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cPP
- c++ 通用弹道仿真计算程序(经典版) 程序源代码-c++ common trajectory simulation program (classic version) source code
trajectory
- 防空导弹攻击机动目标的六自由度弹道仿真文件，基于simulink搭建，简单实用-simulink for trajectory simulation
r4
- Matlab/simulink 导弹三自由度弹道仿真-Matlab/simulink simulation ballistic missile three degrees of freedom
sky_ground_missile
- 空地导弹全弹道仿真：自由下滑段+固定倾角下滑+转平飞过渡段+平飞段+导引段-Space Missile Simulation: free falling segment fell++ fixed angle turn in level flight segment+ transition level flight segment+ guide section
bosuyindao
- 采取波束指令制导方式设计的matlab程序，比较适合弹道仿真-Beam guidance system designed to take command of matlab program, more suitable trajectory simulation
atbm
- 反战术导弹导弹比例导引律三维弹道仿真程序.-The proportion of anti-tactical ballistic missile missile guidance law of three-dimensional trajectory simulation program.
MissileTrajectorySimulation
- c++ 通用弹道仿真计算程序,读取文件，将结果写到文件中-c++ MissileTrajectorySimulation
Trajectory-simulation
- 滑翔，铅垂平面，最大升阻比，三种情况弹道仿真-THE REAL EXAMPLES
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
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
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
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
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
MissileTrajectorySimulation
- 通用弹道仿真计算程序V1.0 本程序包为vxLand提供的经典版的通用导弹、炮弹、火箭弹等的弹道仿真计算程序，适用于无控弹药，(General ballistic simulation calculation program V1.0 This package provides vxLand classic version of the general missile, shells, rockets and other ballistic simulation procedures, ap
6 Degree Missile trajectory Simulation
- 基于MATLAB平台开发的导弹六自由度弹道仿真模型(Six degree of freedom simulation model of Missile Based on MATLAB platform)
龙哥库塔
- 应用龙格库塔法，解决迫击炮的弹道轨迹，可以调节道道的角度，有图片展示。(Using the Runge Kutta method to solve the trajectory of the mortar, the angle of the road can be adjusted and the picture can be displayed.)
Untitled
- 导弹一般采用“自控 + 自导”的制导体制，卫星侦察信息支持下的导弹打击海上移动目作战过程为: 解算卫星侦察信息，获得目标指示信息;将目标指示信息装订到导弹导引部，发射导弹; 导弹按照预先设定的轨道飞行，到达自控终点位置，末制导雷达开机; 末制导雷达覆盖目标，截获目标信号，对目标定位; 导弹对目标进行自动跟踪飞行，直到命中目标(The missile generally uses "self-control + homing" guidance system, and the
daodan
- 本程序基于导弹弹道的模拟，设计了matlab程序(This program is based on the simulation of missile trajectory, and designs the matlab program.)