I am trying to do this homework exercise: Orbit of the Earth
My plot does not show the whole trajectory. I don't know if it is something wrong with my equations or if it is a plotting matter.
Cheers!
import matplotlib.pyplot as plt
import numpy as np
import scipy.integrate as spi
G = 6.6738*10**-11
M = 1.9891*10**30
h = 3600
y = 1.4710*10**11
vx = 3.0287*20**4
def LeapFrog(f, t_start, t_stop, z0, h):
t_vec = np.arange(t_start, t_stop, h)
n = len(t_vec)
d = len(z0)
z_vec = np.zeros((n, d))
z_vec[0,:] = z0
z_half_step=z_vec[0 , :] + (1/2)*h*f(z0,t_vec[0])
for i in range(0, n - 1):
z_vec[i+1,:]=z_vec[i,:] + h*f(z_half_step, t_vec[i])
z_half_step += h*f(z_vec[i+1,:], t_vec[i])
return t_vec, z_vec,
def f(z,t):
x=z[0]
y=z[1]
vx=z[2]
vy=z[3]
r=np.sqrt(x**2+y**2)
dz=np.zeros(4)
dz[0]=vx
dz[1]=vy
dz[2]=-G*M*x/r**3
dz[3]=-G*M*y/r**3
return dz
t_start = 0
t_stop = 24*365*5
z0 = np.array([0,y,vx,0])
t_vec, z_vec = LeapFrog(f, t_start, t_stop, z0, h)
plt.plot(z_vec[:,0],z_vec[:,1], 'g', markersize=1, label='Earth trajectory')
plt.plot(0,0,'yo', label = 'Sun positon')
plt.show()
Okay, so there's a pretty funny typo:
vx = 3.0287*20**4
That's 16 times larger than what you most likely wanted to write and just 20% short of the solar escape velocity.
t_stop
is also written as if in hours, but the rest of the code assumes normal SI seconds (as can be verified by using t_stop = 24 * 365 * 0.99 * h
, which results in almost a complete orbit). It needs multiplying by h
. Sidenote: I like using astropy.units
to keep track of physical quantities!
The code itself works nicely, though!