phi derivation
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4
main.py
4
main.py
@@ -14,7 +14,7 @@ def main():
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m = np.array([1., 1., 1e-1],dtype=np.longdouble)*Ms/Ms # Masses in Solar mass
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a = np.array([1., 1., 5.],dtype=np.longdouble)*au/au # Semi-major axis in astronomical units
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e = np.array([0., 0., 0.],dtype=np.longdouble) # Eccentricity
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psi = np.array([0., 0., 45.],dtype=np.longdouble)*np.pi/180. # Inclination of the orbital plane in degrees
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psi = np.array([0., 0., 80.],dtype=np.longdouble)*np.pi/180. # Inclination of the orbital plane in degrees
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x1 = np.array([0., -1., 0.],dtype=np.longdouble)*a[0]*(1.+e[0])
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x2 = np.array([0., 1., 0.],dtype=np.longdouble)*a[1]*(1.+e[1])
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@@ -27,7 +27,7 @@ def main():
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v = np.array([v1, v2, v3],dtype=np.longdouble)
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#integration parameters
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duration, step = 10*yr, np.array([60000.],dtype=np.longdouble) #integration time and step in seconds
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duration, step = 100*yr, np.array([600000.],dtype=np.longdouble) #integration time and step in seconds
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step = np.sort(step)[::-1]
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integrator = "leapfrog"
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n_bodies = 3
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