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trajectory-simulink-grogram-and-doc
- 这是一个外弹道的简单matlab仿真，其中包含了四节龙格库塔方法（自己编写）程序并用matlab GUI加以实现，可以作为GUI学习的参考，是西北工业大学探测制导与控制技术专业本科课程设计的内容。-This is a simply simulation program by matlab, which contains four Runge-Kutta method program and be realized by matlab GUI,it can serve as a refere
CCRP
- 采用连续计算命中点方法投放炸弹的弹道解算-Using a continuous method of calculating the hit point bombs ballistic solver
External-ballistics-1
- 计算外弹道有关大口径火炮的外弹道计算以及枪弹的计算-the way of math in External ballistics
vbdatm
- VisualBasic6.0编写的底排弹内弹道程序注释丰富；底排弹内弹道数值流场仿真计算，程序编译通过可直接运行，并附带结果和图像供参考。像是一个民爆企业的内部火药计算程序，具体的换算关系不是太懂，是别人发过来让分享的VB源码，可用VB6顺利编译。 Module1模块：用于定义全局变量，函数fun()和xztel()，fun函数：用于实现四阶龙格库塔法解微分方程右端子式，xztel函数：用于计算火药特征尺寸-Ballistic rich program notes written in
Calculate
- 采用瞬时平衡假设，计算导弹的理想弹道，命中精度0.35米-Instantaneous equilibrium assumption, calculate the ideal ballistic missile hit accuracy 0.35 m
trajectory
- 用4阶龙格库塔法求解给定攻角情况下的空地导弹弹道。-to solve a given Angle of attack of the ballistic missile with a four order runge kutta method.
Missile-algorithm
- 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
donghua
- 应用龙哥库塔法求解弹道并且模拟弹道的轨迹，及其对比图-Long 哥库塔 track application and simulation method for solving ballistic trajectory, and its comparison chart
MissileTest
- 描述弹道轨迹，有尾焰和撞击爆炸碎片效果，效果一般，也仅供学习。-Describe the trajectory, there is an explosion and the impact debris plume effects, effects in general, but also for learning.
simulink
- 一个鱼雷攻击目标模型的matalab仿真，用c++实现，最后画出了鱼雷的攻击弹道，实在二维平面内的，里面用了龙格库塔的积分算法，可以参考-A torpedo attack matalab target model simulation, using c++ realize, finally draw a torpedo attack trajectory, it is, which used the Runge-Kutta integration algorithm for 2D plane,
standardtrajectory
- 导弹标准弹道计算，可以给出飞行过程中的高度、速度、攻角等信息-Ballistic Missile standards can be given during the flight altitude, speed, angle of attack and other information
sanwei
- 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
DatComSetUp
- dotcom gui 曲线绘制，进行弹道计算程序，2010@xjtu-dotcom gui
rocket
- 本matlab代码是鲁棒控制导弹弹道的matlab应用示例-Robust Control
zengliangbiliyindao
- 一组有意义的弹道导弹增量比例引导弹道仿真弹道分析程序，分别用一维、二维插值等方法对弹道导弹的弹道进行了仿真，分析了其弹道特性-A set of meaningful ballistic missile incremental proportion guide ballistic trajectory simulation analysis program, with one-dimensional and two-dimensional interpolation method for the
KKVbiaozhundandao
- KKV标准弹道仿真程序，仿真了KKV在中段拦截TBM的弹道。供大家参考。-KKV standard ballistic simulation program, the simulation of KKV in the middle of the TBM interception trajectory.For your reference.
MinEnergeOrbit
- 可生成从任意点发射攻击全球任意点的一条最小能量弹道，并确定关机点参数。-Can generate a minimum energy trajectory launch attacks from any point to any point worldwide, and to determine the shutdown point parameters.
wdd
- 用visual basic编写的火箭外弹道可视化界面及计算程序，模型简单，易使用-Written using visual basic visual interface rocket exterior ballistics and calculation procedures, the model is simple, easy to use
jisuandandaochengxu
- 某炮弹质量为20KG，直径120mm，出炮口是的初速为800m/s，初始发射角等于45°，试计算弹道。解答过程与程序详解-A shell quality is 20 kg, 120 mm in diameter, out of the muzzle velocity of 800 m/s, initial emission Angle is 45 °, try ballistic calculation. The solution process and procedure, rounding
bishe
- 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