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homeword2-06
Matlab源码，仿真飞机姿态更新，主要是捷联惯导的姿态更新(Matlab source code, simulation of aircraft attitude update, mainly SINS attitude update)
- 2010-06-02 13:03:37下载
- 积分：1
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aishwarya
gives an control scheme of the wind enery system
- 2015-03-24 22:41:39下载
- 积分：1
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MIMO
mimo信道容量分析mimo信道容量分析mimo信道容量分析mimo信道容量分析(mimo channel capacity analysismimo channel capacity analysismimo channel capacity analysismimo channel capacity analysis)
- 2014-11-03 20:16:02下载
- 积分：1
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AR模型预测
AR模型预测 模型阶数的确定 以及误差分析计算 相关例子(AR model order to determine the AR forecasts and error analysis)
- 2020-07-07 11:58:57下载
- 积分：1
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QPSKgray
Rayleigh multipath/AWGN(Additive White Gaussian Noise)
QPSK Gray used
- 2009-12-12 21:27:39下载
- 积分：1
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work
关于三相SVPWM仿真的模型，我做电力电子仿真作业的一道题，花了很多时间下载和阅读文献，最后总算成功了，只是仿的结果有点慢，一直找不到为什么。
注意：此模型仿真时需要svpwm.m这个文件，并且matlab软件版本为Matlab7.1。(About three-phase SVPWM simulation model, I do the job of power electronic simulation of a question, spend a lot of time to download and read the literature, but finally succeeded, but the result of imitation of a little slow, could not find why. Note: This model simulation requires svpwm.m this file and matlab software version Matlab7.1.)
- 2011-04-25 16:53:53下载
- 积分：1
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FCM2
a new version of implemented FCM on matlab
- 2013-03-13 02:42:18下载
- 积分：1
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objectTracking.m
kalman filter for traking a moving object
- 2009-05-16 14:30:53下载
- 积分：1
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myQPSK
蒙特卡洛QPSK编码，画出星座图（含噪声）并将模拟误码率与理论值比较(Monte Carlo QPSK encoding, constellation diagram drawn (including noise) and simulated bit error rate compared with the theoretical value)
- 2009-06-03 13:10:10下载
- 积分：1
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equal-area-critirea
E=input( enter the generator voltage: )
V=input( enter the infinite bus voltage: )
Gx=input( enter the reactance of generator: )
L1x=input( enter the line reactance: )
L2x=input( enter the line reactance: )
L3x=input( enter the line reactance: )
L4x=input( enter the line reactance: )
Pi=input( enter the input power: )
X1=Gx+L1x+((L2x*L3x)/(L2x+L3x))+L4x
Pm1=E*V/X1
DO=asin(Pi/Pm1)
A=((L2x*L3x)/(2*(L2x+L3x)))
C=A
B=((L3x/2)^2)/(L2x+L3x)
X2=(Gx+L1x+A)+(L4x+A)+(Gx+L1x+A)*(A+L4x)/B
Pm2=(E*V)/X2
X3=Gx+L1x+L2x+L4x
Pm3=(E*V)/X3
DC=input( enter the fault clearing angle: )
Dm=(3.14-asin(Pi/Pm3))
a1=quad( sin ,DO,DC)
A1=(Pi*(DC-DO)-Pm2*a1)
a2=quad( sin ,DC,Dm)
A2=Pm3*a2-Pi*(Dm-DC)
if(A2>=A1)
disp( the system is stable )
else
disp( the system is unstable )
end
Dcc=acos((Pi*(Dm-DO)-Pm2*(cos(DO))+Pm3*(cos(Dm)))/(Pm3-Pm2))
disp( critical clearing angle: )
Dcc
- 2012-09-11 22:46:05下载
- 积分：1
