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- 弹道导弹对拦截弹仅测角被动跟踪的可观测性分析，弹道导弹对拦截弹仅测角被动跟踪的可观测性分析-Ballistic missile interceptor missile angle measurement only passive tracking observability analysis, ballistic missile interceptor missile angle measurement only passive tracking observability analysis
Missile Pand PJet
- 模拟导弹飞行仿真，模拟弹道飞行轨迹，是研究导弹飞行的重要部分-Simulated missile flight simulation, simulated ballistic flight path, an important part of the missile flight study
CNS
- 天文导航，弹道导弹SINS/CNS组合导航，轨迹发生器，卡尔曼滤波-Celestial navigation, ballistic missile SINS/CNS integrated navigation, trajectory generator, Kalman filtering
Kalmanfilter
- 弹道导弹跟踪过程中的Kalman滤波应用-Application of Kalman filter in ballistic missile tracking
bilidaoyinfa
- 利用C语言实现导弹三自由度弹道，制导采用比例导引法，适合导弹飞行力学初学者学习-Using C language to realize three degrees of freedom ballistic missile, guidance using the proportional guidance method, suitable for beginners learning missile flight mechanics
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
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
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
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
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
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
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
ballis
- A method for the determination of the trajectory of a ballistic missile over a rotating, spherical Earth given only the launch position and impact point has been developed. The iterative solution presented uses a state transition matrix to correc
shizhongxiugai_v1
- 89c51的数字钟程序，在keil里边一。当弹道弹道弹道弹道导弹-89C51 the digital clock procedures, in a keil inside. When the ballistic trajectory of ballistic missile
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