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KozaiLidov/main.py
2021-11-14 00:13:35 +01:00

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Python
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#!/usr/bin/python
# -*- coding:utf-8 -*-
from sys import exit as sysexit
import numpy as np
import matplotlib.pyplot as plt
from lib.objects import Body, System
from lib.plots import display_parameters
from lib.units import *
def main():
#initialisation
m = np.array([1., 1., 1e-5])*Ms # Masses in Solar mass
a = np.array([1., 1., 5.])*au # Semi-major axis in astronomical units
e = np.array([0., 0., 1./4.]) # Eccentricity
psi = np.array([0., 0., 0.])*np.pi/180. # Inclination of the orbital plane in degrees
x1 = np.array([0., -1., 0.])*a[0]
x2 = np.array([0., 1., 0.])*a[1]
x3 = np.array([np.cos(psi[2]), 0., np.sin(psi[2])])*a[2]
q = np.array([x1, x2, x3])
v1 = np.array([np.sqrt(G*m[1]**2/((m[0]+m[1])*np.sqrt(np.sum((q[0]-q[1])**2)))), 0., 0.])
v2 = np.array([-np.sqrt(G*m[0]**2/((m[0]+m[1])*np.sqrt(np.sum((q[0]-q[1])**2)))), 0., 0.])
v3 = np.array([0., np.sqrt(G*(m[0]+m[1])*(2./np.sqrt(np.sum(q[2]**2))-1./a[2])), 0.])
v = np.array([v1, v2, v3])
bodylist = []
for i in range(3):
bodylist.append(Body(m[i], q[i], v[i]))
dyn_syst = System(bodylist)
dyn_syst.COMShift()
duration, step1, step2 = 100*yr, 1e4, 1e5
E1, L1 = dyn_syst.leapfrog(duration, step1, recover_param=True, display=True)
E2, L2 = dyn_syst.leapfrog(duration, step2, recover_param=True)#, display=True)
#E1, L1 = dyn_syst.hermite(duration, step1, recover_param=True)#, display=True)
#E2, L2 = dyn_syst.hermite(duration, step2, recover_param=True)#, display=True)
parameters = [duration, [step1, step2], dyn_syst, "leapfrog"]
display_parameters([E1, E2], [L1, L2], parameters=parameters, savename="3bodies_mass_leapfrog")
return 0
if __name__ == '__main__':
sysexit(main())