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zarchan_the_fourth_edition
- 这是本战略战术导弹制导的书中的matlab程序,比书中的 forchan程序简单易懂-This is the strategic and tactical missile guidance book of Matlab procedures, the book than a simple understandable forchan
matlab_sim
- 实现The Kalman Filter 机器人的自定位-The Kalman Filter is a technique from estimation theory that combines the information of di erent uncertain sources to obtain the values of vari ables of interest together with the uncertainty in these. The lter has b
ResearchontheProcessofShiptoairMissile
- 舰空导弹协同制导流程研究,通过对舰空导弹常见制导方法过程的分析,结合网络中心战以及协同作战能力的概念,提出多平台协同制导对 导弹制导模式的要求,对未来舰空导弹协同制导时的制导过程进行初步探讨,并指出实现协同制导需要解决的关键技术。-Ship-to-air guided missile synergistic flow study, through the ship-to-air guided missile common method of analysis of the process,
bili
- 导弹飞行过程中采用比例导引法，本程序对飞行轨迹就行模拟计算。-Missile flight in the proportional guidance law, the procedures of the flight path on-line simulation.
VRLinkRTW
- 基于VRLinkRTW实现导弹制导仿真联邦成员设计-Simulation based VRLinkRTW Federal members to achieve the design of missile guidance
the-proportional-guidance--
- 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-Given the proportional guidance law of difference equation, based on Matlab language, for proportional guidance law missile ideal ballistic three-dimensional dat
Missile
- 导弹内部控制系统的设计。包括导弹制导，导弹飞行，导弹控制，通信传输等等部分。-Missile internal control system design. Including missile guidance, missile flight, missile control, communications, transport and so on parts.
11111
- 经典导弹导引算法图形界面matlab程序-Classic missile guidance algorithm Matlab graphical interface program
6dof
- 导弹全弹仿真模型 制导律为比例 控制采用pid-Bomb simulation model of the missile guidance law for proportional control using pid
qianzhiliangfa
- 前置量法弹道仿真。前置量法也称角度法或矫直法，采用这种导引方法导引导弹时，在整个飞行过程中，导弹-制导站的连线始终提前于目标-制导站连线，而两条连线之间的夹角 则按某种规律变化。通过建模仿真，使大家更形象生动的理解前置量法。-Front method of trajectory simulation. Front Method, also known as the angle law or straightening method, using this guide guided missile
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
5th-IBM-C
- Tactial and Strategic Missile Guidance一书第五版程序源码，C格式-Tactial and Strategic Missile Guidance book the fifth edition of the program source code, C format
5th-IBM-MATLAB
- Tactial+and+Strategic+Missile+Guidance一书第五版 Matlab格式程序代码-Tactial+and+Strategic+Missile+Guidance book fifth edition of the the Matlab format of the program code
5th-Mac-C
- Tactial+and+Strategic+Missile+Guidance一书源程序 For MacOS in C format-Tactial+and+Strategic+Missile+Guidance book source For MacOS in C format
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
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
Guidance
- 简单的导弹制导模块，根据飞行过程中的误差实时地调整导弹的飞行攻角-Simple missile guidance module, according to the flight of the missile attack angle error adjustment flight in real time
the-missile-guidance-law-simulation
- 三维维平面内导弹拦截目标的某种算法程序,没有对比其他方法，仅供参考-3 d d plane missile intercept target an algorithm program, not compared with other methods, are for reference only
Missile-Spiral-trajectory
- 反导导弹末制导与控制论文及导弹螺旋弹道生成文件，可正确运行。-At the end of the anti-missile missiles and missile guidance and control paper spiral trajectory generated files, you can run correctly.
bilidaoyinfa
- 通过matlab编程实现了比例导引法制导的弹目飞行的轨迹生成(Trajectory Generation of Missile Guided by Proportional Guidance Method)