Tibeuleu/KozaiLidov
1
0
Fork 0
Code Activity

final main

Browse Source
This commit is contained in:
Thibault Barnouin
2022-01-18 22:34:32 +01:00
parent 5168a52ade
commit 81ac7ce307
1 changed files with 3 additions and 3 deletions
Download Patch File Download Diff File Expand all files Collapse all files

6
main.py
View File

@@ -18,7 +18,7 @@ def main():
dtype=np.longdouble)*au # Semi-major axis in astronomical units dtype=np.longdouble)*au # Semi-major axis in astronomical units
e = np.array([0., 0., 0.10], e = np.array([0., 0., 0.10],
dtype=np.longdouble) # Eccentricity dtype=np.longdouble) # Eccentricity
psi = np.array([0., 0., 35.], psi = np.array([0., 0., 80.],
dtype=np.longdouble)*np.pi/180. # Inclination of the orbital plane in degrees dtype=np.longdouble)*np.pi/180. # Inclination of the orbital plane in degrees
x1 = a[0]*(1.+e[0])*np.array([0., -1., 0.], x1 = a[0]*(1.+e[0])*np.array([0., -1., 0.],
@@ -38,14 +38,14 @@ def main():
v = np.array([v1, v2, v3],dtype=np.longdouble) v = np.array([v1, v2, v3],dtype=np.longdouble)
#integration parameters #integration parameters
duration = 2000*yr #integration time in seconds duration = 5000*yr #integration time in seconds
step = np.longdouble(1.0/1.*86400.) #integration step in seconds step = np.longdouble(1.0/1.*86400.) #integration step in seconds
integrator = "leapfrog" integrator = "leapfrog"
n_bodies = 3 n_bodies = 3
display = False display = False
gif = False gif = False
blackstyle = True blackstyle = True
savename = "{0:d}bodies_test_{1:s}".format(n_bodies, integrator) savename = "{0:d}bodies_{1:s}".format(n_bodies, integrator)
display_param = True display_param = True
#simulation start #simulation start