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09173810LMS11
System identification with adaptive filter usinglms
- 2012-03-22 14:59:27下载
- 积分:1
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iniparser
INI parser impelemantation for LPC1769
- 2013-05-08 06:37:27下载
- 积分:1
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Virtual-modems
调制解调器(即Modem),应用程序编程源码,很好的参考资料。(Modem (ie Modem), application programming source code, a good reference.)
- 2014-02-17 16:40:59下载
- 积分:1
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chap_02
solutions in matlab of the book DSP using matlab by proakis
- 2010-10-09 16:09:40下载
- 积分:1
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finalTestLPR
this matlab source code for detect plate number
- 2013-09-14 00:57:05下载
- 积分:1
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liufao_V2.0
有借鉴意义哦,基于混沌的模拟退火算法,模拟数据分析处理的过程。( There are reference Oh, Chaos-based simulated annealing algorithm, Analog data analysis processing.)
- 2016-08-15 00:24:39下载
- 积分:1
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MattProject
Project with report for quantized digital filter realization for a 4th order butterworth filter
- 2014-12-13 00:20:45下载
- 积分:1
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fit
文化算法。利用MATLAB编写的文化搜素算法(Culture Algorithm)
- 2013-10-29 20:26:04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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path-planning
基于改进的人工势场法的机器人路径规划,加入bug算法避免机器人陷入局部最小(Robot path planning based on improved artificial potential field method, adding the robot bug algorithm avoids local minima)
- 2014-05-05 09:10:54下载
- 积分:1