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qrxjq
天线方向图可以看出此算法的性能，该程序把静态方向图与加了旁瓣电平－30db的切比雪夫权方向图相比较(Antenna pattern can be seen the performance of this algorithm, the program direction of the static map with the addition of side lobe level of-30db Chebyshev right direction compared to Figure)
- 2007-10-15 15:56:14下载
- 积分：1
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wa024
对于初学matlab的同学会有帮助，IDW距离反比加权方法，一个师兄的毕设。( Matlab for beginner students will help, IDW inverse distance weighting method, A complete set of brothers.)
- 2017-04-25 16:28:58下载
- 积分：1
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SVM-classifier
用matlab实现非线性支持向量机分类器对多类进行分类。(Using matlab to achieve non-linear support vector machine classifier for multi-class classification.)
- 2011-05-02 19:16:35下载
- 积分：1
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Elastic
弹性波动方程的有限差分 采用的是标准网格(Elastic wave equation finite-difference grid using a standard)
- 2021-01-22 15:48:45下载
- 积分：1
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LQR
研究高超声速飞行器在纵向的运动情况，对系统的速度和飞行高度进行仿真分析，我们将对在不同的 、 值的条件下分析出系统的最优性能(The longitudinal motion of the hypersonic vehicle is studied, and the system speed and flight height are simulated. We will analyze the optimal performance of the system under different conditions and values.)
- 2019-04-02 21:05:13下载
- 积分：1
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puguji
谱估计
(1)修正协方差法
(2)多重信号分类（MUSIC）算法
(3)ESPRIT算法
(4)皮萨论科（Pisarenko）谐波分解法
并对各算法进行分析。
解压后即可在MATLAB上运行(spectral estimation (1) the amendment of covariance (2) multiple signal classification (MUSIC) algorithm (3) ESP RIT algorithm (4) On order pizza's from Branch (Pisarenko) harmonic decomposition of each algorithm for analysis. Unpacked can run in MATLAB)
- 2007-03-30 09:53:56下载
- 积分：1
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MUSIC-revised
本文是music算法的一种改进，其具有更好的性能，以及能够满足大多数用户的需求，希望会给大家带来方便(This article is a modified music algorithm, which has better performance, and the ability to meet the needs of most users, I hope we will bring convenience)
- 2014-01-19 21:37:16下载
- 积分：1
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月球软着陆程序
说明： 月球软着陆仿真：在停泊轨道上，探测器在脉冲制动的作用下，经霍曼变轨，下降到距月面大约 15 公里的近月点，该近月点就是主制动段的初始制动点。主制动段以下是障碍检测与规避和最终着陆段。在主制动段，由于探测器的初始速度很大(1.692km/s)，所以主制动段制导律设计的主要目的就是高效抵消此速度，将探测器导引到期望的末端状态(Lunar soft landing simulation: in the parking orbit, the probe under the action of pulse braking, through the hohmann change of orbit, to descend to about 15 kilometers from the surface of the moon, the near-moon point is the main braking section of the initial braking point. Following is the main braking section for obstacle detection and avoidance and the final landing section. In the main braking section, since the initial velocity of the detector is very large (1.692km/s), the main purpose of the guidance law design of the main braking section is to effectively offset this velocity and guide the detector to the desired terminal state)
- 2021-01-28 22:18:35下载
- 积分：1
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MSA
说明： msa program for the matlab
- 2020-04-29 19:00:58下载
- 积分：1
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QPlayCap01
windows打开拍照检索关闭camera的相关函数实现(The camera Function for windows)
- 2015-02-12 09:18:39下载
- 积分：1
