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H-guide-FDTD-Code
H-Guide Matlab Code by FDTD nethod
- 2009-09-24 23:28:43下载
- 积分:1
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GSM_PSK
GSM,PSK调制的Matlab代码,可以使用的,免费提供给大家@(GSM,PSK modulation
matlab code,can be used in the design.)
- 2009-03-18 17:30:48下载
- 积分:1
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xianxianfanchenzuzhijieqiugen
这是线性议程组的直接解法,有十种不同的解法(这与迭代解法是不同的)……(This is the direct linear solution of the agenda of groups, there are dozens of different method (which is different from the iterative solution) ... ...)
- 2009-05-16 13:34:20下载
- 积分:1
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STR-1.3.Synchro
cours systeme temps reel synchronisation
- 2014-01-17 18:09:49下载
- 积分:1
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01_introduction
Matlab Introduction ppts
- 2009-04-17 20:16:10下载
- 积分:1
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Chapter5
例1 验证方程组初值问题的解
例2 求一个二阶非齐次线性方程组的初值问题的三次近似解
例3 用逐次逼近法求方程组初值问题的解(Cases of a verification of equations initial value problem is solved two cases of seeking a second-order non-homogeneous linear equations of the approximate solution of initial value problem of the three cases of three successive approximation method with the initial value problem of seeking the solution of equations)
- 2010-02-05 23:17:00下载
- 积分:1
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LEO_SPECK
一种无系数表的SPECK编码算法,不再单独划分动态存储空间用于 LSP、LIS 系数表,可在损失一定PSNR的情况下,降低算法的实现复杂度,提高处理速度
(A coefficient table SPECK coding algorithm is no longer a separate division of the dynamic storage space for the LSP, LIS coefficient table, in the case of the loss of a certain PSNR, reduce the algorithm complexity, increase processing speed
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- 2012-05-16 18:29:26下载
- 积分:1
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testpro3
matlab code for Particle swarm optimzation
- 2013-05-15 09:15:49下载
- 积分:1
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zigzag
matlab写的图像Zigzag置乱的函数,特别适用于初学者学习(matlab write Zigzag calculation function, especially for beginners to learn)
- 2014-07-14 00:41:58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