搜索资源列表
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
GMisssileTraje
- 通用弹道仿真计算程序源码V1.0本程序源码包为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源码，适用于无控弹药，用户能需要根据加入三点法、比例导引等导引方法，修改、扩充成相应的的有控、制导导模拟仿真弹道程序源码。程序源码包中MissileTrajectorySimulationRk.h的rk()是经典的4阶龙格库塔方法求常微分方程的数值算法的函数子程序源码，大家可参考使用。M -The general trajectory simulation program so
TMisssileTrach
- 导弹拦截的比例制导MATLAB仿真程序源码，从别的地地方看到的，研究过，做的不错 -The proportion of guided missile interception MATLAB simulation program source code, from other places, places to see, and have studied, do good
jiguangfangzhen
- 激光对红外成像制导系统干扰效能的仿真研究,以比例制导律和碰撞干扰模型为基础，通过计算机仿真研究激光对红外制导系统的干扰效能.-Laser jamming effectiveness of infrared imaging guidance system simulation research, on the basis of the proportional guidance law and the collision interference model, through computer s
predict
- 一种预测制导律，稍加改动即可进行仿真，效果还不错(A predictive guidance law)
激光对红外成像制导系统干扰效能的仿真研究
- 以比例制导律和碰撞干扰模型为基础，通过计算机仿真研究激光对红外制导系统的干扰效能，给出了详尽的仿真结果(Based on the proportional guidance law and collision jamming model, the jamming effectiveness of the laser to the infrared guidance system is studied by computer simulation, and the detailed simulat
比例导引法
- 建立模型添加比例导引法制导律、受力分析、运动分析，飞行力学仿真，仿真结果图片显示。(The model added speed tracking law, force analysis, motion analysis, flight mechanics simulation, and simulation result picture display.)
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
matlab仿真程序
- 自适应滑模制导，末制导。matlab，供学习参考(Adaptive sliding mode guidance and terminal guidance)
DF
- 自己搭建的六自由度仿真模型，有很高的参考价值(matlab/simulink/uav/airplane)
MATLAB——导引律程序
- 攻击角约束制导律matlab仿真程序 比例变结构均有(Matlab simulation program for attack angle constraint guidance law)
Simulink仿真
- 为制导律、控制率的仿真做了很好的基础模型(A good basic model is built for guidance law and control rate simulation.)
弹道仿真
- 制导控制一体化6自由度弹道仿真, C++ , Matlab(The 6DOF Trajectory simulation of the integrated guidance and control design.)