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2下载：
最优制导律反战术弹道导弹TBM弹道仿真，matlab编写。,Optimal Guidance Law TBM anti-tactical ballistic missile trajectory simulation, matlab prepared.
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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 Matla
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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-Given the proportional guidance law of difference equation, based on Matlab language, for proportional guidance law missile ideal ballistic three-dimensional dat
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求解导弹弹道……与制导律有些相关。是三维仿真弹道程序-Solving ballistic missile guidance law ... ... and some related. Three-dimensional trajectory simulation program
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导弹全弹仿真模型 制导律为比例 控制采用pid-Bomb simulation model of the missile guidance law for proportional control using pid
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导弹二次最优制导律设计matlab仿真程序，可以自己设置导弹和目标位置、速度，攻击角度-Missile quadratic optimal guidance law matlab simulation programCan set missile and the target position, speed, attack Angle and so on
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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.
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导弹根据比例导引法追踪目标，可以显示出遭遇时间，设定的目标运动轨迹发生变化，他们的遭遇时间也相应发生变化。-Missile guidance law based on the proportion of target tracking, can show the encounter time, set the target trajectory change their encounter time is also changed accordingly.
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simlink编写的BTT导弹六自由度模型，制导律采用经典的比例制导律-Simlink write the bluetail ticket tracker (BTT) missile six degrees of freedom model of guidance law USES the classical proportional guidance law
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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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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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三维维平面内导弹拦截目标的某种算法程序,没有对比其他方法，仅供参考-3 d d plane missile intercept target an algorithm program, not compared with other methods, are for reference only
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对导弹拦截目标的末制导方法在二维平面内进行仿真，列举了两种控制算法，做了比较，程序完全可以运行，硕士论文中间的一部分程序-Of missile intercept target terminal guidance method was simulated in a two-dimensional plane, enumerates two kinds of control algorithm, in comparison, the program can be run completely, m
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考虑导弹自动驾驶仪动态特性的带攻角约束的制导律-Impact angle guidance law considering missile`s dynamics of autopilot
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missile guidance and navigation using Pagony method
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