搜索资源列表
61
- 提出了一种结合SVD的小波变换方法,对其在外弹道测量数据中的野值剔除进行了研究。对观测数据进行小波分解,将小波分解后的近似分量和细节分量组合实现相空间重构,作为SVD方法的输入观测矩阵,根据奇异 熵增量准则,对奇异值进行筛选,根据SVD逆变换重构原信号。这一方法克服了Hankel矩阵相空间构建方法数据 端点失真问题。以小波分解后分量重构的相空间可以满足正交性,进一步提高了SVD进行数据降噪和野值检测的精度。仿真数据和试验数据处理结果证明了这一方法的有效性。-Proposed a meth
ab-v-datm
- VisualBasic6.0编写的底排弹内弹道程序注释丰富;底排弹内弹道数值流场仿真计算,程序编译通过可直接运行,并附带结果和图像供参考。-VisualBasic6.0 prepared bottom row ballistic missile program Notes rich bottom row ballistic missile flow field numerical simulation, the program can be run directly compile and w
proportional-guidance-law
- 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.给出了一种目标做正弦 机动飞行的轨道方程,并采用Matlab对拦截弹拦截目标进行了目标拦截仿真.分析了拦截弹速度和目标速度,以 及导引系数对拦截弹弹道的影响,研究了导弹实际飞行中弹道曲率与法向过载的关系.-Proportional guidance law is introduced,and trajectory equation of intercepting missile based on proport
matlab-example
- 我的毕业设计,用matlab仿真外弹道,在已有的外弹道模型下运用龙格库塔算法进行解算,最后做了相应的GUI界面!-I graduated from the design, simulation using matlab exterior ballistics, exterior ballistics in the existing model using Runge-Kutta algorithm solver, and finally made the corresponding GUI in
trajectory
- 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-Proportional navigation law gives the differential equations, using Matlab language, the ideal proportional navigation law missile trajectory simulation of three
missile-simulation1
- 导弹弹道matlab仿真程序,用于对导弹弹道进行设计仿真-missile simulation programme in matlab languege,used for missile dandao design
dandao3
- 弹道方程组的三个阶段仿真程序 通过将其分成三个阶段 分别得到数值解-Equations of the three-stage ballistic simulation program will be divided into three stages through to obtain numerical solutions were
trajectory-simulink-grogram-and-doc
- 这是一个外弹道的简单matlab仿真,其中包含了四节龙格库塔方法(自己编写)程序并用matlab GUI加以实现,可以作为GUI学习的参考,是西北工业大学探测制导与控制技术专业本科课程设计的内容。-This is a simply simulation program by matlab, which contains four Runge-Kutta method program and be realized by matlab GUI,it can serve as a refere
vbdatm
- VisualBasic6.0编写的底排弹内弹道程序注释丰富;底排弹内弹道数值流场仿真计算,程序编译通过可直接运行,并附带结果和图像供参考。像是一个民爆企业的内部火药计算程序,具体的换算关系不是太懂,是别人发过来让分享的VB源码,可用VB6顺利编译。 Module1模块:用于定义全局变量,函数fun()和xztel(),fun函数:用于实现四阶龙格库塔法解微分方程右端子式,xztel函数:用于计算火药特征尺寸-Ballistic rich program notes written in
Missile-algorithm
- 基于MATLAB导弹仿真源代码(missile simulation) 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 based on MATLAB source code (missile simulation) Differential equation gives the proportiona
simulink
- 一个鱼雷攻击目标模型的matalab仿真,用c++实现,最后画出了鱼雷的攻击弹道,实在二维平面内的,里面用了龙格库塔的积分算法,可以参考-A torpedo attack matalab target model simulation, using c++ realize, finally draw a torpedo attack trajectory, it is, which used the Runge-Kutta integration algorithm for 2D plane,
Trajectory-simulation-program
- 包含了铅垂平面内弹道仿真的matlab程序(不带有气动参数,需要自己给定),含有差值,仿真的整个过程。导弹飞行动力学材料。-Contains the vertical plane trajectory simulation matlab program (not with the pneumatic parameter, needs its own given), contains the difference, the whole process simulation. Missile fli
waidandao
- 使用龙格库塔法对火箭弹水平轰炸弹道进行仿真-Using the Runge-Kutta method for level bombing rocket trajectory simulation
HTV-2-trajectory-Calculate
- 按正弦方式变化的攻角控制规律,利用MATLAB对HTV-2跳跃滑翔式飞行器弹道过程进行了仿真-Tracking the development plans of The DARPA/AF Falcon program,the program calculates the reentry skipping trajectory
2Dzhidao
- 2维的导弹制导程序,可以用于仿真2D的弹道路径,使用matlab仿真-2-dimensional guided missile program, can be used to simulate 2D trajectory path, the use of matlab simulation
3Dzhidao
- 三维的导弹比例导引法设计的制导程序,可以用于3D弹道路径的仿真,使用matlab程序设计-Three-dimensional design of the missile proportional navigation guidance program, can be used to simulate 3D trajectory path using matlab programming
Monte-Carlo
- 对仿真弹道进行3个参数偏差的蒙特卡罗打靶分析,然后给出置信区间高度-THE REAL EXAMPLES
zd500113359
- 导弹仿真代码可以准确的得出外弹道曲线非常实用方便-Missile simulation code can accurately draw the outer ballistic curve very practical and convenient
TCtrajectory
- 通过TeeChart插件,对外弹道进行了可视化仿真计算,输出了弹道曲线。-Using TeeChart,it can get the curve of the trajectory.
gswgmcz
- 攻击飞机类目标,导弹弹道设计仿真程序,仅供参考-guidance law design