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ceshecheng
- 导弹参数已知的情况下，给定弹道倾角测射程-Ballistic missile parameters are known in the case of a given angle measurement range
p
- 使用四阶龙格库塔法求解内弹道方程，得出二级轻气炮各项参数-Fourth-order Runge-Kutta method to solve ballistic equations, draw the two-stage light gas gun, the parameters of the
bilidaoyinfa
- 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
MISSILE
- 针对三点法三维运动学弹道仿真问题，建立了两种仿真模型 第一种模型采用数值积分算法求解 三点法运动学方程组，求解过程较为复杂 第二种模型利用三维空间相关几何知识，将求解三点法三维运动学 弹道的图解法转化为求解一元二次方程的问题，使求解过程简单直观 最后，对两种模型进行了仿真，并将其 应用到地空导弹制导控制系统的仿真研究中，将理想弹道与控制弹道进行了对比 结果表明，两个模型均解决了一般情形下三点法三维运动学弹道求解的问题，为三点法三维制导律以及弹道特性研究提供了一种方法-Three-po
gd
- 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-VisualBasic6.0 prepared bottom row ballistic missile program Notes rich bottom row ballistic missile flow field numerical simulation, the program can be run directly compiled by
61
- 提出了一种结合SVD的小波变换方法，对其在外弹道测量数据中的野值剔除进行了研究。对观测数据进行小波分解，将小波分解后的近似分量和细节分量组合实现相空间重构，作为SVD方法的输入观测矩阵，根据奇异 熵增量准则，对奇异值进行筛选，根据SVD逆变换重构原信号。这一方法克服了Hankel矩阵相空间构建方法数据 端点失真问题。以小波分解后分量重构的相空间可以满足正交性，进一步提高了SVD进行数据降噪和野值检测的精度。仿真数据和试验数据处理结果证明了这一方法的有效性。-Proposed a meth
ab-v-datm
- 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。-VisualBasic6.0 prepared bottom row ballistic missile program Notes rich bottom row ballistic missile flow field numerical simulation, the program can be run directly compile and w
MissileTrajectorySimulation
- 通用弹道仿真计算程序(简版)V1.0--C++源代码****通用弹道仿真计算程序(简版)V1.0--C++源代码-General ballistic simulation program (short version) V1.0, c++ source code
ode45-matlab
- 本程序特别适合于弹道计算等方面使用。比ODE45函数的速度加快了很多，且程序充分展示了Matlab向量运算的强大功能，以及编程的简单快捷。-This procedure is particularly suitable for use ballistic calculations and other aspects. ODE45 faster than a lot of functions and procedures for demonstrating the power of Matlab
MISSILETEST
- 实现模拟导弹发射场景，实现多视角观察导弹运行弹道-Implementation scenarios simulated missile launch, multi-perspective on running ballistic missile
s-function
- matlab 仿真弹道导弹拦截来袭敌方导弹的程序，用s函数编写，既直观而且转换成c/c++很方便，可以与vc混合编程，有问题随时联系-Matlab simulation of ballistic missile intercepting the enemy s missile program, written using the s function, both intuitive and converted to c/c++ is very convenient, can be mixed w
non-controlled--missile-Simulation
- 用matlab/simulink搭建的六自由度无控弹道导弹模型，用来仿真在不加控制力作用下弹道导弹的飞行轨迹，simulink模型用RTW很方便转换成c/c++，适合飞行控制专业的新手学习，有问题请留言。-Using matlab/simulink to build the six degrees of freedom without controlled ballistic missile model is used to simulate the flight trajectory, in
chengxu
- 本程序特别适合于弹道计算等方面使用。比ODE45函数的速度加快了很多，且程序充分展示了Matlab向量运算的强大功能，以及编程的简单快捷。-The program is especially suitable for ballistic calculation such as the use of. Than the ODE45 function more quickly, and it shows the powerful function of Matlab vector operation
daodan
- 仿真了弹道导弹在大气层上方的自由飞行段和重新进入大气层的再入段的飞行过程，可以作为初学者的参考。-Simulation of ballistic missiles above the atmosphere again free flight segment and re-entry into the atmosphere during the flight load segments can be used as reference.
daodan-dandao
- 反舰导弹和战术导弹的弹道仿真模型，能够给出导弹在铅垂平面和三维空间的飞行弹道-Anti-ship missiles and tactical ballistic missile simulation model, able to give the flight trajectory of the missile in the vertical plane and three-dimensional space
Missile-guidance-laws
- 关于导弹拦截的相关技术研究，比较了现有价值的追逃策略及相关算法-The increasing maneuverability potential of tactical ballistic missiles motivates the development of improved interceptor guidance laws. In this paper two guidance laws are compared, both based on a pursuit–evasion di0
dandao
- 结算导弹弹道的程序 通过ode45结算非线性方程 得到弹道方程组的数值解-Ballistic missile program through the clearing settlement ode45 ballistic nonlinear equations numerical solution of equations
dandao3
- 弹道方程组的三个阶段仿真程序 通过将其分成三个阶段 分别得到数值解-Equations of the three-stage ballistic simulation program will be divided into three stages through to obtain numerical solutions were
icbm3d.0.4.beos_
- 这是一个3D防御游戏（包括所有源代码）。 它像原来的“导弹司令部”和它的克隆，在比赛中你用它来摧毁的冲击反洲际弹道导弹武器控制导弹（及其他脏东西）。-This is a 3D defense game (including all source code). It is like the original "Missile Command" and its clones, in the game you use it to destroy the impact of anti-inter
Movement-Trajectory-of-Bombing
- 考虑了轰炸机水平轰炸时投弹方向与载机速度方向不一致的情况，研究了投射炸弹的运动轨迹并建立了一组弹道方程，最后通过MATLAB采用龙格-库塔法求解轰炸弹道。-Considered inconsistent with the carrier aircraft bomb direction speed horizontal direction bombers bombing case study projected trajectory of the bomb and the establishmen