Created
October 1, 2014 20:48
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Plotting satellite orbits with Gnuplot
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r(p,e,f) = p/(1.0 + e * cos(f)) | |
orbit_x(p,e,i,an,argp,f) = \ | |
r(p,e,f) * (\ | |
cos(f) * ((cos(argp) * cos(an)) - (sin(argp) * sin(an) * cos(i))) + \ | |
sin(f) * (-(cos(argp) * sin(an) * cos(i)) - (sin(argp) * cos(an)))) | |
orbit_y(p,e,i,an,argp,f) = \ | |
r(p,e,f) * (\ | |
cos(f) * ((sin(argp) * cos(an) * cos(i)) + (cos(argp) * sin(an))) + \ | |
sin(f) * ((cos(argp) * cos(an) * cos(i)) - (sin(argp) * sin(an)))) | |
orbit_z(p,e,i,an,argp,f) = \ | |
r(p,e,f) * (\ | |
cos(f) * (sin(argp) * sin(i)) + \ | |
sin(f) * (cos(argp) * sin(i))) | |
set view equal xyz | |
set parametric | |
set key off | |
set grid | |
p1 = 1.0 | |
e1 = 0.0 | |
i1 = 0.0 | |
an1 = 0.0 | |
argp1 = 0.0 | |
p2 = 1.0 | |
e2 = 0.7 | |
i2 = pi/4 | |
an2 = 0.0 | |
argp2 = 0.0 | |
splot \ | |
orbit_x(p1,e1,i1,an1,argp1,u), \ | |
orbit_y(p1,e1,i1,an1,argp1,u), \ | |
orbit_z(p1,e1,i1,an1,argp1,u) \ | |
title "Orbit 1", \ | |
orbit_x(p2,e2,i2,an2,argp2,u), \ | |
orbit_y(p2,e2,i2,an2,argp2,u), \ | |
orbit_z(p2,e2,i2,an2,argp2,u) \ | |
title "Orbit 2" |
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