start adimension of problem
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@@ -23,10 +23,10 @@ class Body:
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self.vp = np.zeros(3)
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self.vp = np.zeros(3)
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def __repr__(self): # Called upon "print(body)"
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def __repr__(self): # Called upon "print(body)"
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return "Body of mass: {0:.2e}kg, position: {1}, velocity: {2}".format(self.m, self.q, self.v)
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return r"Body of mass: {0:.2f} $M_\odot$, position: {1}, velocity: {2}".format(self.m, self.q, self.v)
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def __str__(self): # Called upon "str(body)"
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def __str__(self): # Called upon "str(body)"
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return "Body of mass: {0:.2e}kg".format(self.m)
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return r"Body of mass: {0:.2f} $M_\odot$".format(self.m)
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class System:
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class System:
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@@ -35,20 +35,30 @@ class System:
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self.bodylist = np.array(bodylist)
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self.bodylist = np.array(bodylist)
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self.time = 0
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self.time = 0
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@property
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def get_masses(self): #return the masses of each object
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def get_masses(self): #return the masses of each object
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return np.array([body.m for body in self.bodylist])
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return np.array([body.m for body in self.bodylist])
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@property
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def get_positions(self): #return the positions of the bodies
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def get_positions(self): #return the positions of the bodies
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xdata = np.array([body.q[0] for body in self.bodylist])
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xdata = np.array([body.q[0] for body in self.bodylist])
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ydata = np.array([body.q[1] for body in self.bodylist])
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ydata = np.array([body.q[1] for body in self.bodylist])
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zdata = np.array([body.q[2] for body in self.bodylist])
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zdata = np.array([body.q[2] for body in self.bodylist])
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return xdata, ydata, zdata
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return xdata, ydata, zdata
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@property
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def get_velocities(self): #return the positions of the bodies
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def get_velocities(self): #return the positions of the bodies
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return np.array([body.v for body in self.bodylist])
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vxdata = np.array([body.v[0] for body in self.bodylist])
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vydata = np.array([body.v[1] for body in self.bodylist])
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vzdata = np.array([body.v[2] for body in self.bodylist])
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return vxdata, vydata, vzdata
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@property
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def get_momenta(self): #return the momenta of the bodies
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def get_momenta(self): #return the momenta of the bodies
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return np.array([body.p for body in self.bodylist])
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pxdata = np.array([body.p[0] for body in self.bodylist])
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pydata = np.array([body.p[1] for body in self.bodylist])
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pzdata = np.array([body.p[2] for body in self.bodylist])
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return pxdata, pydata, pzdata
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def Mass(self): #return total system mass
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def Mass(self): #return total system mass
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mass = 0
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mass = 0
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@@ -133,7 +143,7 @@ class System:
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E[j] = self.Eval()
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E[j] = self.Eval()
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L[j] = self.Lval()
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L[j] = self.Lval()
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if display and j%100==0:
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if display and j%5==0:
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# display progression
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# display progression
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if len(self.bodylist) == 1:
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if len(self.bodylist) == 1:
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d.on_running(self, step=j, label="step {0:d}/{1:d}".format(j,N))
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d.on_running(self, step=j, label="step {0:d}/{1:d}".format(j,N))
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36
lib/plots.py
36
lib/plots.py
@@ -10,8 +10,8 @@ from lib.units import *
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class DynamicUpdate():
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class DynamicUpdate():
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#Suppose we know the x range
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#Suppose we know the x range
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min_x = -10
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min_x = -1
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max_x = 10
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max_x = 1
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plt.ion()
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plt.ion()
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@@ -64,11 +64,17 @@ class DynamicUpdate():
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self.ax.grid()
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self.ax.grid()
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if self.blackstyle:
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if self.blackstyle:
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self.ax.legend(labelcolor='w', frameon=True, framealpha=0.2)
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self.ax.legend(labelcolor='w', frameon=True, framealpha=0.2)
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self.ax.set_xlabel('AU', color='w')
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self.ax.set_ylabel('AU', color='w')
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self.ax.set_zlabel('AU', color='w')
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else:
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else:
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self.ax.legend()
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self.ax.legend()
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self.ax.set_xlabel('AU')
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self.ax.set_ylabel('AU')
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self.ax.set_zlabel('AU')
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def on_running(self, dyn_syst, step=None, label=None):
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def on_running(self, dyn_syst, step=None, label=None):
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xdata, ydata, zdata = dyn_syst.get_positions()
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xdata, ydata, zdata = dyn_syst.get_positions
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values = np.sqrt(np.sum((np.array((xdata,ydata,zdata))**2).T,axis=1))
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values = np.sqrt(np.sum((np.array((xdata,ydata,zdata))**2).T,axis=1))
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self.min_x, self.max_x = -np.max([np.abs(values).max(),self.max_x]), np.max([np.abs(values).max(),self.max_x])
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self.min_x, self.max_x = -np.max([np.abs(values).max(),self.max_x]), np.max([np.abs(values).max(),self.max_x])
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self.set_lims()
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self.set_lims()
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@@ -88,25 +94,12 @@ class DynamicUpdate():
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#We need to draw *and* flush
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#We need to draw *and* flush
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self.fig.canvas.draw()
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self.fig.canvas.draw()
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self.fig.canvas.flush_events()
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self.fig.canvas.flush_events()
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if not step is None and step%1000==0:
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if not step is None and step%10==0:
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self.fig.savefig("tmp/{0:06d}.png".format(step),bbox_inches="tight")
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self.fig.savefig("tmp/{0:06d}.png".format(step),bbox_inches="tight")
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def close(self):
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def close(self):
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plt.close()
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plt.close()
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#Example
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def __call__(self):
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import numpy as np
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import time
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self.on_launch()
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xdata = []
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ydata = []
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for x in np.arange(0,10,0.5):
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xdata.append(x)
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ydata.append(np.exp(-x**2)+10*np.exp(-(x-7)**2))
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self.on_running(xdata, ydata)
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time.sleep(1)
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return xdata, ydata
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def display_parameters(E,L,parameters,savename=""):
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def display_parameters(E,L,parameters,savename=""):
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"""
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"""
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@@ -116,17 +109,18 @@ def display_parameters(E,L,parameters,savename=""):
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duration, step, dyn_syst, integrator = parameters
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duration, step, dyn_syst, integrator = parameters
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if type(step) != list:
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if type(step) != list:
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step = [step]
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step = [step]
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if (len(E) == duration//step[0]) and (len(L) == duration//step[0]):
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print(E.shape, L.shape)
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if (len(E.shape) == 1) and (len(L.shape) == 2):
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E, L = [E], [L]
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E, L = [E], [L]
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bodies = ""
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bodies = ""
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for body in dyn_syst.bodylist:
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for body in dyn_syst.bodylist:
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bodies += str(body)+" ; "
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bodies += str(body)+" ; "
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title = "Relative difference of the {0:s} "+"for a system composed of {0:s}\n integrated with {1:s} for a duration of {2:.2f} years ".format(bodies, integrator, duration/yr)
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title = "Relative difference of the {0:s} "+"for a system composed of {0:s}\n integrated with {1:s} for a duration of {2:.2f} years ".format(bodies, integrator, duration)
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fig1 = plt.figure(figsize=(15,7))
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fig1 = plt.figure(figsize=(15,7))
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ax1 = fig1.add_subplot(111)
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ax1 = fig1.add_subplot(111)
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for i in range(len(E)):
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for i in range(len(E)):
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ax1.plot(np.arange(E[i].shape[0])*step[i]/yr, np.abs((E[i]-E[i][0])/E[i][0]), label="step of {0:.2e}yr".format(step[i]/yr))
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ax1.plot(np.arange(E[i].shape[0])*step[i], np.abs((E[i]-E[i][0])/E[i][0]), label="step of {0:.2e}yr".format(step[i]))
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ax1.set(xlabel=r"$t (yr)$", ylabel=r"$\left|\frac{\delta E_m}{E_m(t=0)}\right|$", yscale='log')
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ax1.set(xlabel=r"$t (yr)$", ylabel=r"$\left|\frac{\delta E_m}{E_m(t=0)}\right|$", yscale='log')
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ax1.legend()
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ax1.legend()
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fig1.suptitle(title.format("mechanical energy"))
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fig1.suptitle(title.format("mechanical energy"))
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@@ -137,7 +131,7 @@ def display_parameters(E,L,parameters,savename=""):
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for i in range(len(L)):
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for i in range(len(L)):
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dL = ((L[i]-L[i][0])/L[i][0])
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dL = ((L[i]-L[i][0])/L[i][0])
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dL[np.isnan(dL)] = 0.
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dL[np.isnan(dL)] = 0.
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ax2.plot(np.arange(L[i].shape[0])*step[i]/yr, np.abs(np.sum(dL,axis=1)), label="step of {0:.2e}yr".format(step[i]/yr))
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ax2.plot(np.arange(L[i].shape[0])*step[i], np.abs(np.sum(dL,axis=1)), label="step of {0:.2e}yr".format(step[i]))
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ax2.set(xlabel=r"$t (yr)$", ylabel=r"$\left|\frac{\delta \vec{L}}{\vec{L}(t=0)}\right|$",yscale='log')
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ax2.set(xlabel=r"$t (yr)$", ylabel=r"$\left|\frac{\delta \vec{L}}{\vec{L}(t=0)}\right|$",yscale='log')
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ax2.legend()
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ax2.legend()
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fig2.suptitle(title.format("kinetic moment"))
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fig2.suptitle(title.format("kinetic moment"))
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@@ -4,7 +4,7 @@
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Units used in the project.
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Units used in the project.
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"""
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"""
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globals()['G'] = 6.67e-11 #Gravitational constant in SI units
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globals()['Ms'] = 2e30 #Solar mass in kg
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globals()['Ms'] = 2e30 #Solar mass in kg
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globals()['au'] = 1.5e11 #Astronomical unit in m
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globals()['au'] = 1.5e11 #Astronomical unit in m
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globals()['yr'] = 3.15576e7 #year in seconds
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globals()['yr'] = 3.15576e7 #year in seconds
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globals()['G'] = 6.67e-11*yr**2 #Gravitational constant in SI units
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6
main.py
6
main.py
@@ -9,8 +9,8 @@ from lib.units import *
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def main():
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def main():
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#initialisation
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#initialisation
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m = np.array([1., 1., 1e-5])*Ms # Masses in Solar mass
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m = np.array([1., 1., 1e-5])*Ms/Ms # Masses in Solar mass
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a = np.array([1., 1., 5.])*au # Semi-major axis in astronomical units
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a = np.array([1., 1., 5.])*au/au # Semi-major axis in astronomical units
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e = np.array([0., 0., 1./4.]) # Eccentricity
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e = np.array([0., 0., 1./4.]) # Eccentricity
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psi = np.array([0., 0., 0.])*np.pi/180. # Inclination of the orbital plane in degrees
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psi = np.array([0., 0., 0.])*np.pi/180. # Inclination of the orbital plane in degrees
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@@ -25,7 +25,7 @@ def main():
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v = np.array([v1, v2, v3])
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v = np.array([v1, v2, v3])
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#integration parameters
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#integration parameters
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duration, step = 100*yr, [1e4, 1e5]
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duration, step = 100*yr/yr, np.array([1./(365.25*2.), 1./365.25])*yr/yr #integration time and step in years
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integrator = "leapfrog"
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integrator = "leapfrog"
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n_bodies = 2
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n_bodies = 2
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display = False
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display = False
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