己编写的比例导引法 simulink 打击机动目标-I have written simulink proportional navigation law against maneuvering targets
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一种有效的导引方法，是对比例导引方式的改进。-An effective guidance method is proportional navigation mode improvements.
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比例导引法 导弹三维仿真，可以用来计算导弹的飞行轨迹-The Proportional Navigation Act missile three-dimensional simulation
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该程序建立了导弹的六自由度的仿真模型，导引律采用一种不同于比例导引律的最优制导方式。-The program established a six degrees of freedom simulation model missile guidance law is different from using a proportional navigation guidance law optimal way.
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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.
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Project : Missile Target Simulation using Proportional Navigation
Proportional navigation is the guidance law used by most missiles in operational use
today. This method of guidance, generates missile acceleration commands in proportion
to the
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导弹制导算法MATLAB仿真例程，制导系统、自寻的制导律设计与仿真，如追踪法、平行接近法、比例导引法等-Missile guidance algorithm based on MATLAB simulation routines, guidance systems, guidance law design and simulation of self-seeking, such as tracing, nearly parallel method, proportional navigation
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基于MATLAB导弹仿真源代码(missile simulation)
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-Missile simulation based on MATLAB source code (missile simulation)
Differential equation gives the proportiona
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增量比例导引算法，可用于弹道目标的拦截等处理-Interception increment proportional navigation algorithm can be used for ballistic targets handling
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无人机/有人直升机协同空对地攻击方法.蒙特卡洛法，比例导引，弹道精度分析，对地攻击-UAV/someone coordinated ground attack helicopters approach. Monte Carlo method, proportional navigation, trajectory accuracy analysis, ground attack
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导弹比例导引法的最优控制方法改进的仿真文件-Optimal Control of Missile proportional navigation and improved simulation files
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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 miss
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matlab/simulink 三种方法的弹道仿真（追踪法、比例导引法、平行接近法） -matlab/simulink Trajectory Simulation of three methods (tracing method, proportional navigation law, parallel close to the law)
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MATLAB编写的平面比例导引运动学程序，自己写的，可用于导弹导引段过载分析-MATLAB prepared proportion plane kinematics program guide, write your own can be used to guide the missile segment analysis Overload
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比例导引,真正的程序，实测可用！可以修改为其它导引律-Proportional Navigation
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设计的比例导引法引导导弹飞行的程序，比较适合航空制导-Design proportional navigation guidance missile program, more suitable for aerospace guidance
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三维的导弹比例导引法设计的制导程序，可以用于3D弹道路径的仿真，使用matlab程序设计-Three-dimensional design of the missile proportional navigation guidance program, can be used to simulate 3D trajectory path using matlab programming
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