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Description: 基于VxWorks的导弹模拟器的设计与实现
基于VxWorks的导弹模拟器的设计与实现-VxWorks-based missile simulator design and missile-based VxWorks Simulator Design and Implementation
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Size: 2936832 |
Author: 秦清全 |
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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。
-Missile simulation
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Size: 1024 |
Author: 许龙 |
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Description: 关于导弹制导的一些文献 适合初学者对制导率原理的认识和设计-Some of the literature on missile guidance guidance for beginners to understand and design principles of the rate
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Size: 13633536 |
Author: marlin |
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Description: 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.
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Size: 6786048 |
Author: 刘睿智 |
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Description: 导弹可视化仿真源程序：包括m文件、可视化界面-Missile visualization simulation program
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Size: 19456 |
Author: 韩华翔 |
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Description: 本文主要通过极点配置法，设计了导弹三通道的控制系统，整体性能达到了设计的基本要求，在导弹垂直上升阶段及俯仰阶段，分别选取特征点进行仿真，达到了垂直发射中姿态角控制的要求。但是，采用极点配置法设计的控制律仍存在许多不足，短时间内具有良好的性能，而某一时刻之后系统将面临着严重的振荡。可以考虑采用其它方法重新设计，或是多种控制方法的结合，扬长避短，可获得更为理想的效果。-In this paper, the pole placement method, the design of a missile three-channel control system, the overall performance of the basic requirements of the design, select the feature points to simulate the missile vertical upward phase and pitch, respectively, reached the vertical launch attitude angle controlrequirements. However, the pole assignment method designed control law there are still many deficiencies in a short period of time has a good performance, a moment after which the system will face severe oscillation. Can consider using other methods to re-design, or a combination of a variety of control methods to advantage, the availability of more desirable effect.
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Size: 64512 |
Author: 战斗机 |
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Description: dynamic meshing of a missile body
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Size: 973824 |
Author: waseem121 |
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Description: 导弹空气动力学，用于导弹计算流体力学和弹道仿真研究的参考书籍，非常系统和实用.-missile aerodynamic.This book is a good reference for CFD of missiles and Trajectory simulation.
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Size: 8304640 |
Author: Neil |
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Description: 针对不确定非线性 BTT 导弹控制系统, 提出了一种基于模糊高斯基函数神经网络的自适应控制设计方法。在设计过程中将不确定部分合为一项, 应用模糊神经网络的万能逼近性质来逼近系统不确定项, 然后利用滑模控制和自适应模糊神经网络理论设计了控制器, 应用 Ly apunov 稳定性理论保证闭环系统的稳定性,并推导出自适应律,最后通过仿真结果验证该方法的有效性。-BTT missile based on fuzzy neural network adaptive control
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Size: 398336 |
Author: 刘漂帆 |
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Description: 弹道仿真matlab程序及导弹飞行力学
既包含程序，也包含相关的理论基础ppt资料-The trajectory simulation matlab program and missile flight mechanics includes both the program and also includes the theoretical basis ppt information
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Size: 1952768 |
Author: sunshines |
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Description: 从卫星观测的弹道导弹跟踪启动，算法是提出了在大气层外初始阶段，从一个或多个移动平台 (通常卫星) 使用视线 (LOS) 测量启动轨道弹道导弹。这一问题的主要特点是贫穷目标议案可观测性，导致出现很病态估计问题。-Ballistic Missile Track Initiation from Satellite Observations
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Size: 1382400 |
Author: xuelinger |
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Description: 一个关于导弹，火箭的程序，里面有阻力系数等气动参数。-A missile, rocket program, which drag coefficient and other aerodynamic parameters.
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Size: 4096 |
Author: 道斯 |
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Description: Missile adjust its direction to track the airplane-Including files:
1.matlab source code
2.vedio demo
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Size: 309248 |
Author: |
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Description: Simulation of Missile Communication using matlab
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Size: 190464 |
Author: Femi |
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Description: 导弹弹道的模拟程序。有误差分析。非常有参考价值！-Missile trajectory simulation program. Error analysis. Reference value!
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Size: 3072 |
Author: 张越 |
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Description: Amirkabir Univ的5状态导弹仿真MATLAB源代码.-Amirkabir Univ s 5 States Missile Simulation matlab source code.
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Size: 14336 |
Author: vivieny28 |
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Description: 导弹铅垂平面内的无控段和载入段弹道仿真MATLAB源代码-Missile trajectory simulation
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Size: 2048 |
Author: 上官元偌 |
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Description: ACM 中的导弹防御算法，内容详细，已生成可执行文件-ACM missile defense algorithm, very detailed
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Size: 6144 |
Author: liz |
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Description: 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-point method for three-dimensional kinematic trajectory simulation problem, create a simulation model of the first two models using numerical integration algorithm for three-point method kinematics equations, solving process is more complicated second model using three-dimensional geometry of space-related knowledge, The three-point method for solving three-dimensional kinematic trajectory graphical method for solving a quadratic equation into the problem solving process so simple and intuitive Finally, the two models for simulation, and its application to air missile guidance and control system simulation study, the ideal trajectory were compared with the control trajectory results show that the two models are to solve the general case point method for solving the problem of three-dimensional kinematic trajectory, three-dimensional guidance law for the three-point method, and provides a ballistic characteristics method
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Size: 245760 |
Author: 叶新 |
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Description: 根据导弹相对动力学方程用m文件和simulink进行仿真计算-According to the missile with relative dynamics equation m file and simulink for simulation calculation
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Size: 14336 |
Author: 郑旭 |
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