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sa_fig6_25.m
% Angular distribution for a circle of scatterers
thmax=pi/4;
th=-pi/4:pi/400:pi/4;
f=2*sqrt(thmax^2-th.^2)/thmax^2;
figure;
plot(th*180/pi,f,'k')
xlabel('Arrival Angle')
Ylabel('PAP')
axis(
sa_fig4_24.m
% Smart Antennas figure4.24 plotting elevation plane pattern
a=1;
N=10;
pinc=2*pi/N;
th=-pi/2:.01:pi/2;
th0=pi/6;
ph0=0;
AF=zeros(1,length(th));
for n=1:N
AF=AF+exp(-1j*2*pi*a*(sin(th
sa_fig6_22.m
% Angular distribution for a circle of scatterers
thmax=pi/4;
th=-pi/4+.01:.001:pi/4-.01;
f=1./sqrt(thmax^2-th.^2);
figure;
plot(th*180/pi,f,'k')
xlabel('Arrival Angle')
Ylabel('PAP')
axis([
sa_fig6_27.m
% Angular distribution for a circle of scatterers
sigth=pi/6;
th=-pi/2:pi/400:pi/2;
f=pi*exp(-abs(th*sqrt(2)/sigth))/(sqrt(2)*sigth);
figure;
plot(th*180/pi,f,'k')
xlabel('Arrival Angle')
Yla
sa_fig3_6.m
% Smart Antennas figure 3.6 plotting array factor in rectangular and polar coordinates.
set(0,'defaultfigurecolor','w')
N=12;
d=.25;
th=-pi/2:.01:pi/2;
an=th*180/pi;
AF2=abs(sin(N*pi*d*sin(th)
sa_fig3_1x.m
% Smart antennas 3-D pattern for loop antennas with radius a
% use 100 data points in theta and 100 data points in phi
set(0,'defaultfigurecolor','w')
tend=pi;
%a is inserted below before the pi
sa_fig8_3.m
%Godara Method
% Example 8.1
d=.5;
N=3;
theta=-pi/2:.01:pi/2;
ang=theta*180/pi;
th0=0; % receive angle
th1=-45*pi/180; % first interferer angle
th2=60*pi/180; % secon
sa_fig4_28.m
%kaiser weighted planar square array. N elements in the x and in the y directions
% spacing dx=dy=d. Kaiser bessel weights with alpha=3.
% Beamsteered to theta0=45, phi0=45.
d=.5;
N=16;
sa_fig8_32.m
% This is a simulation to model the Elam SDMA technique
% Developed by Frank B. Gross, November 11, 2004
% define the sample baseband modulation initially as a 1kHz phase modulation tone
% WAL
sa_fig4_27.m
%Smart Antennas Figure 4.27 kaiser weighted planar square array.
% N elements in the x and in the y directions
% spacing dx=dy=d. Kaiser bessel weights with alpha=3.
% Beamsteered to the