Integrating and plotting an orbit in an NFW potentialΒΆ
We first need to import some relevant packages:
>>> import astropy.units as u
>>> import numpy as np
>>> import gala.integrate as gi
>>> import gala.dynamics as gd
>>> import gala.potential as gp
>>> from gala.units import galactic
In the examples below, we will work use the galactic
UnitSystem
:
as I define it, this is: \({\rm kpc}\), \({\rm Myr}\), \({\rm M}_\odot\).
We first create a potential object to work with. For this example, we’ll use a spherical NFW potential, parametrized by a scale radius and the circular velocity at the scale radius:
>>> pot = gp.SphericalNFWPotential(v_c=200*u.km/u.s, r_s=10.*u.kpc, units=galactic)
As a demonstration, we’re going to first integrate a single orbit in this potential.
The easiest way to do this is to use the integrate_orbit
method of the potential object, which accepts a set of initial conditions and
a specification for the time-stepping. We’ll define the initial conditions as a
CartesianPhaseSpacePosition
object:
>>> ics = gd.CartesianPhaseSpacePosition(pos=[10,0,0.]*u.kpc,
... vel=[0,175,0]*u.km/u.s)
>>> orbit = pot.integrate_orbit(ics, dt=2., n_steps=2000)
This method returns a CartesianOrbit
object that contains an
array of times and the (6D) position at each time-step. By default, this method
uses Leapfrog integration to compute the orbit
(LeapfrogIntegrator
), but you can optionally specify
a different (e.g., more precise) integrator class as a keyword argument:
>>> orbit = pot.integrate_orbit(ics, dt=2., n_steps=2000,
... Integrator=gi.DOPRI853Integrator)
We can integrate many orbits in parallel by passing in a 2D array of initial conditions. Here, as an example, we’ll generate some random initial conditions by sampling from a Gaussian around the initial orbit (with a positional scale of 100 pc, and a velocity scale of 1 km/s):
>>> norbits = 128
>>> new_pos = np.random.normal(ics.pos.to(u.pc).value, 100., size=(3,norbits))*u.pc
>>> new_vel = np.random.normal(ics.vel.to(u.km/u.s).value, 1, size=(3,norbits))*u.km/u.s
>>> new_ics = gd.CartesianPhaseSpacePosition(pos=new_pos, vel=new_vel)
>>> orbits = pot.integrate_orbit(new_ics, dt=2., n_steps=2000)
We’ll now plot the final positions of these orbits over isopotential contours.
We use the plot_contours()
method of the potential
object to plot the potential contours. This function returns a
Figure
object, which we can then use to over-plot
the orbit points:
>>> grid = np.linspace(-15,15,64)
>>> fig = pot.plot_contours(grid=(grid,grid,0), cmap='Greys')
>>> ax = fig.axes[0] # grab the first plot axes
>>> ax.plot(orbits.pos[0,-1], orbits.pos[1,-1], # this is x and y, the last timestep
... marker='.', linestyle='none', alpha=0.5, color='#cc0000')
(Source code, png, hires.png, pdf)