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with open('somefile.txt', 'a') as f: | |
N = len(a) | |
for i in xrange(N): | |
f.write("%e %e %e\n" %(a[i],b[i],c[i])) |
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import struct | |
with open('somefile.txt', 'a') as f: | |
N = len(a) | |
for i in xrange(N): | |
f.write(struct.pack("f", a[i])) | |
f.write(struct.pack("f", b[i])) | |
f.write(struct.pack("f", c[i])) |
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# Create a directory to work in | |
mkdir rebound | |
cd rebound | |
# Create a virtual environment to work in | |
# (not required, but keeps your python installation clean) | |
virtualenv venv | |
source venv/bin/activate | |
# Install rebound |
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import json | |
import sys | |
if len(sys.argv)!=2: | |
print "Usage: ipynb2py.py FILENAME" | |
exit(1) | |
with open(sys.argv[1]) as data_file: | |
ipynb = json.load(data_file) | |
code = "" |
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/** | |
* A.S. This is my planetesimal disk with special integrator for close encounters. | |
* Particle id's: 0 = star, 1 = massive body, 2 = planetesimal, 3 = CLOSE ENCOUNTER | |
* | |
*/ | |
#include <stdio.h> | |
#include <stdlib.h> | |
#include <unistd.h> | |
#include <math.h> | |
#include <time.h> |
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#!/usr/bin/python | |
from selenium import webdriver | |
import unittest, time, re | |
from random import choice | |
correctanswers = [] | |
def tryitnow (): | |
# Copy and paste the module url below, including the key: |
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%matplotlib inline | |
import matplotlib | |
import numpy as np | |
import matplotlib.pyplot as plt | |
m = np.array([1.0, 3.0404326480226416e-06, 0.0009547919152112404, 0.0002858856727222417]) | |
r = np.array([[0.0, 0.0, 0.0], [-0.5774742940580093, 0.7974401660237153, -2.611328235294271e-05], [-5.2320819021823235, 1.4130269395522546, 0.11120655650204452], [-3.5888816588976513, -9.343800743805208, 0.30528182406879745]]) | |
v = np.array([[0.0, 0.0, 0.0], [-0.8263301482607002, -0.5903562644526552, 2.5048741249552767e-05], [-0.11971493094874505, -0.40317587415621225, 0.00435283234131933], [0.28498977476287424, -0.11757835716481167, -0.009305024058343627]]) | |
plt.xlim([-6,6]) | |
plt.ylim([-6,6]) | |
plt.plot(r[:,0:1],"o",label=["sun"]); |
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t = 0. | |
tmax = 2.*np.pi # corresponds to 1 year | |
steps = 1000 | |
dt = tmax/steps | |
N = len(m) | |
track = np.zeros((steps*N,3)) | |
for k in range(steps): # integrate for one year | |
for i in range(N): #update positions for all particles | |
r[i][0] += dt/2.*v[i][0] | |
r[i][1] += dt/2.*v[i][1] |
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%matplotlib inline | |
import rebound | |
sim = rebound.Simulation() | |
sim.add(["Sun","Earth","Jupiter","Saturn"]) | |
rebound.OrbitPlot(sim); |
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