Home Intro Basic Concept Comm-Link System Design Satellite Orbit Cost References

orbits.m
clear
clc
close all
format compact


run distances

[x3, y3, z3] = sphere;
surf(x3.*rmars, y3.*rmars, z3.*rmars);


theta = [0:.01:2*pi];

phi(1:numel(theta)) = 0;

r(1:numel(theta)) = R_GMO+rmars;

[x, y, z] = sph2cart(theta,phi, r);

hold on
plot3(x, y, z, '-yo')
axis equal

comet3(x,y,z)
dist_sats =
   3.5382e+07
beamwidth_sat =
   22.5609
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