Exemplo n.º 1
0
    def example2(self):
        """
        Lidov-Kozai problem of a planet around a star around a supermassive black hole.
        Includes perturbations from other stars in the form of vector resonant relaxation (VRR)
        
        """

        code = SecularMultiple()  ### initialize the code
        CONST_G = code.CONST_G  ### extract physical constants from the code
        CONST_C = code.CONST_C
        CONST_R_SUN = code.CONST_R_SUN
        RJup = 0.1027922358015816 * CONST_R_SUN
        MJup = 0.0009546386983890755
        day = 1.0 / 365.25
        second = day / (24.0 * 3600.0)
        meter = 1.0 / 1.496e+11

        ### Input parameters ###
        m1 = 1.0
        m2 = MJup
        m3 = 4.0e6

        a1 = 1.0e-1
        a2 = 1.0e4
        e1 = 0.01
        e2 = 0.1
        i1 = 4.5 * np.pi / 180.0
        i2 = 19.9 * np.pi / 180.0
        AP1 = np.pi
        AP2 = 0.38 * np.pi
        LAN1 = 0.01
        LAN2 = np.pi

        R1 = 1.0 * CONST_R_SUN
        R2 = 1.0 * RJup
        R3 = CONST_G * m3 / (CONST_C**2)

        m_star = 1.0
        gamma = 3.0 / 2.0
        VRR_model = 3

        ### Simulation parameters ###
        VRR_include_mass_precession = True
        include_inner_1PN_terms = True
        include_outer_1PN_terms = True

        ### Process parameters ###
        P1 = 2.0 * np.pi * np.sqrt(a1**3 / (CONST_G * (m1 + m2)))
        P2 = 2.0 * np.pi * np.sqrt(a2**3 / (CONST_G * (m1 + m2 + m3)))

        masses = [m1, m2, m3]
        radii = [R1, R2, R3]
        semimajor_axes = [a1, a2]
        eccentricities = [e1, e2]
        inclinations = [i1, i2]
        APs = [AP1, AP2]
        LANs = [LAN1, LAN2]

        N = len(masses)
        particles = Tools.create_nested_multiple(N,
                                                 masses,
                                                 semimajor_axes,
                                                 eccentricities,
                                                 inclinations,
                                                 APs,
                                                 LANs,
                                                 radii=radii)
        orbits = [x for x in particles if x.is_binary == True]
        N_orbits = len(orbits)

        inner_orbit = orbits[0]
        outer_orbit = orbits[1]

        c1 = 4.8
        c2 = -2.9
        log10_sigma_h_km_s = (np.log10(m3) - c2) / c1

        sigma_h_km_s = pow(10.0, log10_sigma_h_km_s)
        sigma_h = 1.0e3 * sigma_h_km_s * meter / second
        print('sigma_h_km_s', sigma_h_km_s, 'sigma_h', sigma_h)

        #       K_12 = K_12_function(gamma)
        #        K_32 = K_32_function(gamma)
        #        C_NRR = ((3.0*numpy.pi)/(64.0))*1.0/( K_12 - (1.0/5.0)*K_32 + (5.0*numpy.pi/8.0)*(1.0/(2.0*gamma-1.0)) )

        r_h = CONST_G * m3 * (1.0 / (sigma_h**2 *
                                     (1.0 + gamma))) * (1.0 + (1.0 + gamma) /
                                                        (gamma - 1.0))

        r_0 = r_h
        n_0 = (2.0 * m3 / m_star) * ((3.0 - gamma) / (4.0 * np.pi * r_h**3))

        r = a2
        rho_star = compute_rho_star_r(r, gamma, n_0, r_0, m_star)
        n_star = compute_n_star_r(r, gamma, n_0, r_0, m_star)
        M_star = compute_M_star_r(r, gamma, n_0, r_0, m_star)
        N_star = compute_N_star_r(r, gamma, n_0, r_0, m_star)
        sigma_r = compute_sigma_r(r, gamma, n_0, r_0, m_star, m3, CONST_G)

        print('n_star', n_star, 'M_star', M_star, 'N_star', N_star, 'sigma_r',
              sigma_r)

        LK_timescale = (P2**2 / P1) * (
            (m1 + m2 + m3) / m3) * pow(1.0 - e2**2, 3.0 / 2.0)
        print('LK_timescale', LK_timescale)
        VRR_mass_precession_timescale = (1.0 / 2.0) * pow(
            1.0 - e2**2, -1.0 / 2.0) * (m3 / M_star) * P2
        VRR_mass_precession_rate = 1.0 / VRR_mass_precession_timescale
        VRR_timescale = (P2 / 2.0) * (m3 / m_star) * 1.0 / np.sqrt(N_star)
        #VRR_timescale *= 0.1

        print('VRR_mass_precession_timescale', VRR_mass_precession_timescale,
              'VRR_timescale', VRR_timescale)

        outer_orbit.VRR_include_mass_precession = VRR_include_mass_precession
        outer_orbit.VRR_mass_precession_rate = VRR_mass_precession_rate

        VRR_reorientation_timestep = np.sqrt(0.1) * VRR_timescale
        print('VRR_reorientation_timestep', VRR_reorientation_timestep)

        outer_orbit.VRR_model = VRR_model
        reorientation_function(VRR_model, VRR_timescale,
                               VRR_reorientation_timestep, outer_orbit)

        v_bin = np.sqrt(CONST_G * (m1 + m2) / a1)
        q_sigma = (m1 + m2) / m_star
        log_Lambda = np.log(3.0 * ((1.0 + 1.0 / q_sigma) /
                                   (1.0 + 2.0 / q_sigma)) * sigma_r**2 /
                            v_bin**2)
        evaporation_timescale = np.sqrt(
            (1.0 + q_sigma) /
            (2.0 * np.pi * q_sigma)) * (m1 + m2) * sigma_r / (8.0 * np.sqrt(
                np.pi) * CONST_G * a1 * m_star**2 * n_star * log_Lambda)
        print('evaporation_timescale', evaporation_timescale)

        inner_orbit.include_1PN_terms = include_inner_1PN_terms
        outer_orbit.include_1PN_terms = include_outer_1PN_terms
        code.add_particles(particles)
        primary = code.particles[0]

        code.enable_tides = False
        code.enable_root_finding = True
        code.enable_VRR = True

        a_AU_print = [[] for x in range(N_orbits)]
        e_print = [[] for x in range(N_orbits)]
        INCL_print = [[] for x in range(N_orbits)]
        rel_INCL_print = [[] for x in range(N_orbits)]
        t_print = []

        t = 0.0
        Nsteps = 1000
        tend = evaporation_timescale
        dt_fixed = tend / float(Nsteps)
        t_next_reorientation = VRR_reorientation_timestep

        import time
        start = time.time()
        while t <= tend:
            dt = dt_fixed
            if t + dt > t_next_reorientation:
                dt = t_next_reorientation - t
                t_next_reorientation += VRR_reorientation_timestep

                reorientation_function(VRR_model, VRR_timescale,
                                       t_next_reorientation, outer_orbit)

            t += dt
            code.evolve_model(t)

            print('t', t, 'es', [o.e for o in orbits], 'Omegas',
                  [o.LAN for o in orbits])
            for i in range(N_orbits):
                rel_INCL_print[i].append(orbits[i].INCL_parent)
                a_AU_print[i].append(orbits[i].a)
                e_print[i].append(orbits[i].e)
                INCL_print[i].append(orbits[i].INCL)
            t_print.append(t)

        print('wall time', time.time() - start)

        t_print = np.array(t_print)
        for i in range(N_orbits):
            INCL_print[i] = np.array(INCL_print[i])
            rel_INCL_print[i] = np.array(rel_INCL_print[i])
            e_print[i] = np.array(e_print[i])
            a_AU_print[i] = np.array(a_AU_print[i])

        from matplotlib import pyplot
        fig = pyplot.figure(figsize=(8, 8))
        plot1 = fig.add_subplot(2, 1, 1, yscale="log")
        plot2 = fig.add_subplot(2, 1, 2, yscale="linear")
        colors = ['k', 'r', 'g']
        for i in range(N_orbits):
            color = colors[i]
            plot1.plot(1.0e-6 * t_print, a_AU_print[i], color=color)
            plot1.plot(1.0e-6 * t_print,
                       a_AU_print[i] * (1.0 - e_print[i]),
                       color=color)
            plot1.plot(1.0e-6 * t_print,
                       a_AU_print[i] * (1.0 + e_print[i]),
                       color=color)
            #plot2.plot(1.0e-6*t_print,INCL_print[i]*180.0/np.pi,color=color,linestyle='dotted')
            plot2.plot(1.0e-6 * t_print,
                       rel_INCL_print[i] * 180.0 / np.pi,
                       color=color)

            plot1.set_xlabel("$t/\mathrm{Myr}$")
            plot2.set_xlabel("$t/\mathrm{Myr}$")
            plot1.set_ylabel("$r_i/\mathrm{AU}$")
            plot2.set_ylabel("$\mathrm{incl}_\mathrm{rel}/\mathrm{deg}$")
        fig.savefig("example2.pdf")
        pyplot.show()
Exemplo n.º 2
0
def run_simulation(tend,Nsteps,particles, \
    VRR_reorientation_timestep,VRR_model,VRR_timescale,outer_orbit, \
    enable_tides=False,enable_root_finding=True,enable_VRR=True):
    code = SecularMultiple()  ### initialize the code

    code.add_particles(particles)
    primary = code.particles[0]

    code.enable_tides = enable_tides
    code.enable_root_finding = enable_root_finding
    code.enable_VRR = enable_VRR

    orbits = [x for x in particles if x.is_binary == True]
    N_orbits = len(orbits)

    a_AU_print = [[] for x in range(N_orbits)]
    e_print = [[] for x in range(N_orbits)]
    rp_AU_print = [[] for x in range(N_orbits)]
    INCL_print = [[] for x in range(N_orbits)]
    rel_INCL_print = [[] for x in range(N_orbits)]
    t_print = []

    t = 0.0

    dt_fixed = tend / float(Nsteps)
    t_next_reorientation = VRR_reorientation_timestep

    found_root = False
    import time
    start = time.time()
    while t <= tend:
        dt = dt_fixed
        if t + dt > t_next_reorientation:
            dt = t_next_reorientation - t
            t_next_reorientation += VRR_reorientation_timestep

            reorientation_function(VRR_model, VRR_timescale,
                                   t_next_reorientation, outer_orbit)

        t += dt
        code.evolve_model(t)

        #print 't',t,'es',[o.e for o in orbits],'Omegas',[o.LAN for o in orbits]

        if code.flag == 2:
            t = code.model_time
            print 'root found at t=', t
            found_root = True

        for i in range(N_orbits):
            rel_INCL_print[i].append(orbits[i].INCL_parent)
            a_AU_print[i].append(orbits[i].a)
            e_print[i].append(orbits[i].e)
            INCL_print[i].append(orbits[i].INCL)
            rp_AU_print[i].append(orbits[i].a * (1.0 - orbits[i].e))
        t_print.append(t)

        if found_root == True:
            break

    print 'wall time', time.time() - start

    t_print = np.array(t_print)
    for i in range(N_orbits):
        INCL_print[i] = np.array(INCL_print[i])
        rel_INCL_print[i] = np.array(rel_INCL_print[i])
        e_print[i] = np.array(e_print[i])
        a_AU_print[i] = np.array(a_AU_print[i])
        rp_AU_print[i] = np.array(rp_AU_print[i])

    code.reset()

    data = found_root, t_print, rel_INCL_print, e_print, a_AU_print, rp_AU_print

    return data