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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