Ejemplo n.º 1
0
def integrate_solar_system(sun, planets, time_end=5.0 | units.yr, n_steps=500):
    """
  evolve the system using kepler_orbiters
  """

    converter = nbody_system.nbody_to_si(1 | units.MSun, 1 | units.AU)

    planets_around_sun = Kepler(converter, channel_type="sockets")

    # central particle
    planets_around_sun.central_particle.add_particles(sun[0:1])

    # to set the central particle at the center of the coordinate system
    #planets_around_sun.central_particle.position = (0.0, 0.0, 0.0) | units.AU
    #planets_around_sun.central_particle.velocity = (0.0, 0.0, 0.0) | units.kms

    # orbiters
    planets_around_sun.orbiters.add_particles(planets)
    planets_around_sun.commit_particles()

    # to change the integration method
    #planets_around_sun.parameters.method = 1
    #print planets_around_sun.get_method()

    channel_from_planetets_to_framework = planets_around_sun.orbiters.new_channel_to(
        planets)
    channel_from_sun_to_framework = planets_around_sun.central_particle.new_channel_to(
        sun)

    positions_sun = quantities.AdaptingVectorQuantity()
    positions_planets = quantities.AdaptingVectorQuantity()

    dt = time_end / float(n_steps)
    time = 0.0 | units.yr

    print " ** evolving solar system for", time_end.in_(
        units.yr), ", with time-step of", dt.in_(units.yr)
    print "    this might take a while"
    while time <= time_end:
        #print "\t", time.in_(units.yr)
        planets_around_sun.evolve_model(time)
        channel_from_planetets_to_framework.copy()
        channel_from_sun_to_framework.copy()
        positions_sun.append(sun.position)
        positions_planets.append(planets.position)
        time += dt
    print " **"

    planets_around_sun.stop()

    return positions_sun, positions_planets
Ejemplo n.º 2
0
    def test1(self):
        convert_nbody = nbody_system.nbody_to_si(1.0 | units.MSun,
                                                 149.5e6 | units.km)
        instance = Kepler(
            convert_nbody)  #, redirection="none")#, debugger="xterm")
        instance.initialize_code()

        stars = self.new_system_of_sun_and_earth()
        earth = stars[1]

        instance.central_particle.add_particle(stars[0])
        earth = instance.orbiters.add_particle(stars[1])
        instance.commit_particles()

        instance.evolve_model(365 | units.day)

        instance.particles.copy_values_of_all_attributes_to(stars)

        position_at_start = earth.position.value_in(units.AU)[0]
        position_after_full_rotation = earth.position.value_in(units.AU)[0]
        self.assertAlmostEqual(position_at_start, position_after_full_rotation,
                               6)

        instance.evolve_model(365.0 + (365.0 / 2) | units.day)

        instance.particles.copy_values_of_all_attributes_to(stars)
        position_after_half_a_rotation = earth.position.value_in(units.AU)[0]
        self.assertAlmostEqual(-position_at_start,
                               position_after_half_a_rotation, 3)

        instance.evolve_model(365.0 + (365.0 / 2) + (365.0 / 4) | units.day)

        instance.particles.copy_values_of_all_attributes_to(stars)
        position_after_half_a_rotation = earth.position.value_in(units.AU)[1]
        self.assertAlmostEqual(-position_at_start,
                               position_after_half_a_rotation, 3)

        instance.cleanup_code()

        instance.stop()
Ejemplo n.º 3
0
    def test1(self):
        convert_nbody = nbody_system.nbody_to_si(1.0 | units.MSun, 149.5e6 | units.km)
        instance = Kepler(convert_nbody)#, redirection="none")#, debugger="xterm")
        instance.initialize_code()

        
        stars = self.new_system_of_sun_and_earth()
        earth = stars[1]

        instance.central_particle.add_particle(stars[0])
        earth = instance.orbiters.add_particle(stars[1])
        instance.commit_particles()

        instance.evolve_model(365 | units.day)

        instance.particles.copy_values_of_all_attributes_to(stars)
        
        position_at_start = earth.position.value_in(units.AU)[0]
        position_after_full_rotation = earth.position.value_in(units.AU)[0]
        self.assertAlmostEqual(position_at_start, position_after_full_rotation, 6)
        
        instance.evolve_model(365.0 + (365.0 / 2) | units.day)
        
        instance.particles.copy_values_of_all_attributes_to(stars)
        position_after_half_a_rotation = earth.position.value_in(units.AU)[0]
        self.assertAlmostEqual(-position_at_start, position_after_half_a_rotation, 3)
                
        instance.evolve_model(365.0 + (365.0 / 2) + (365.0 / 4)  | units.day)
        
        instance.particles.copy_values_of_all_attributes_to(stars)
        position_after_half_a_rotation = earth.position.value_in(units.AU)[1]
        self.assertAlmostEqual(-position_at_start, position_after_half_a_rotation, 3)
        
        instance.cleanup_code()
        
        instance.stop()
Ejemplo n.º 4
0
 def test0(self):
     instance = Kepler()
     instance.stop()
Ejemplo n.º 5
0
 def test0(self):
     instance = Kepler()
     instance.stop()