def add_comets(star, m_comets, n_comets, q_min, a_min, a_max, seed):
    #bodies.position -= star.position
    #bodies.velocity -= star.velocity

    cloud_xyz = generate_initial_oort_cloud(star.mass, n_comets, q_min, a_min,
                                            a_max, seed)
    masses = new_salpeter_mass_distribution(n_comets, 0.1 | units.MSun,
                                            100 | units.MSun)
    masses = m_comets * masses / masses.sum()
    print("total mass in comets: M=", masses.sum().in_(units.MEarth))

    comets = Particles(n_comets)
    comets.mass = masses
    comets.name = "comet"
    comets.host = star
    comets.x = cloud_xyz[:, 2] | units.au
    comets.y = cloud_xyz[:, 3] | units.au
    comets.z = cloud_xyz[:, 4] | units.au
    comets.vx = cloud_xyz[:, 5] | 2 * numpy.pi * units.au / units.yr
    comets.vy = cloud_xyz[:, 6] | 2 * numpy.pi * units.au / units.yr
    comets.vz = cloud_xyz[:, 7] | 2 * numpy.pi * units.au / units.yr

    comets.position += star.position
    comets.velocity += star.velocity

    return comets
Exemplo n.º 2
0
def construct_particle_set_from_orbital_elements(name,
                                                 mass,
                                                 a,
                                                 ecc,
                                                 inc,
                                                 Ma,
                                                 Aop,
                                                 LoAn,
                                                 Mparent=1 | units.MSun):

    print("length:", len(a), len(ecc), len(inc), len(Ma), len(Aop), len(LoAn),
          len(name))

    p = Particles(len(a))
    print(name)
    p.name = name
    p.type = "asteroid"
    p.host = "Sun"
    p.mass = mass
    from orbital_elements_to_cartesian import orbital_elements_to_pos_and_vel
    from orbital_elements_to_cartesian import orbital_period

    from amuse.ext.orbital_elements import new_binary_from_orbital_elements
    for i in range(len(p)):
        Ta = True_anomaly_from_mean_anomaly(numpy.rad2deg(Ma[i]), ecc[i])
        b = new_binary_from_orbital_elements(Mparent,
                                             p[i].mass,
                                             a[i],
                                             ecc[i],
                                             Ta,
                                             inc[i],
                                             LoAn[i],
                                             Aop[i],
                                             G=constants.G)
        p[i].position = b[1].position - b[0].position
        p[i].velocity = b[1].velocity - b[0].velocity

        rho = 2.0 | units.g / units.cm**3
        p.radius = (p.mass / rho)**(1. / 3.)

    return p