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trajectory1.C语言计算导弹弹道
- C语言计算导弹弹道,C语言计算导弹弹道 ,C language calculated ballistic missiles, C language calculated ballistic missile
zyzd.rar
- 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.
弹道分析
- 用matlab来编写的较复杂的程序，用来对导弹进行弹道分析-prepared using Matlab to the more complex procedures for the analysis of ballistic missile
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- matlab程序 防御系统弹道导弹目标识别方面的matlab程序-matlab program of ballistic missile defense system target identification procedures matlab
dandaofenxi
- 复杂情况下的弹道分析仿真。对于导弹专业的理论仿真很实用。-Complex case of ballistic analysis simulation. For the theoretical simulation of the missile professional practical.
atbm
- 反战术导弹导弹比例导引律三维弹道仿真程序.-The proportion of anti-tactical ballistic missile missile guidance law of three-dimensional trajectory simulation program.
ProportionalNavigationGuidanceEmuator
- 用比例导引律仿真拦截器拦截来袭导弹的时间步长模拟算法,MT弹道数据，具体自己定-Proportional guidance law simulation interceptor missiles to intercept incoming time-step simulation algorithm, MT ballistic data, specific itself
COM_imm
- This paper studies the problem of tracking a ballistic object in the reentry phase by processing radar measurements. A suitable (highly nonlinear) model of target motion is developed and the theoretical Cramer—Rao lower bounds (CRLB) of estimat
CS
- This paper studies the problem of tracking a ballistic object in the reentry phase by processing radar measurements. A suitable (highly nonlinear) model of target motion is developed and the theoretical Cramer—Rao lower bounds (CRLB) of estimat
EKF
- This paper studies the problem of tracking a ballistic object in the reentry phase by processing radar measurements. A suitable (highly nonlinear) model of target motion is developed and the theoretical Cramer—Rao lower bounds (CRLB) of estimat
Trajectorysimulationpackage
- 弹道仿真程序包，共5个m文件，一个主程序，4个子程序，很好的弹道模型仿真！-Trajectory simulation package, a total of 5 m file, a main, 4 sub-procedures, good ballistic model simulation!
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
Untitled2
- 一种基于弹道模型的机动目标跟踪算法 !针对当前目标跟踪算法中跟踪模型与现代反舰导弹实际运动不匹配而影响跟踪精度的问题!根据反 舰导弹的弹道特点!通过分析导弹受力情况和运动状态的关系!提出了一种基于弹道模型的机动目标跟踪算 法!并针对高速跃升俯冲运动!分别与基于L:$L=模型的目标跟踪算法作了性能比较 仿真结果表明!该算 法在原理上是正确可行的!可显著提高对高速强机动目标的跟踪性能-a maneuvering target tracking algorithm based on bal
nanomos-r186.tar
- nanoMOS is a 2-D simulator for thin body (less than 5 nm), fully depleted, double-gated n-MOSFETs. A choice of three transport models is currently available (drift-diffusion, classical ballistic, and quantum ballistic). The transport models treat qua
Basedon Matlab Simulink simulation
- Based on Matlab / Simulink simulation of ballistic missile three-channel-Based on Matlab/Simulink simulation of ballistic missile three-channel
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- simulation of ballistic target trajectiry
ballistic-missile-simulation
- 导弹的弹道分析程序，实现导弹弹道仿真，分析数据-Ballistic missile analysis procedures to achieve the missile trajectory simulation, analysis of data
Ballistic-missile-ballistics
- 弹道导弹弹道学，PDG格式。偶尔在一国防科技网看到的。相当不错。-Ballistic missile ballistics, PDG format. Occasionally, a National Defense Science and Technology Network to see. Quite good.
internal-ballistic
- 改程序为火炮内弹道程序，可以计算气体压力，速度等变化情况-Reform program for the Interior Ballistic program can calculate the gas pressure, speed changes
interior-ballistic
- 底排弹内弹道计算程序,使用VB编制，带有计算结果及附图可供参考-Interior Ballistic Caculate