How do I animate a 3d plot of a satellite orbit given its' orbital parameters.
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The plot function that made is the following:
function plotOrbit(a, e, i, OM, om, mu)
% a, e, i, OM, om are the orbital parameters
% mu = 3.986*10^5 (Earth's gravitational parameter)
r_vect = [];
v_vect = [];
for th = 0: 0.01: (2*pi + 0.01)
% par2car is an .m file that uses the orbital parameters to obtain
% the position and velocity vectors.
[rr, vv] = par2car(a, e, i, OM, om, th, mu);
r_vect = [r_vect; rr'];
end
plot3(r_vect(:, 1), r_vect(:, 2), r_vect(:, 3))
end
I would like to have a moving point along the orbit which varies it's velocity over time.
1 件のコメント
Henrique Chaves
2021 年 10 月 19 日
@E. Miguel Reiner Santos Sorry for bother you, but i want to make something similiar to you.
Can you make available your code please?
Thanks !
回答 (2 件)
Srivardhan Gadila
2020 年 10 月 28 日
The following is the example code based on the above functions:
1. If you want the point moving i.e., new point to appear and previous point to disappear:
figure
for i = 1:10
plot3(i,abs(sqrt(100-i^2)),5,'o');
xlim([0 10])
ylim([0 10])
zlim([0 10])
% hold on
pause(1)
end
% hold off
2. If you want all the previous points to appear in the plot as well:
figure
for i = 1:10
plot3(i,abs(sqrt(100-i^2)),5,'o');
xlim([0 10])
ylim([0 10])
zlim([0 10])
hold on
pause(1)
end
hold off
0 件のコメント
Matteo Marzorati
2021 年 12 月 8 日
you can use Matlab function comet3(X,Y,Z), where the 3 inputs are the vectors that define the orbit
0 件のコメント
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