def test_calculate_trajectory_iterator_RuntimeWarning_kerrnewman():
M = 0.5 * 5.972e24 * u.kg
a = 0. * u.one
Q = 0. * u.C
q = 0. * u.C / u.kg
bl = BoyerLindquistDifferential(
t=0.0 * u.s,
r=306.0 * u.m,
theta=np.pi / 2 * u.rad,
phi=np.pi / 2 * u.rad,
v_r=0.0 * u.m / u.s,
v_th=-0.01 * u.rad / u.s,
v_p=10.0 * u.rad / u.s,
)
mkn = KerrNewman(coords=bl, M=M, a=a, Q=Q, q=q)
end_lambda = 200.
step_size = 0.4e-6
OdeMethodKwargs = {"stepsize": step_size}
geod = Timelike(metric=mkn,
coords=bl,
end_lambda=end_lambda,
step_size=step_size)
with warnings.catch_warnings(record=True) as w:
it = geod.calculate_trajectory_iterator(
OdeMethodKwargs=OdeMethodKwargs, )
for _, _ in zip(range(1000), it):
pass
assert len(w) >= 1
def test_kerr_frame_dragging():
"""
Tests, if higher spin implies a "faster" capture (in terms of lambda),
owing to frame dragging effects
"""
q0 = [2.5, np.pi / 2, 0.]
p0 = [0., 0., -8.5]
end_lambda = 10.
step_size = 0.005
sch_geod = Timelike(position=q0,
momentum=p0,
a=0.,
end_lambda=end_lambda,
step_size=step_size,
return_cartesian=False,
julia=False)
kerr_geod = Timelike(position=q0,
momentum=p0,
a=0.9,
end_lambda=end_lambda,
step_size=step_size,
return_cartesian=False,
julia=False)
sch_traj = sch_geod.trajectory
kerr_traj = kerr_geod.trajectory
# Final lambda_sch > Final lambda_kerr
assert sch_traj[0].shape[0] > kerr_traj[0].shape[0]
assert sch_traj[0][-1] > kerr_traj[0][-1]
# Final r_sch > Final r_kerr
assert sch_traj[1][:, 0][-1] > kerr_traj[1][:, 0][-1]
def test_kerr0_eq_kn00():
metric_params = (0.5, 0.)
q0 = [2.5, np.pi / 2, 0.]
p0 = [0., 0., -8.5]
k = Timelike(
metric="Kerr",
metric_params=metric_params,
position=q0,
momentum=p0,
steps=50,
delta=0.5,
return_cartesian=True,
suppress_warnings=True,
)
kn = Timelike(
metric="KerrNewman",
metric_params=metric_params,
position=q0,
momentum=p0,
steps=50,
delta=0.5,
return_cartesian=True,
suppress_warnings=True,
)
assert_allclose(k.trajectory[0], kn.trajectory[0], atol=1e-6, rtol=1e-6)
assert_allclose(k.trajectory[1], kn.trajectory[1], atol=1e-6, rtol=1e-6)
def test_kerr0_eq_sch():
metric_params = (0., )
q0 = [4., np.pi / 2, 0.]
p0 = [0., 0., 0.]
k = Timelike(
metric="Kerr",
metric_params=metric_params,
position=q0,
momentum=p0,
steps=50,
delta=0.5,
return_cartesian=True,
suppress_warnings=True,
)
s = Timelike(
metric="Schwarzschild",
metric_params=metric_params,
position=q0,
momentum=p0,
steps=50,
delta=0.5,
return_cartesian=True,
suppress_warnings=True,
)
assert_allclose(k.trajectory[0], s.trajectory[0], atol=1e-6, rtol=1e-6)
assert_allclose(k.trajectory[1], s.trajectory[1], atol=1e-6, rtol=1e-6)
def test_calculate_trajectory_iterator_RuntimeWarning_kerr():
M = 1e25 * u.kg
a = 0. * u.one
bl = BoyerLindquistDifferential(
t=0.0 * u.s,
r=306.0 * u.m,
theta=np.pi / 2 * u.rad,
phi=np.pi / 2 * u.rad,
v_r=0.0 * u.m / u.s,
v_th=0.01 * u.rad / u.s,
v_p=10.0 * u.rad / u.s,
)
mk = Kerr(coords=bl, M=M, a=a)
end_lambda = 1.
stepsize = 0.4e-6
OdeMethodKwargs = {"stepsize": stepsize}
geod = Timelike(metric=mk,
coords=bl,
end_lambda=end_lambda,
step_size=stepsize,
return_cartesian=False)
with warnings.catch_warnings(record=True) as w:
it = geod.calculate_trajectory_iterator(
OdeMethodKwargs=OdeMethodKwargs, )
for _, _ in zip(range(1000), it):
pass
assert len(w) >= 1
def test_calculate_trajectory_iterator_RuntimeWarning_schwarzschild():
M = 1e25 * u.kg
sph = SphericalDifferential(
t=0.0 * u.s,
r=306.0 * u.m,
theta=np.pi / 2 * u.rad,
phi=-np.pi / 2 * u.rad,
v_r=0.0 * u.m / u.s,
v_th=0.01 * u.rad / u.s,
v_p=10.0 * u.rad / u.s,
)
ms = Schwarzschild(coords=sph, M=M)
end_lambda = 1.
stepsize = 0.4e-6
OdeMethodKwargs = {"stepsize": stepsize}
geod = Timelike(metric=ms,
coords=sph,
end_lambda=end_lambda,
step_size=stepsize,
return_cartesian=False)
with warnings.catch_warnings(record=True) as w:
it = geod.calculate_trajectory_iterator(
OdeMethodKwargs=OdeMethodKwargs, )
for _, _ in zip(range(1000), it):
pass
assert len(w) >= 1
def perihelion():
"""
An example to showcase the usage of the various modules in ``einsteinpy``. \
Here, we assume a Schwarzschild spacetime and obtain & plot the apsidal precession of \
test particle orbit in it.
Returns
-------
geod: ~einsteinpy.geodesic.Geodesic
Geodesic defining test particle trajectory
"""
# Mass of the black hole in SI
M = 6e24 * u.kg
# Defining the initial coordinates of the test particle
# in SI
sph = SphericalDifferential(
t=10000.0 * u.s,
r=130.0 * u.m,
theta=np.pi / 2 * u.rad,
phi=-np.pi / 8 * u.rad,
v_r=0.0 * u.m / u.s,
v_th=0.0 * u.rad / u.s,
v_p=1900.0 * u.rad / u.s,
)
# Schwarzschild Metric Object
ms = Schwarzschild(coords=sph, M=M)
# Calculating Geodesic
geod = Timelike(metric=ms, coords=sph, end_lambda=0.002, step_size=5e-8)
return geod
def precession():
"""
An example to showcase the usage of the various modules in ``einsteinpy``.
Here, we assume a Schwarzschild spacetime and obtain a test particle orbit, that
shows apsidal precession.
Returns
-------
geod: ~einsteinpy.geodesic.Timelike
Timelike Geodesic, defining test particle trajectory
"""
# Defining initial conditions
metric = "Schwarzschild"
position = [40.0, np.pi / 2, 0.0]
momentum = [0.0, 0.0, 3.83405]
# Calculating Geodesic
geod = Timelike(
metric=metric,
metric_params=(),
position=position,
momentum=momentum,
steps=5500,
delta=1.0,
)
return geod
def test_calculate_trajectory1_kerrnewman():
# This needs more investigation
# the test particle should not move as gravitational & electromagnetic forces are balanced
M = 0.5 * 5.972e24 * u.kg
a = 0. * u.one
Q = 11604461683.91822052001953125 * u.C
q = _G * M.value / _Cc * u.C / u.kg
r = 1e6
end_lambda = 1000.0
step_size = 0.5
bl = BoyerLindquistDifferential(
t=0.0 * u.s,
r=r * u.m,
theta=np.pi / 2 * u.rad,
phi=0.0 * u.rad,
v_r=0.0 * u.m / u.s,
v_th=0.0 * u.rad / u.s,
v_p=0.0 * u.rad / u.s,
)
mkn = KerrNewman(coords=bl, M=M, a=a, Q=Q, q=q)
geod = Timelike(metric=mkn,
coords=bl,
end_lambda=end_lambda,
step_size=step_size,
return_cartesian=False)
ans = geod.trajectory
assert_allclose(ans[0][1], ans[-1][1], 1e-2)
def precession():
"""
An example to showcase the usage of the various modules in ``einsteinpy``.
Here, we assume a Schwarzschild spacetime and obtain a test particle orbit, that
shows apsidal precession.
Returns
-------
geod: ~einsteinpy.geodesic.Timelike
Timelike Geodesic, defining test particle trajectory
"""
# Defining initial conditions
position = [40.0, np.pi / 2, 0.0]
momentum = [0.0, 0.0, 3.83405]
spin = 0.0
# Calculating Geodesic
geod = Timelike(
position=position,
momentum=momentum,
a=spin,
end_lambda=2000.0,
step_size=0.5,
return_cartesian=True,
julia=True,
)
return geod
def test_str_repr():
"""
Tests, if the ``__str__`` and ``__repr__`` messages match
"""
M = 1e25 * u.kg
sph = SphericalDifferential(
t=0.0 * u.s,
r=306.0 * u.m,
theta=np.pi / 2 * u.rad,
phi=-np.pi / 2 * u.rad,
v_r=0.0 * u.m / u.s,
v_th=0.01 * u.rad / u.s,
v_p=10.0 * u.rad / u.s,
)
ms = Schwarzschild(coords=sph, M=M)
end_lambda = 1.
step_size = 0.4e-6
geod = Timelike(metric=ms,
coords=sph,
end_lambda=end_lambda,
step_size=step_size)
assert str(geod) == repr(geod)
def test_calculate_trajectory2_schwarzschild():
# based on the revolution of earth around sun
# data from https://en.wikipedia.org/wiki/Earth%27s_orbit
distance_at_perihelion = 147.10e9
speed_at_perihelion = 29290
angular_vel = (speed_at_perihelion / distance_at_perihelion)
sph = SphericalDifferential(
t=0.0 * u.s,
r=distance_at_perihelion * u.m,
theta=np.pi / 2 * u.rad,
phi=0.0 * u.rad,
v_r=0.0 * u.m / u.s,
v_th=0.0 * u.rad / u.s,
v_p=angular_vel * u.rad / u.s,
)
metric = Schwarzschild(coords=sph, M=1.989e30 * u.kg)
end_lambda = 3.154e7
geod = Timelike(metric=metric,
coords=sph,
end_lambda=end_lambda,
step_size=end_lambda / 2e3,
return_cartesian=False)
ans = geod.trajectory
# velocity should be 29.29 km/s at aphelion(where r is max)
i = np.argmax(ans[:, 1]) # index where radial distance is max
v_aphelion = (((ans[i][1] * ans[i][7]) * (u.m / u.s)).to(u.km / u.s)).value
assert_allclose(v_aphelion, 29.29, rtol=0.01)
def test_calculate_state_raises_TypeError():
"""
Tests, if ``_calculate_state`` raises TypeError, in case of \
coordinate mismatch
"""
distance_at_perihelion = 147.10e9
speed_at_perihelion = 29290
x_sph = CartesianDifferential(
t=0.0 * u.s,
x=distance_at_perihelion / np.sqrt(2) * u.m,
y=distance_at_perihelion / np.sqrt(2) * u.m,
z=0. * u.m,
v_x=-speed_at_perihelion / np.sqrt(2) * u.m / u.s,
v_y=speed_at_perihelion / np.sqrt(2) * u.m / u.s,
v_z=0 * u.m / u.s) # .spherical_differential()
metric = Schwarzschild(coords=x_sph.spherical_differential(),
M=1.989e30 * u.kg)
end_lambda = 3.154e7
with pytest.raises(TypeError):
geod = Timelike(
metric=metric,
coords=x_sph,
end_lambda=end_lambda,
step_size=end_lambda / 2e3,
)
def test_Geodesics_has_trajectory(dummy_data):
sph, metric, end_lambda, step_size = dummy_data
geo = Timelike(metric=metric,
coords=sph,
end_lambda=end_lambda,
step_size=step_size)
assert isinstance(geo.trajectory, np.ndarray)
def test_str_repr(dummy_time_python):
q0, p0, a, end_lambda, step_size, julia = dummy_time_python
geod = Timelike(position=q0,
momentum=p0,
a=a,
end_lambda=end_lambda,
step_size=step_size,
return_cartesian=True,
julia=julia)
assert str(geod) == repr(geod)
def test_calculate_trajectory_iterator_kerr(bl, M, a, end_lambda, step_size,
OdeMethodKwargs, return_cartesian):
mk = Kerr(coords=bl, M=M, a=a)
geod = Timelike(metric=mk,
coords=bl,
end_lambda=end_lambda,
step_size=step_size,
return_cartesian=return_cartesian)
traj = geod.trajectory
traj_iter = geod.calculate_trajectory_iterator(
OdeMethodKwargs=OdeMethodKwargs, return_cartesian=return_cartesian)
traj_iter_list = list()
for _, val in zip(range(50), traj_iter):
traj_iter_list.append(val[1])
traj_iter_arr = np.array(traj_iter_list)
assert_allclose(traj[:50, :], traj_iter_arr, rtol=1e-10)
def dummy_geod():
return Timelike(
metric="Kerr",
metric_params=(0.9,),
position=[2.15, np.pi / 2, 0.],
momentum=[0., 0., 1.5],
steps=50,
delta=0.5,
omega=0.01, # Close orbit
return_cartesian=True,
suppress_warnings=True,
)
def test_constant_rad():
geod = Timelike(
metric="Kerr",
metric_params=(0.99, ),
position=[4., np.pi / 3, 0.],
momentum=[0., 0.767851, 2.],
return_cartesian=False,
steps=50,
delta=1.,
)
r = geod.trajectory[1][:, 1]
assert_allclose(r, 4., atol=1e-2, rtol=1e-2)
def test_equatorial_geodesic(dummy_time_python):
q0, p0, a, end_lambda, step_size, julia = dummy_time_python
geod = Timelike(position=q0,
momentum=p0,
a=a,
end_lambda=end_lambda,
step_size=step_size,
return_cartesian=False,
julia=julia)
theta = q0[1]
assert_allclose(geod.trajectory[1][:, 1], theta, atol=1e-4, rtol=1e-4)
def test_geodesic_attribute2(dummy_time_python):
q0, p0, a, end_lambda, step_size, julia = dummy_time_python
geod = Timelike(position=q0,
momentum=p0,
a=a,
end_lambda=end_lambda,
step_size=step_size,
return_cartesian=True,
julia=julia)
traj = geod.trajectory
assert traj
assert traj[0].shape[0] == traj[1].shape[0]
assert traj[1].shape[1] == 6
def test_geodesic_attribute1(dummy_time_python):
q0, p0, a, end_lambda, step_size, julia = dummy_time_python
geod = Timelike(position=q0,
momentum=p0,
a=a,
end_lambda=end_lambda,
step_size=step_size,
return_cartesian=True,
julia=julia)
traj = geod.trajectory
assert isinstance(traj, tuple)
assert isinstance(traj[0], np.ndarray)
assert isinstance(traj[1], np.ndarray)
def test_compare_calculate_trajectory_iterator_cartesian_kerrnewman(
test_input):
a, Q, q, end_lambda, step_size = test_input
M = 2e24 * u.kg
x_bl = CartesianDifferential(t=0.0 * u.s,
x=1e6 * u.m,
y=1e6 * u.m,
z=20.5 * u.m,
v_x=1e4 * u.m / u.s,
v_y=1e4 * u.m / u.s,
v_z=-30.0 * u.m / u.s).bl_differential(M=M,
a=a)
mkn = KerrNewman(coords=x_bl, M=M, a=a, Q=Q, q=q)
OdeMethodKwargs = {"stepsize": step_size}
return_cartesian = True
geod = Timelike(metric=mkn,
coords=x_bl,
end_lambda=end_lambda,
step_size=step_size,
return_cartesian=return_cartesian)
traj = geod.trajectory
traj_iter = geod.calculate_trajectory_iterator(
OdeMethodKwargs=OdeMethodKwargs, return_cartesian=return_cartesian)
traj_iter_list = list()
for _, val in zip(range(20), traj_iter):
traj_iter_list.append(val[1])
traj_iter_arr = np.array(traj_iter_list)
assert_allclose(traj[:20], traj_iter_arr)
def test_compare_calculate_trajectory_iterator_bl_kerrnewman(test_input):
a, Q, q, end_lambda, step_size = test_input
M = 0.5 * 5.972e24 * u.kg
bl = BoyerLindquistDifferential(
t=0.0 * u.s,
r=1e6 * u.m,
theta=0.6 * np.pi * u.rad,
phi=np.pi / 8 * u.rad,
v_r=1e4 * u.m / u.s,
v_th=-0.01 * u.rad / u.s,
v_p=0.0 * u.rad / u.s,
)
mkn = KerrNewman(coords=bl, M=M, a=a, Q=Q, q=q)
OdeMethodKwargs = {"stepsize": step_size}
return_cartesian = False
geod = Timelike(metric=mkn,
coords=bl,
end_lambda=end_lambda,
step_size=step_size,
return_cartesian=return_cartesian)
traj = geod.trajectory
traj_iter = geod.calculate_trajectory_iterator(
OdeMethodKwargs=OdeMethodKwargs, return_cartesian=return_cartesian)
traj_iter_list = list()
for _, val in zip(range(20), traj_iter):
traj_iter_list.append(val[1])
traj_iter_arr = np.array(traj_iter_list)
assert_allclose(traj[:20], traj_iter_arr)
def test_calculate_trajectory_schwarzschild(sph, M, end_lambda, step_size):
ms = Schwarzschild(coords=sph, M=M)
geod = Timelike(metric=ms,
coords=sph,
end_lambda=end_lambda,
step_size=step_size,
return_cartesian=False)
ans = geod.trajectory
testarray = list()
for i in ans:
x = i[:4]
g = ms.metric_covariant(x)
testarray.append(g[0][0] * (i[4]**2) + g[1][1] * (i[5]**2) + g[2][2] *
(i[6]**2) + g[3][3] * (i[7]**2))
testarray = np.array(testarray)
assert_allclose(testarray, _c**2, 1e-4)
def test_calculate_trajectory0_kerrnewman():
# Based on the revolution of earth around sun
# Data from https://en.wikipedia.org/wiki/Earth%27s_orbit
# Initialized with cartesian coordinates
# Function returning cartesian coordinates
M = 1.989e30 * u.kg
a = 0. * u.one
Q = 0. * u.C
q = 0. * u.C / u.kg
distance_at_perihelion = 147.10e9
speed_at_perihelion = 29290
x_bl = CartesianDifferential(
t=0.0 * u.s,
x=distance_at_perihelion / np.sqrt(2) * u.m,
y=distance_at_perihelion / np.sqrt(2) * u.m,
z=0.0 * u.m,
v_x=-speed_at_perihelion / np.sqrt(2) * u.m / u.s,
v_y=speed_at_perihelion / np.sqrt(2) * u.m / u.s,
v_z=0.0 * u.m / u.s).bl_differential(M=M, a=a)
mkn = KerrNewman(coords=x_bl, M=M, a=a, Q=Q, q=q)
end_lambda = 3.154e7
geod = Timelike(
metric=mkn,
coords=x_bl,
end_lambda=end_lambda,
step_size=end_lambda / 1.5e3,
)
ans = geod.trajectory
# velocity should be 29.29 km/s at aphelion(where r is max)
R = np.sqrt(ans[:, 1]**2 + ans[:, 2]**2 + ans[:, 3]**2)
i = np.argmax(R) # index where radial distance is max
v_aphelion = ((np.sqrt(ans[i, 5]**2 + ans[i, 6]**2 + ans[i, 7]**2) *
(u.m / u.s)).to(u.km / u.s)).value
assert_allclose(v_aphelion, 29.29, rtol=0.01)
def dummy_data():
M = 6e24 * u.kg
sph = SphericalDifferential(
t=0.0 * u.s,
r=130.0 * u.m,
theta=np.pi / 2 * u.rad,
phi=-np.pi / 8 * u.rad,
v_r=0.0 * u.m / u.s,
v_th=0.0 * u.rad / u.s,
v_p=1900.0 * u.rad / u.s,
)
ms = Schwarzschild(coords=sph, M=M)
end_lambda = 0.002
step_size = 5e-8
geod = Timelike(metric=ms, coords=sph, end_lambda=end_lambda, step_size=step_size)
return geod
def test_calculate_trajectory_kerr(bl, M, a, end_lambda, step_size):
mk = Kerr(coords=bl, M=M, a=a)
geod = Timelike(metric=mk,
coords=bl,
end_lambda=end_lambda,
step_size=step_size,
return_cartesian=False)
ans = geod.trajectory
testarray = list()
for i in ans:
x = i[:4]
g = mk.metric_covariant(x)
testarray.append(g[0][0] * (i[4]**2) + g[1][1] * (i[5]**2) + g[2][2] *
(i[6]**2) + g[3][3] * (i[7]**2) +
2 * g[0][3] * i[4] * i[7])
testarray = np.array(testarray)
assert_allclose(testarray, _c**2, 1e-8)
def test_calculate_trajectory3_schwarzschild():
# same test as with test_calculate_trajectory2_schwarzschild(),
# but initialized with cartesian coordinates
# and function returning cartesian coordinates
distance_at_perihelion = 147.10e9
speed_at_perihelion = 29290
x_sph = CartesianDifferential(
t=0.0 * u.s,
x=distance_at_perihelion / np.sqrt(2) * u.m,
y=distance_at_perihelion / np.sqrt(2) * u.m,
z=0. * u.m,
v_x=-speed_at_perihelion / np.sqrt(2) * u.m / u.s,
v_y=speed_at_perihelion / np.sqrt(2) * u.m / u.s,
v_z=0 * u.m / u.s).spherical_differential()
metric = Schwarzschild(coords=x_sph, M=1.989e30 * u.kg)
end_lambda = 3.154e7
geod = Timelike(
metric=metric,
coords=x_sph,
end_lambda=end_lambda,
step_size=end_lambda / 2e3,
)
ans = geod.trajectory
# velocity should be 29.29 km/s at aphelion(where r is max)
R = np.sqrt(ans[:, 1]**2 + ans[:, 2]**2 + ans[:, 3]**2)
i = np.argmax(R) # index where radial distance is max
v_aphelion = ((np.sqrt(ans[i, 5]**2 + ans[i, 6]**2 + ans[i, 7]**2) *
(u.m / u.s)).to(u.km / u.s)).value
assert_allclose(v_aphelion, 29.29, rtol=0.01)