📄 isodop.m
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% PLOT OF CONSTANT DOPPLER CONTOURS - ISODOPS
% -------------------------------------------
clear;clc;clf;
% Set Aircraft Parameters
ro=.1; % vg/vac ratio
h=10000; % feet
% Calculate Doppler Contour
for i=1:9;
rr=ro+.1*(i-1);
phi=acos(rr); % depression angle
a=tan(phi);
xmin=h/a+1e-3;
x=xmin:30000;
y1=sqrt(a^2*x.^2-h^2);
q=1:xmin;
Ay=zeros(size(q));
Ay1=[Ay y1];
% Plot Doppler Contour
Ax=xmin*ones(size(q));
x1=[Ax x];
plot(x1,Ay1,'k',x1,-Ay1,'k',-x1,Ay1,'k',-x1,-Ay1,'k');
grid;axis([-3e4 3e4 -5e4 5e4]);hold on;
end;hold off;
title('Constant Doppler Contours - Isodops');
xlabel('Ground Track Range - feet');
ylabel('Cross Track Range - feet');
text(2.5e4,.2e4,'Ground Track');
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