using matlab simulate the orbit of famous halley’s comet. note that comet’s eccentricity and semimajor axis are 0.96658 and 17.737au, respectively. in matlab

To simulate the orbit of Halley's comet using MATLAB, you can use the built-in functions and algorithms for orbital mechanics. Here's how you can do it:

  1. Define the orbital parameters of Halley's comet:
main.m
eccentricity = 0.96658;
semimajor_axis = 17.737; % in astronomical units (AU)
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  1. Set up the simulation time:
main.m
time_span = 100; % in years
time_step = 0.01; % in years
t = 0:time_step:time_span;
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  1. Calculate the mean anomaly:
main.m
mean_motion = 2 * pi / (semimajor_axis ^ (3 / 2)); % in 1/year
mean_anomaly = mean_motion * t;
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  1. Calculate the eccentric anomaly using the mean anomaly and eccentricity:
main.m
eccentric_anomaly = fzero(@(E) E - eccentricity * sin(E) - mean_anomaly, mean_anomaly);
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  1. Calculate the true anomaly using the eccentric anomaly and eccentricity:
main.m
true_anomaly = 2 * atan(sqrt((1 + eccentricity) / (1 - eccentricity)) * tan(eccentric_anomaly / 2));
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  1. Calculate the distance from the sun to Halley's comet (r):
main.m
r = semimajor_axis * (1 - eccentricity^2) ./ (1 + eccentricity * cos(true_anomaly));
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  1. Convert the polar coordinates to Cartesian coordinates:
main.m
x = r .* cos(true_anomaly);
y = r .* sin(true_anomaly);
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  1. Plot the orbit:
main.m
plot(x, y);
xlabel('x (AU)');
ylabel('y (AU)');
title('Orbit of Halley''s Comet');
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By running the above code, you will get a plot showing the orbit of Halley's comet over the specified time span. Adjusting the time_span and time_step variables will allow you to simulate the orbit over a longer or shorter time period with finer or coarser resolution.

Note that this simulation assumes a simplified two-dimensional orbit and does not account for gravitational perturbations from other celestial bodies or relativistic effects.

I hope this helps you simulate the orbit of Halley's comet using MATLAB!

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