搜索资源列表
Monte-Carlo
- 对仿真弹道进行3个参数偏差的蒙特卡罗打靶分析，然后给出置信区间高度-THE REAL EXAMPLES
dualpulse1
- 双脉冲固体火箭发动机外弹道的matlab程序-dual pulse solid rocket motor external ballistica
trajectory1
- 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
zhiliangyinshu
- 采用数值积分法求解相对量运动微分方程组，计算燃料相对质量因数。速度V =500m/s，时间t =3s，x方向位置x =674m，y方向位置y =329m，初始攻角 ，初始弹道倾角 -Using numerical integration method to solve the relative motion differential equations, the calculation of fuel relative quality factor. Velocity V = 500 m/s,
Navigation-Trajectory-Simulation
- 基于MATLAB+GUI的导弹比例导引的三自由度弹道仿真-MATLAB+ GUI based missile proportion of guiding three degrees of freedom trajectory simulation
zd500113359
- 导弹仿真代码可以准确的得出外弹道曲线非常实用方便-Missile simulation code can accurately draw the outer ballistic curve very practical and convenient
gas-and-steam-launch
- 水下潜艇导弹燃气蒸汽式弹射时的内弹道方程和参数求解。-Solving interior ballistic equations and parameters when missile launched by gas and steam system on submarine.
neiwaidandaojisuan
- 该程序已经编写好，用于求解普通弹丸内外弹道的参数值，需要代码的话请联系上传者-nei wai dan dao ji suan
Gauss
- 高斯伪谱法求解的弹道，希望对大家有用的！代码比较复杂，但是可以运行。-Gauss pseudo spectral method for solving the trajectory, we hope to be useful! Code is more complex, but can be run.
zhen
- matlab/simulink 三种方法：追踪法、比例导引法、平行接近法的弹道仿真-matlab/simulink tracing method, proportional navigation law, parallel close to the law
trajectory
- 弹道程序,通过输入输入相关参数，可以进行外弹道计算-The program of calculate the trajectory
TCtrajectory
- 通过TeeChart插件，对外弹道进行了可视化仿真计算，输出了弹道曲线。-Using TeeChart,it can get the curve of the trajectory.
sdtbm
- 本程序为弹道仿真程序，主要用于反弹道导弹仿真设计，供参考-guidance system
6DOF
- 本程序为弹道仿真程序，为6自由度仿真程序，供参考-guidance law
zytbm
- 本程序为弹道仿真程序，最有比例制导律仿真程序，供参考使用-guidance LAW
gswgmcz
- 攻击飞机类目标，导弹弹道设计仿真程序,仅供参考-guidance law design
Matlab
- 该程序为弹道仿真测试程序，可供学习使用，仅供参考-guidance law
HW
- 用于演示尾椎法自导弹道的GUI界面程序,参数自定义，动画演示-a code used to demonstrate the guide process of weizhui method
Trajectory-Simulation
- 基于Matlab的比例导引弹道仿真分析.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-Trajectory Simulation Analysis Based on Matlab
Air-defense-missile
- 对防空导弹的拦截弹道进行了仿真了，主要特点是采用了模块化设计。-The airlift missile intercepted trajectory was simulated, the main feature is the use of modular design.