-
FIR
FIR有限序列冲击响应滤波器的设计matlab全部代码(design of FIR filter )
- 2011-12-07 21:15:24下载
- 积分:1
-
RBF
可用于电力系统短期负荷预测的RBF神经网络程序(Power system can be used for short-term load forecasting procedures of the RBF neural network)
- 2009-04-17 09:25:29下载
- 积分:1
-
costas
使用costas环实现载波同步,绘制出了载波频率跟踪曲线(Achieve carrier synchronization using the costas loop, draw the curve of the carrier frequency tracking)
- 2020-10-12 22:37:34下载
- 积分:1
-
circle
Matlab Code to plot a circle
- 2012-10-22 19:58:03下载
- 积分:1
-
1111
matlab--巴特沃斯高通滤波算法来增强图像(Matlab, butterworth high pass filter algorithm to enhance image)
- 2014-10-16 14:28:53下载
- 积分:1
-
jcs-RBTS
基于交叉熵法的电力系统可靠性分析,需要输入测试系统数据才行哟!(Reliability analysis of cross-entropy-based power systems, test systems need to enter data for the job yo!)
- 2021-04-19 21:28:51下载
- 积分:1
-
MATLAB ABC改进版
说明: 人工蜂群算法(Artificial Bee Colony, ABC)是由Karaboga于2005年提出的一种新颖的基于群智能的全局优化算法,其直观背景来源于蜂群的采蜜行为,蜜蜂根据各自的分工进行不同的活动,并实现蜂群信息的共享和交流,从而找到问题的最优解。对原始算法的改进。(The improvement of the original Artificial Bee Colony.)
- 2020-06-05 16:06:24下载
- 积分:1
-
25811238mimo_ofdm
用于mimo的matlab程序,主要是检测算法,非常有用,大家可以多用用(The matlab program for mimo, mainly detection algorithm, is very useful, we can multi-purpose use)
- 2010-05-18 15:55:04下载
- 积分:1
-
inverter_pwm2
This model demonstrates a DC-AC converter.
3 leg Mosfet operated inverter is constructed .
Can be used to demonstrate the relationship of input DC, output voltage, modulation index , filter selection and switching frequency.
3rd harmonic injection features
- 2013-12-20 14:24:58下载
- 积分:1
-
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