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Description: 一个关于模拟导弹发射系统的C51源程序，自己写的，不完整，也拿来了
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Size: 1560 |
Author: hushoufang |
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Description: 一个关于模拟导弹发射系统的C51源程序，自己写的，不完整，也拿来了-A simulated missile launch system on the C51 source, wrote it myself, incomplete, but also brought
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Size: 1024 |
Author: hushoufang |
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Description: 导弹飞行动力学，空气动力学，做动力仿真飞行器仿真必修。-Missile flight dynamics, air dynamics, simulation of vehicle dynamics simulation to do compulsory.
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Size: 9129984 |
Author: Charles |
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Description: 防御导弹
Problem
某国为了防御敌国的导弹袭击，发展出一种导弹拦截系统。但是这种导弹拦截系统有一个缺陷：虽然它的第一发炮弹能够达到任意的高度，但是以后每一发炮弹都不能高于前一发的高度。某天，雷达捕捉到敌国的导弹来袭。由于该系统还在使用阶段，所以只有一套系统，因此有可能不能拦截所有的导弹。
-dao dan xi tong wen ti
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Size: 8192 |
Author: 杨阳 |
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Description: 这是导弹追踪问题的源代码，对于类似的题目（缉私）也适用-This is the question of the missile tracking the source code, for a similar topic (anti-) also applies to
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Size: 1024 |
Author: tang lu ming |
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Description: 燃料相对因素是导弹推进剂的质量和导弹总的质量的比值，它对于导弹的总体设计至关重要，决定了发动机的类型以及导弹的射程等性能，程序实现了对目标成功打击的优化弹道-The relative factor is the missile propellant fuel quality and the quality of the overall ratio of the missile, which is essential for the overall design of the missile determines the type of engine performance such as the missile range, the program achieved a successful attack on the target trajectory optimization
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Size: 31744 |
Author: 宁国富 |
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Description: 比例导引理想弹道仿真Matlab代码，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。-Ideal proportional navigation trajectory simulation Matlab code, the law gives the proportional navigation differential equations using Matlab language, the ideal ratio of ballistic missile guidance method for simulation of three-dimensional data, to map out the ideal three-dimensional trajectory
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Size: 1024 |
Author: madier |
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Description: 实现导弹发射效果，图像逼真，3D效果很好，是学习的好资料-Achieve the effect of missile launches, the image realistic, 3D effects are very good, good information on learning
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Size: 10620928 |
Author: 吴成志 |
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Description: 在matlab中进行试验的导弹功能模型仿真-The missile test in matlab function model simulation
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Size: 1024 |
Author: 曹东任 |
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Description: 空地导弹弹道设计，某型空地导弹总体设计，整个弹道分为五部分：自由下滑段、固定弹道倾角下落、转平飞过渡段、平飞段、导引段-Air-to-ground missile trajectory design
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Size: 2048 |
Author: |
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Description: 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
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Size: 2048 |
Author: 上官元偌 |
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Description: 包含导弹飞行力学的课程讲义等内容，另外还包含一个导弹弹道的仿真模型。实现性能较好-Contains the the course handouts content of the missile flight mechanics also contains a simulation model of the missile trajectory. To achieve better performance
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Size: 1949696 |
Author: 上官元偌 |
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Description: 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.
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Size: 1024 |
Author: 张杰 |
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Description: 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
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Size: 2048 |
Author: tocont |
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Description: 空地导弹弹道设计，某型空地导弹总体设计，整个弹道分为五部分：自由下滑段、固定弹道倾角下落、转平飞过渡段、平飞段、导引段-Air-to-ground missile trajectory design
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Size: 2048 |
Author: sedto |
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Description: 跟踪导弹动画模拟，在matlab下实现。-Tracking missiles animation, matlab implementation.
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Size: 1024 |
Author: 季冲 |
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Description: 本程序是利用matlab编程实现大气层内飞行的导弹的姿态控制程序，程序仿真时有GUI界面，方便调试参数-This program is the use of matlab programming attitude control procedures within the atmosphere flying missiles, the program has a GUI interface emulation, easy debugging parameters
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Size: 25600 |
Author: 玉海 |
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Description: Matlab，导弹纵向、横侧向运动分析。包括长短周期简化等各种对比分析程序。-Matlab, missile longitudinal, transverse lateral motion analysis. Including simplification cycle length comparative analysis of various programs.
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Size: 4096 |
Author: 周梦婕 |
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Description: 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.)
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Size: 14336 |
Author: panda13 |
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