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import numpy as np
import pytest
import astropy.units as u
from astropy.constants import c as speed_of_light
from astropy.coordinates import (
HCRS,
ICRS,
ITRS,
Angle,
CartesianDifferential,
CartesianRepresentation,
ConvertError,
HeliocentricMeanEcliptic,
Longitude,
SkyCoord,
SphericalDifferential,
SphericalRepresentation,
get_body_barycentric,
get_body_barycentric_posvel,
)
from astropy.tests.helper import assert_quantity_allclose, quantity_allclose
from astropy.time import Time
from sunpy.coordinates import (
GeocentricEarthEquatorial,
GeocentricSolarEcliptic,
GeocentricSolarMagnetospheric,
Geomagnetic,
Heliocentric,
HeliocentricEarthEcliptic,
HeliocentricInertial,
HeliographicCarrington,
HeliographicStonyhurst,
Helioprojective,
HelioprojectiveRadial,
SolarMagnetic,
SphericalScreen,
propagate_with_solar_surface,
sun,
transform_with_sun_center,
)
from sunpy.coordinates.ephemeris import get_body_heliographic_stonyhurst, get_earth
from sunpy.coordinates.frames import _J2000
from sunpy.sun.constants import radius as _RSUN
from sunpy.sun.constants import sidereal_rotation_rate
from sunpy.sun.models import differential_rotation
from sunpy.time import parse_time
def test_hcc_to_hgs():
'''
Check that a coordinate pointing to the observer in Heliocentric
coordinates maps to the latitude/longitude of the observer in
HeliographicStonyhurst coordinates.
'''
lat = 10 * u.deg
lon = 20 * u.deg
observer = HeliographicStonyhurst(lat=lat, lon=lon)
hcc_in = Heliocentric(x=0*u.km, y=0*u.km, z=1*u.km, observer=observer)
hgs_out = hcc_in.transform_to(HeliographicStonyhurst())
assert_quantity_allclose(hgs_out.lat, lat)
assert_quantity_allclose(hgs_out.lon, lon)
def test_hpc_hpc():
# Use some unphysical values for solar parameters for testing, to make it
# easier to calculate expected results.
rsun = 1*u.m
D0 = 1*u.km
L0 = 1*u.deg
observer_in = HeliographicStonyhurst(lat=0*u.deg, lon=0*u.deg, radius=D0)
observer_out = HeliographicStonyhurst(lat=0*u.deg, lon=L0, radius=D0)
hpc_in = Helioprojective(0*u.arcsec, 0*u.arcsec, rsun=rsun, observer=observer_in)
hpc_out = Helioprojective(observer=observer_out, rsun=rsun)
hpc_new = hpc_in.transform_to(hpc_out)
assert hpc_new.observer == hpc_out.observer
# Calculate the distance subtended by an angle of L0 from the centre of the
# Sun.
dd = -1 * rsun * np.tan(L0)
# Calculate the angle corresponding to that distance as seen by the new
# observer.
theta = np.arctan2(dd, (D0 - rsun))
assert quantity_allclose(theta, hpc_new.Tx, rtol=1e-3)
def test_hpc_hpc_sc():
# Use some unphysical values for solar parameters for testing, to make it
# easier to calculate expected results.
rsun = 1*u.m
D0 = 1*u.km
L0 = 1*u.deg
observer_in = HeliographicStonyhurst(lat=0*u.deg, lon=0*u.deg, radius=D0)
observer_out = HeliographicStonyhurst(lat=0*u.deg, lon=L0, radius=D0)
sc_in = SkyCoord(0*u.arcsec, 0*u.arcsec, rsun=rsun, observer=observer_in,
frame='helioprojective')
hpc_out = Helioprojective(observer=observer_out, rsun=rsun)
hpc_new = sc_in.transform_to(hpc_out)
assert hpc_new.observer.lat == hpc_out.observer.lat
assert hpc_new.observer.lon == hpc_out.observer.lon
assert hpc_new.observer.radius == hpc_out.observer.radius
def test_hpc_hpc_null():
hpc_in = Helioprojective(0*u.arcsec, 0*u.arcsec)
hpc_out = Helioprojective()
hpc_new = hpc_in.transform_to(hpc_out)
assert hpc_new is not hpc_in
assert quantity_allclose(hpc_new.Tx, hpc_in.Tx)
assert quantity_allclose(hpc_new.Ty, hpc_in.Ty)
assert hpc_out.observer == hpc_new.observer
@pytest.mark.parametrize(('Tx', 'Ty', 'psi', 'delta', 'theta'),
[(0*u.arcsec, 0*u.arcsec, 0*u.deg, -90*u.deg, 0*u.arcsec),
(360*u.arcsec, 0*u.arcsec, 270*u.deg, -89.9*u.deg, 360*u.arcsec),
(0*u.arcsec, -720*u.arcsec, 180*u.deg, -89.8*u.deg, 720*u.arcsec),
(360*u.arcsec, -720*u.arcsec, 206.564946*u.deg, -89.776393*u.deg, 804.984145*u.arcsec)])
def test_hpc_hpr(Tx, Ty, psi, delta, theta):
observer = HeliographicStonyhurst(0*u.deg, 0*u.deg, radius=1*u.AU)
hpc = Helioprojective(Tx, Ty, observer=observer)
hpr = hpc.transform_to(HelioprojectiveRadial(observer=observer))
assert_quantity_allclose(hpr.psi, psi)
assert_quantity_allclose(hpr.delta, delta)
assert_quantity_allclose(hpr.theta, theta)
hpc_back = hpr.transform_to(hpc)
assert_quantity_allclose(hpc_back.Tx, Tx)
assert_quantity_allclose(hpc_back.Ty, Ty)
def test_hpc_hpc_spherical_screen():
D0 = 20*u.R_sun
L0 = 67.5*u.deg
Tx0 = 45*u.deg
observer_in = HeliographicStonyhurst(lat=0*u.deg, lon=0*u.deg, radius=D0)
# Once our coordinate is placed on the screen, observer_out will be looking
# directly along the line containing itself, the coordinate, and the Sun
observer_out = HeliographicStonyhurst(lat=0*u.deg, lon=L0, radius=2*D0)
sc_in = SkyCoord(Tx0, 0*u.deg, observer=observer_in,
frame='helioprojective')
with SphericalScreen(observer_in):
sc_3d = sc_in.make_3d()
sc_out = sc_in.transform_to(Helioprojective(observer=observer_out))
assert quantity_allclose(sc_3d.distance, D0)
assert quantity_allclose(sc_out.Tx, 0*u.deg, atol=1e-6*u.deg)
assert quantity_allclose(sc_out.Ty, 0*u.deg, atol=1e-6*u.deg)
# Law of Cosines to compute the coordinate's distance from the Sun, and then
# r_expected is the distance from observer_out to the coordinate
radius_expected = 2 * D0 - np.sqrt(2 * D0**2 - 2 * D0 * D0 * np.cos(45*u.deg))
assert quantity_allclose(sc_out.distance, radius_expected)
# Now test with a very large screen, letting us approximate the two
# observers as being the same (aside from a different zero point for Tx)
r_s = 1e9 * u.lightyear
with SphericalScreen(observer_in, radius=r_s):
sc_3d = sc_in.make_3d()
sc_out = sc_in.transform_to(Helioprojective(observer=observer_out))
assert quantity_allclose(sc_3d.distance, r_s)
assert quantity_allclose(sc_out.Tx, Tx0 + L0)
assert quantity_allclose(sc_out.Ty, 0*u.deg)
assert quantity_allclose(sc_out.distance, r_s)
def test_hcrs_hgs():
# Get the current Earth location in HCRS
adate = parse_time('2015/05/01 01:13:00')
earth_hcrs = SkyCoord(get_body_barycentric('earth', adate), frame='icrs', obstime=adate).hcrs
# Convert from HCRS to HGS
earth_hgs = earth_hcrs.transform_to(HeliographicStonyhurst)
# The HGS longitude of the Earth should be zero within numerical error
# Due to an issue with wrapping at +-360, we shift it to pass the test.
assert quantity_allclose((earth_hgs.lon+1*u.deg) % (360*u.deg), 1*u.deg, atol=1e-12*u.deg)
# The HGS latitude and radius should be within valid ranges
assert quantity_allclose(earth_hgs.lat, 0*u.deg, atol=7.3*u.deg)
assert quantity_allclose(earth_hgs.radius, 1*u.AU, atol=0.017*u.AU)
def test_hcrs_hgs_array_obstime():
# Get the Earth location in HCRS at two times
times = Time(['2017-01-01', '2017-06-01'])
earth_hcrs = SkyCoord(get_body_barycentric('earth', times), frame='icrs', obstime=times).hcrs
# Transform each time in separate calls (uses scalar obstime)
earth_hgs_0 = earth_hcrs[0].transform_to(HeliographicStonyhurst)
earth_hgs_1 = earth_hcrs[1].transform_to(HeliographicStonyhurst)
# Transform both times in one call (uses array obstime)
earth_hgs = earth_hcrs.transform_to(HeliographicStonyhurst)
# Confirm that the two approaches produce the same results
assert quantity_allclose(earth_hgs_0.lon, earth_hgs[0].lon, atol=1e-12*u.deg)
assert quantity_allclose(earth_hgs_0.lat, earth_hgs[0].lat, rtol=1e-10)
assert quantity_allclose(earth_hgs_0.radius, earth_hgs[0].radius, rtol=1e-10)
assert quantity_allclose(earth_hgs_1.lon, earth_hgs[1].lon, atol=1e-12*u.deg)
assert quantity_allclose(earth_hgs_1.lat, earth_hgs[1].lat, rtol=1e-10)
assert quantity_allclose(earth_hgs_1.radius, earth_hgs[1].radius, rtol=1e-10)
def test_hgs_hcrs():
# This test checks the HGS->HCRS transformation by transforming from HGS to
# HeliocentricMeanEcliptic (HME). It will fail if there are errors in Astropy's
# HCRS->ICRS or ICRS->HME transformations.
# Use published HGS coordinates in the Astronomical Almanac (2013), pages C6-C7
obstime = Time('2013-01-28')
earth_hgs = SkyCoord(0*u.deg, -5.73*u.deg, 0.9848139*u.AU, frame=HeliographicStonyhurst,
obstime=obstime)
# Transform to HME at observation-time equinox
earth_hme = earth_hgs.transform_to(HeliocentricMeanEcliptic(equinox=obstime))
# Validate against published values from the Astronomical Almanac (2013), page C6 per page E2
# The dominant source of inaccuracy is the limited precision of the published B0 used above
assert quantity_allclose(earth_hme.lon, Angle('308d13m30.51s') - 180*u.deg, atol=5*u.arcsec)
assert quantity_allclose(earth_hme.lat, -Angle('-0.27s'), atol=10*u.arcsec)
assert quantity_allclose(earth_hme.distance, 0.9848139*u.AU, atol=5e-7*u.AU)
def test_hcrs_hgs_different_obstime():
# Test whether the HCRS->HGS transformation handles a change in obstime the same way as forcing
# a HCRS loopback in Astropy
time1 = Time('2001-01-01')
time2 = Time('2001-02-01')
coord = HCRS(1*u.km, 2*u.km, 3*u.km, representation_type='cartesian', obstime=time1)
out_frame = HeliographicStonyhurst(obstime=time2)
sunpy_coord = coord.transform_to(out_frame)
astropy_coord = coord.transform_to(HCRS(obstime=time2)).transform_to(out_frame)
assert quantity_allclose(sunpy_coord.cartesian.xyz, astropy_coord.cartesian.xyz)
def test_hcrs_hgs_reversibility():
# Test whether the HCRS->HGS transformation is reversed by the HGS->HCRS transformation
time1 = Time('2001-01-01')
time2 = Time('2001-02-01')
coord = HCRS(1*u.km, 2*u.km, 3*u.km, representation_type='cartesian', obstime=time1)
new_coord = coord.transform_to(HeliographicStonyhurst(obstime=time2)).transform_to(coord)
assert quantity_allclose(coord.cartesian.xyz, new_coord.cartesian.xyz)
def test_hgs_hgc_roundtrip():
obstime = "2011-01-01"
hgsin = HeliographicStonyhurst(lat=10*u.deg, lon=20*u.deg, obstime=obstime)
hgcout = hgsin.transform_to(HeliographicCarrington(observer='earth', obstime=obstime))
assert_quantity_allclose(hgsin.lat, hgcout.lat)
assert_quantity_allclose(hgsin.lon + sun.L0(obstime), hgcout.lon)
hgsout = hgcout.transform_to(HeliographicStonyhurst(obstime=obstime))
assert_quantity_allclose(hgsout.lat, hgsin.lat)
assert_quantity_allclose(hgsout.lon, hgsin.lon)
def test_hgs_cartesian_rep_to_hpc():
# This test checks transformation HGS->HPC when the coordinate is in a Cartesian
# representation and that it is the same as a transformation from an HGS frame with a
# spherical representation
obstime = "2011-01-01"
hgscoord_cart = SkyCoord(x=1*u.km, y=0.*u.km, z=0.*u.km,
frame=HeliographicStonyhurst(obstime=obstime),
representation_type='cartesian')
hpc_frame = Helioprojective(observer='earth', obstime=obstime)
hgscoord_sph = hgscoord_cart.copy()
hgscoord_sph.representation_type = 'spherical'
hpccoord_cart = hgscoord_cart.transform_to(hpc_frame)
hpccoord_sph = hgscoord_sph.transform_to(hpc_frame)
assert_quantity_allclose(hpccoord_cart.Tx, hpccoord_sph.Tx)
assert_quantity_allclose(hpccoord_cart.Ty, hpccoord_sph.Ty)
assert_quantity_allclose(hpccoord_cart.distance, hpccoord_sph.distance)
def test_hgs_cartesian_rep_to_hcc():
# This test checks transformation HGS->HCC when the coordinate is in a Cartesian
# representation and that it is the same as a transformation from an HGS frame with a
# spherical representation
obstime = "2011-01-01"
hgscoord_cart = SkyCoord(x=1*u.km, y=0.*u.km, z=0.*u.km,
frame=HeliographicStonyhurst(obstime=obstime),
representation_type='cartesian')
hcc_frame = Heliocentric(observer='earth', obstime=obstime)
hgscoord_sph = hgscoord_cart.copy()
hgscoord_sph.representation_type = 'spherical'
hcccoord_cart = hgscoord_cart.transform_to(hcc_frame)
hcccoord_sph = hgscoord_sph.transform_to(hcc_frame)
assert_quantity_allclose(hcccoord_cart.x, hcccoord_sph.x)
assert_quantity_allclose(hcccoord_cart.y, hcccoord_sph.y)
assert_quantity_allclose(hcccoord_cart.z, hcccoord_sph.z)
def test_hgs_cartesian_rep_to_hgc():
# This test checks transformation HGS->HCC when the coordinate is in a Cartesian
# representation and that it is the same as a transformation from an HGS frame with a
# spherical representation
obstime = "2011-01-01"
hgscoord_cart = SkyCoord(x=1*u.km, y=0.*u.km, z=0.*u.km,
frame=HeliographicStonyhurst(obstime=obstime),
representation_type='cartesian')
hgscoord_sph = hgscoord_cart.copy()
hgscoord_sph.representation_type = 'spherical'
# HGC
hgcframe = HeliographicCarrington(observer='earth', obstime=obstime)
hgccoord_cart = hgscoord_cart.transform_to(hgcframe)
hgccoord_sph = hgscoord_sph.transform_to(hgcframe)
assert_quantity_allclose(hgccoord_cart.lat, hgccoord_sph.lat)
assert_quantity_allclose(hgccoord_cart.lon, hgccoord_sph.lon)
assert_quantity_allclose(hgccoord_cart.radius, hgccoord_sph.radius)
def test_hcc_to_hpc_different_observer():
# This test checks transformation HCC->HPC in the case where the HCC and HPC frames are
# defined by different observers.
rsun = 1*u.m
D0 = 1*u.km
L0 = 1*u.deg
observer_1 = HeliographicStonyhurst(lat=0*u.deg, lon=0*u.deg, radius=D0)
observer_2 = HeliographicStonyhurst(lat=0*u.deg, lon=L0, radius=D0)
hcc_frame = Heliocentric(observer=observer_1)
hpc_frame = Helioprojective(observer=observer_2)
hcccoord = SkyCoord(x=rsun, y=rsun, z=rsun, frame=hcc_frame)
hpccoord_out = hcccoord.transform_to(hpc_frame)
hpccoord_expected = hcccoord.transform_to(HeliographicStonyhurst).transform_to(hpc_frame)
assert_quantity_allclose(hpccoord_out.Tx, hpccoord_expected.Tx)
assert_quantity_allclose(hpccoord_out.Ty, hpccoord_expected.Ty)
assert_quantity_allclose(hpccoord_out.distance, hpccoord_expected.distance)
def test_hpc_to_hcc_different_observer():
# This test checks transformation HPC->HCC in the case where the HCC and HPC frames are
# defined by different observers.
rsun = 1*u.m
D0 = 1*u.km
L0 = 1*u.deg
observer_1 = HeliographicStonyhurst(lat=0*u.deg, lon=0*u.deg, radius=D0)
observer_2 = HeliographicStonyhurst(lat=0*u.deg, lon=L0, radius=D0)
hcc_frame = Heliocentric(observer=observer_1)
hpc_frame = Helioprojective(observer=observer_2, rsun=rsun)
hpccoord = SkyCoord(Tx=0*u.arcsec, Ty=0*u.arcsec, frame=hpc_frame)
hcccoord_out = hpccoord.transform_to(hcc_frame)
hcccoord_expected = hpccoord.transform_to(HeliographicStonyhurst).transform_to(hcc_frame)
assert_quantity_allclose(hcccoord_out.x, hcccoord_expected.x)
assert_quantity_allclose(hcccoord_out.y, hcccoord_expected.y)
assert_quantity_allclose(hcccoord_out.z, hcccoord_expected.z)
def test_hcc_to_hpc_same_observer():
# This test checks transformation HCC->HPC in the case of same observer
rsun = 1*u.m
D0 = 1*u.km
observer = HeliographicStonyhurst(lat=0*u.deg, lon=0*u.deg, radius=D0)
hcc_frame = Heliocentric(observer=observer)
hpc_frame = Helioprojective(observer=observer, rsun=rsun)
hcccoord = SkyCoord(x=rsun, y=rsun, z=rsun, frame=hcc_frame)
hpccoord_out = hcccoord.transform_to(hpc_frame)
hpccoord_expected = hcccoord.transform_to(HeliographicStonyhurst).transform_to(hpc_frame)
assert_quantity_allclose(hpccoord_out.Tx, hpccoord_expected.Tx)
assert_quantity_allclose(hpccoord_out.Ty, hpccoord_expected.Ty)
assert_quantity_allclose(hpccoord_out.distance, hpccoord_expected.distance)
def test_hpc_to_hcc_same_observer():
# This test checks transformation HPC->HCC in the case of same observer
rsun = 1*u.m
D0 = 1 * u.km
observer = HeliographicStonyhurst(lat=0 * u.deg, lon=0 * u.deg, radius=D0)
hcc_frame = Heliocentric(observer=observer)
hpc_frame = Helioprojective(observer=observer, rsun=rsun)
hpccoord = SkyCoord(Tx=0 * u.arcsec, Ty=0 * u.arcsec, frame=hpc_frame)
hcccoord_out = hpccoord.transform_to(hcc_frame)
hcccoord_expected = hpccoord.transform_to(HeliographicStonyhurst).transform_to(hcc_frame)
assert_quantity_allclose(hcccoord_out.x, hcccoord_expected.x)
assert_quantity_allclose(hcccoord_out.y, hcccoord_expected.y)
assert_quantity_allclose(hcccoord_out.z, hcccoord_expected.z)
def test_hpc_hcc_different_observer_radius():
# Tests HPC->HCC with a change in observer at different distances from the Sun
observer1 = HeliographicStonyhurst(0*u.deg, 0*u.deg, 1*u.AU)
hpc = Helioprojective(0*u.arcsec, 0*u.arcsec, 0.5*u.AU, observer=observer1)
observer2 = HeliographicStonyhurst(90*u.deg, 0*u.deg, 0.75*u.AU)
hcc = hpc.transform_to(Heliocentric(observer=observer2))
assert_quantity_allclose(hcc.x, -0.5*u.AU)
assert_quantity_allclose(hcc.y, 0*u.AU, atol=1e-10*u.AU)
assert_quantity_allclose(hcc.z, 0*u.AU, atol=1e-10*u.AU)
def test_hgs_hgs():
# Test HGS loopback transformation
obstime = Time('2001-01-01')
old = SkyCoord(90*u.deg, 10*u.deg, 1*u.AU, frame=HeliographicStonyhurst(obstime=obstime))
new = old.transform_to(HeliographicStonyhurst(obstime=obstime + 1*u.day))
assert_quantity_allclose(new.lon, old.lon - 1*u.deg, atol=0.1*u.deg) # due to Earth motion
assert_quantity_allclose(new.lat, old.lat, atol=1e-3*u.deg)
assert_quantity_allclose(new.radius, old.radius, atol=1e-5*u.AU)
def test_hgc_hgc():
# Test HGC loopback transformation
obstime = Time('2001-01-01')
old = SkyCoord(90*u.deg, 10*u.deg, 1*u.AU, frame=HeliographicCarrington(observer='earth',
obstime=obstime))
new = old.transform_to(HeliographicCarrington(observer='earth', obstime=obstime + 1*u.day))
assert_quantity_allclose(new.lon, 75.815592 * u.deg, atol=1e-7*u.deg) # solar rotation
# These are not equal to the old values, because the coordinates stay fixed
# in inertial space, whilst the frame (fixed to the center of the Sun)
# moves slightly.
assert_quantity_allclose(new.lat, 10.000037 * u.deg, atol=1e-7*u.deg)
assert_quantity_allclose(new.radius, 0.999991 * u.AU, atol=1e-7*u.AU)
def test_hgc_hgc_different_observers():
obstime = Time('2001-01-01')
hgc_earth = HeliographicCarrington(observer='earth', obstime=obstime)
hgc_mars = HeliographicCarrington(observer='mars', obstime=obstime)
hgc_sun = HeliographicCarrington(observer='sun', obstime=obstime)
sc = SkyCoord(10*u.deg, 20*u.deg, 1*u.AU, frame=HeliographicStonyhurst(obstime=obstime))
sc_hgc_earth = sc.transform_to(hgc_earth)
sc_hgc_mars = sc_hgc_earth.transform_to(hgc_mars)
sc_hgc_sun = sc_hgc_mars.transform_to(hgc_sun)
ltt_earth = hgc_earth.observer.radius / speed_of_light
assert_quantity_allclose(sc_hgc_earth.lon - sc_hgc_sun.lon, ltt_earth * sidereal_rotation_rate)
ltt_mars = hgc_mars.observer.radius / speed_of_light
assert_quantity_allclose(sc_hgc_mars.lon - sc_hgc_sun.lon, ltt_mars * sidereal_rotation_rate)
def test_hgc_self_observer():
# Test specifying observer='self' for HGC
obstime = Time('2001-01-01')
hgc = HeliographicCarrington(10*u.deg, 20*u.deg, 3*u.AU, observer='self', obstime=obstime)
# Transform to HGS (i.e., observer='self' in the source frame)
hgs = hgc.transform_to(HeliographicStonyhurst(obstime=obstime))
# Manually calculate the post-transformation longitude
lon = sun.L0(obstime,
light_travel_time_correction=False,
nearest_point=False,
aberration_correction=False)
lon += (hgc.radius - _RSUN) / speed_of_light * sidereal_rotation_rate
assert_quantity_allclose(Longitude(hgs.lon + lon), hgc.lon)
assert_quantity_allclose(hgs.lat, hgc.lat)
assert_quantity_allclose(hgs.radius, hgc.radius)
# Transform back to HGC (i.e., observer='self' in the destination frame)
hgc_loop = hgs.transform_to(hgc.replicate_without_data())
assert_quantity_allclose(hgc_loop.lon, hgc.lon)
assert_quantity_allclose(hgc_loop.lat, hgc.lat)
assert_quantity_allclose(hgc_loop.radius, hgc.radius)
def test_hgc_loopback_self_observer():
# Test the HGC loopback where only one end has observer='self'
obstime = Time('2001-01-01')
coord = HeliographicCarrington(10*u.deg, 20*u.deg, 3*u.AU, observer='self', obstime=obstime)
new_observer = HeliographicStonyhurst(40*u.deg, 50*u.deg, 6*u.AU)
new_frame = HeliographicCarrington(observer=new_observer, obstime=obstime)
new_coord = coord.transform_to(new_frame)
# Manually calculate the longitude shift due to the difference in Sun-observer distance
lon = (6*u.AU - 3*u.AU) / speed_of_light * sidereal_rotation_rate
assert_quantity_allclose(new_coord.lon, coord.lon + lon)
assert_quantity_allclose(new_coord.lat, coord.lat)
assert_quantity_allclose(new_coord.radius, coord.radius)
def test_hcc_hcc():
# Test same observer and changing obstime
observer = HeliographicStonyhurst(0*u.deg, 0*u.deg, 1*u.AU, obstime='2001-02-01')
from_hcc = Heliocentric(0.2*u.AU, 0.3*u.AU, 0.4*u.AU, observer=observer, obstime='2001-01-01')
to_hcc = from_hcc.transform_to(Heliocentric(observer=observer, obstime='2001-03-31'))
# Since the observer is the same, the coordinates should be nearly the same but not exactly
# equal due to motion of the origin (the Sun)
assert np.all(from_hcc.cartesian.xyz != to_hcc.cartesian.xyz)
assert_quantity_allclose(from_hcc.cartesian.xyz, to_hcc.cartesian.xyz, rtol=2e-3)
# Test changing observer and same obstime
observer1 = HeliographicStonyhurst(0*u.deg, 0*u.deg, 1*u.AU, obstime='2001-01-01')
observer2 = HeliographicStonyhurst(0*u.deg, 0*u.deg, 1*u.AU, obstime='2001-03-31')
from_hcc = Heliocentric(0.2*u.AU, 0.3*u.AU, 0.4*u.AU, observer=observer1, obstime='2001-02-01')
to_hcc = from_hcc.transform_to(Heliocentric(observer=observer2, obstime='2001-02-01'))
# This change in observer is approximately a 90-degree rotation about the Y axis
assert_quantity_allclose(to_hcc.x, -from_hcc.z, rtol=2e-3)
assert_quantity_allclose(to_hcc.y, from_hcc.y, rtol=2e-3)
assert_quantity_allclose(to_hcc.z, from_hcc.x, rtol=2e-3)
def test_hcc_hgs_observer_mismatch():
# Test whether the transformation gives the same answer regardless of what obstime the observer
# coordinate is represented in
observer1 = HeliographicStonyhurst(0*u.deg, 0*u.deg, 1*u.AU, obstime='2001-01-01')
observer2 = observer1.transform_to(HeliographicStonyhurst(obstime='2001-03-31'))
hcc1 = Heliocentric(0.2*u.AU, 0.3*u.AU, 0.4*u.AU, observer=observer1, obstime=observer1.obstime)
hgs1 = hcc1.transform_to(HeliographicStonyhurst(obstime=hcc1.obstime))
hcc2 = Heliocentric(0.2*u.AU, 0.3*u.AU, 0.4*u.AU, observer=observer2, obstime=observer1.obstime)
hgs2 = hcc2.transform_to(HeliographicStonyhurst(obstime=hcc2.obstime))
assert_quantity_allclose(hgs1.lon, hgs2.lon)
assert_quantity_allclose(hgs1.lat, hgs2.lat)
assert_quantity_allclose(hgs1.radius, hgs2.radius)
def test_hgs_hcc_observer_mismatch():
# Test whether the transformation gives the same answer regardless of what obstime the observer
# coordinate is represented in
observer1 = HeliographicStonyhurst(0*u.deg, 0*u.deg, 1*u.AU, obstime='2001-01-01')
observer2 = observer1.transform_to(HeliographicStonyhurst(obstime='2001-03-31'))
hgs = HeliographicStonyhurst(20*u.deg, 40*u.deg, 0.5*u.AU, obstime=observer1.obstime)
hcc1 = hgs.transform_to(Heliocentric(observer=observer1, obstime=hgs.obstime))
hcc2 = hgs.transform_to(Heliocentric(observer=observer2, obstime=hgs.obstime))
assert_quantity_allclose(hcc1.cartesian.xyz, hcc2.cartesian.xyz)
def test_hgs_hcrs_sunspice():
# Compare our HGS->HCRS transformation against SunSPICE by transforming beyond it
# "HEQ" is another name for HEEQ, which is equivalent to Heliographic Stonyhurst
# "HAE" is equivalent to Astropy's Heliocentric Mean Ecliptic, and defaults to J2000.0
#
# IDL> coord = [1.d, 0.d, 10.d]
# IDL> convert_sunspice_lonlat, '2019-06-01', coord, 'HEQ', 'HAE', /au, /degrees
# IDL> print, coord
# 1.0000000 -108.65371 10.642778
old = SkyCoord(0*u.deg, 10*u.deg, 1*u.AU, frame=HeliographicStonyhurst(obstime='2019-06-01'))
new = old.transform_to(HeliocentricMeanEcliptic)
assert_quantity_allclose(new.lon, Longitude(-108.65371*u.deg), atol=0.1*u.arcsec, rtol=0)
assert_quantity_allclose(new.lat, 10.642778*u.deg, atol=0.1*u.arcsec, rtol=0)
assert_quantity_allclose(new.distance, old.radius)
# Transform to HAE precessed to the mean ecliptic of date instead of J2000.0
# IDL> coord = [1.d, 0.d, 10.d]
# IDL> convert_sunspice_lonlat, '2019-06-01', coord, 'HEQ', 'HAE', /precess, /au, /degrees
# IDL> print, coord
# 1.0000000 -108.38240 10.640314
new = old.transform_to(HeliocentricMeanEcliptic(equinox='2019-06-01'))
assert_quantity_allclose(new.lon, Longitude(-108.38240*u.deg), atol=0.1*u.arcsec, rtol=0)
assert_quantity_allclose(new.lat, 10.640314*u.deg, atol=0.1*u.arcsec, rtol=0)
assert_quantity_allclose(new.distance, old.radius)
def test_hgs_hgc_sunspice():
# Compare our HGS->HGC transformation against SunSPICE
# "HEQ" is another name for HEEQ, which is equivalent to Heliographic Stonyhurst
# "Carrington" does not include light travel time to the observer, which our HGC includes
#
# IDL> coord = [1.d, 0.d, 10.d]
# IDL> convert_sunspice_lonlat, '2019-06-01', coord, 'HEQ', 'Carrington', /au, /degrees
# IDL> print, coord
# 1.0000000 16.688242 10.000000
old = SkyCoord(0*u.deg, 10*u.deg, 1*u.AU, frame=HeliographicStonyhurst(obstime='2019-06-01'))
new = old.transform_to(HeliographicCarrington(observer='earth'))
# Calculate the difference in longitude due to light travel time from the Sun to the Earth
delta_lon = sidereal_rotation_rate * (sun.earth_distance(old.obstime) - _RSUN) / speed_of_light
assert_quantity_allclose(new.lon, 16.688242*u.deg + delta_lon, atol=1e-2*u.arcsec, rtol=0)
assert_quantity_allclose(new.lat, old.lat)
assert_quantity_allclose(new.radius, old.radius)
def test_hgs_hcc_sunspice():
# Compare our HGS->HCC transformation against SunSPICE
# "HEQ" is another name for HEEQ, which is equivalent to Heliographic Stonyhurst
# "HGRTN" is equivalent to our Heliocentric, but with the axes permuted
# SunSPICE, like us, assumes an Earth observer if not explicitly specified
#
# IDL> coord = [7d5, 8d5, 9d5]
# IDL> convert_sunspice_coord, '2019-06-01', coord, 'HEQ', 'HGRTN'
# Assuming Earth observation
# IDL> print, coord
# 688539.32 800000.00 908797.89
old = SkyCoord(CartesianRepresentation([7e5, 8e5, 9e5]*u.km),
frame=HeliographicStonyhurst(obstime='2019-06-01'))
new = old.transform_to(Heliocentric(observer='earth'))
assert_quantity_allclose(new.x, 800000.00*u.km, atol=1e-2*u.km)
assert_quantity_allclose(new.y, 908797.89*u.km, atol=1e-2*u.km)
assert_quantity_allclose(new.z, 688539.32*u.km, atol=1e-2*u.km)
def test_hpc_hgs_implicit_hcc():
# An HPC->HGS transformation should give the same answer whether the transformation step
# through HCC is implicit or explicit
start = SkyCoord(0*u.arcsec, 0*u.arcsec, 0.5*u.AU,
frame=Helioprojective(obstime='2019-06-01', observer='earth'))
frame = HeliographicStonyhurst(obstime='2019-12-01')
implicit = start.transform_to(frame)
explicit1 = start.transform_to(Heliocentric(obstime=start.obstime, observer='earth')).\
transform_to(frame)
explicit2 = start.transform_to(Heliocentric(obstime=frame.obstime, observer='earth')).\
transform_to(frame)
assert_quantity_allclose(implicit.separation_3d(explicit1), 0*u.AU, atol=1e-10*u.AU)
assert_quantity_allclose(implicit.separation_3d(explicit2), 0*u.AU, atol=1e-10*u.AU)
def test_velocity_hcrs_hgs():
# Obtain the position/velocity of Earth in ICRS
obstime = Time(['2019-01-01', '2019-04-01', '2019-07-01', '2019-10-01'])
pos, vel = get_body_barycentric_posvel('earth', obstime)
loc = pos.with_differentials(vel.represent_as(CartesianDifferential))
earth = SkyCoord(loc, frame='icrs', obstime=obstime)
# The velocity of Earth in HGS Y should be very close to zero because the XZ plane tracks
# the Earth.
new = earth.heliographic_stonyhurst
assert_quantity_allclose(new.velocity.d_y, 0*u.km/u.s, atol=1e-5*u.km/u.s)
# Test the loopback to ICRS
newer = new.icrs
assert_quantity_allclose(newer.velocity.d_xyz, vel.xyz)
def test_velocity_hgs_hgc():
# Construct a simple HGS coordinate with zero velocity
obstime = Time(['2019-01-01', '2019-04-01', '2019-07-01', '2019-10-01'])
pos = CartesianRepresentation(1, 0, 0)*u.AU
vel = CartesianDifferential(0, 0, 0)*u.km/u.s
loc = (pos.with_differentials(vel))._apply('repeat', obstime.size)
coord = SkyCoord(HeliographicStonyhurst(loc, obstime=obstime))
# The induced velocity in HGC should be entirely longitudinal, and approximately equal to one
# full rotation every mean synodic period (27.2753 days)
hgc_frame = HeliographicCarrington(observer='earth', obstime=obstime)
new = coord.transform_to(hgc_frame)
new_vel = new.data.differentials['s'].represent_as(SphericalDifferential, new.data)
assert_quantity_allclose(new_vel.d_lon, -360*u.deg / (27.27253*u.day), rtol=1e-2)
assert_quantity_allclose(new_vel.d_lat, 0*u.deg/u.s)
assert_quantity_allclose(new_vel.d_distance, 0*u.km/u.s, atol=1e-7*u.km/u.s)
def test_velocity_hgs_hci():
# HGS and HCI share the same origin and Z axis, so the induced velocity is entirely angular
obstime = Time(['2021-01-01', '2021-04-01', '2021-07-01', '2021-10-01'])
venus_hgs = get_body_heliographic_stonyhurst('venus', obstime, include_velocity=True)
venus_hci = venus_hgs.transform_to(HeliocentricInertial(obstime=obstime))
# The induced velocity is the longitude component of Earth's velocity, ~360 deg/yr
induced_dlon = get_earth(obstime, include_velocity=True).heliocentricinertial.d_lon
assert_quantity_allclose(induced_dlon, 360*u.deg/u.yr, rtol=0.05)
# The HCI velocity should be the same as the HGS velocity except for the induced velocity
assert_quantity_allclose(venus_hci.d_distance, venus_hgs.d_radius, rtol=1e-5)
assert_quantity_allclose(venus_hci.d_lon, venus_hgs.d_lon + induced_dlon, rtol=1e-6)
assert_quantity_allclose(venus_hci.d_lat, venus_hgs.d_lat)
def test_velocity_hcrs_hci():
# HCRS and HCI are both inertial frames with the same origin, so there is no induced velocity.
# There is an induced angular velocity for HCRS->HGS, which should be canceled out by the
# induced angular velocity for HGS->HCI.
# Define an HCRS coordinate with a purely radial velocity
sc_hcrs = SkyCoord(ra=[0, 90, 180, 270]*u.deg, pm_ra_cosdec=[0, 0, 0, 0]*u.deg/u.d,
dec=[10, 20, 30, 40]*u.deg, pm_dec=[0, 0, 0, 0]*u.deg/u.d,
distance=[5, 6, 7, 8]*u.AU, radial_velocity=[1, 2, 3, 4]*u.km/u.s,
frame='hcrs', obstime='2021-01-01')
# Transform to HCI, and get the velocity vector in spherical coordinates
sc_hci = sc_hcrs.heliocentricinertial
# The HCI velocity should have the same amplitude, and should be purely radial
assert_quantity_allclose(sc_hci.d_distance, sc_hcrs.velocity.norm(), rtol=1e-6)
assert_quantity_allclose(sc_hci.d_lon, 0*u.arcsec/u.s, atol=1e-9*u.arcsec/u.s)
assert_quantity_allclose(sc_hci.d_lat, 0*u.arcsec/u.s, atol=1e-9*u.arcsec/u.s)
def test_hme_hee_sunspice():
# Compare our HME->HEE transformation against SunSPICE
# "HAE" is equivalent to Astropy's Heliocentric Mean Ecliptic, and defaults to J2000.0
#
# IDL> coord = [1.d, 0.d, 10.d]
# IDL> convert_sunspice_lonlat, '2019-06-01', coord, 'HAE', 'HEE', /au, /degrees
# IDL> print, coord
# 1.0000000 110.01610 10.000300
old = SkyCoord(0*u.deg, 10*u.deg, 1*u.AU, frame=HeliocentricMeanEcliptic(obstime='2019-06-01'))
new = old.transform_to(HeliocentricEarthEcliptic)
assert_quantity_allclose(new.lon, Longitude(110.01610*u.deg), atol=0.01*u.arcsec, rtol=0)
assert_quantity_allclose(new.lat, 10.000300*u.deg, atol=0.01*u.arcsec, rtol=0)
assert_quantity_allclose(new.distance, old.distance)
# Transform from HAE precessed to the mean ecliptic of date instead of J2000.0
# IDL> coord = [1.d, 0.d, 10.d]
# IDL> convert_sunspice_lonlat, '2019-06-01', coord, 'HAE', 'HEE', /au, /degrees, /precess
# IDL> print, coord
# 1.0000000 109.74535 10.000070
old = SkyCoord(0*u.deg, 10*u.deg, 1*u.AU, frame=HeliocentricMeanEcliptic(obstime='2019-06-01',
equinox='2019-06-01'))
new = old.transform_to(HeliocentricEarthEcliptic)
assert_quantity_allclose(new.lon, Longitude(109.74535*u.deg), atol=0.05*u.arcsec, rtol=0)
assert_quantity_allclose(new.lat, 10.000070*u.deg, atol=0.01*u.arcsec, rtol=0)
assert_quantity_allclose(new.distance, old.distance)
def test_hee_earth():
# The Earth in HEE should have negligible Z component
times = parse_time('2013-08-10 12:00') + np.arange(10) * u.s
earth_hee = get_earth(times).heliocentricearthecliptic
assert_quantity_allclose(0*u.m, earth_hee.cartesian.z, atol=1e-4*u.m)
def test_hee_hee():
# Test HEE loopback transformation
obstime = Time('2001-01-01')
old = SkyCoord(90*u.deg, 10*u.deg, 1*u.AU, frame=HeliocentricEarthEcliptic(obstime=obstime))
new = old.transform_to(HeliocentricEarthEcliptic)
assert_quantity_allclose(new.lon, old.lon)
assert_quantity_allclose(new.lat, old.lat)
assert_quantity_allclose(new.distance, old.distance)
new = old.transform_to(HeliocentricEarthEcliptic(obstime=obstime + 1*u.day))
assert_quantity_allclose(new.lon, old.lon - 1*u.deg, atol=0.1*u.deg) # due to Earth motion
assert_quantity_allclose(new.lat, old.lat, atol=0.5*u.arcsec)
assert_quantity_allclose(new.distance, old.distance, rtol=1e-5)
def test_hee_gse_sunspice():
# Compare our HEE->GSE transformation against SunSPICE
#
# IDL> coord = [0.7d, -20.d, 10.d]
# IDL> convert_sunspice_coord, '2019-06-01', coord, 'HEE', 'GSE', /au, /degrees
# IDL> print, coord
# 0.45215884 32.777377 15.594639
old = SkyCoord(-20*u.deg, 10*u.deg, 0.7*u.AU,
frame=HeliocentricEarthEcliptic(obstime='2019-06-01'))
new = old.geocentricsolarecliptic
assert_quantity_allclose(new.lon, 32.777377*u.deg, atol=0.01*u.arcsec, rtol=0)
assert_quantity_allclose(new.lat, 15.594639*u.deg, atol=0.01*u.arcsec, rtol=0)
assert_quantity_allclose(new.distance, 0.45215884*u.AU)
def test_gse_gse():
# Test GSE loopback transformation
old = SkyCoord(90*u.deg, 10*u.deg, 0.7*u.AU,
frame=GeocentricSolarEcliptic(obstime='2001-01-01'))
new = old.transform_to(GeocentricSolarEcliptic)
assert_quantity_allclose(new.lon, old.lon)
assert_quantity_allclose(new.lat, old.lat)
assert_quantity_allclose(new.distance, old.distance)
def test_hgs_hci_sunspice():
# Compare our HGS->HCI transformation against SunSPICE
# "HEQ" is another name for HEEQ, which is equivalent to Heliographic Stonyhurst
#
# IDL> coord = [1.d, 120.d, 10.d]
# IDL> convert_sunspice_lonlat, '2019-06-01', coord, 'HEQ', 'HCI', /au, /degrees
# IDL> print, coord
# 1.0000000 -65.736793 10.000000
old = SkyCoord(120*u.deg, 10*u.deg, 1*u.AU, frame=HeliographicStonyhurst(obstime='2019-06-01'))
new = old.transform_to(HeliocentricInertial)
assert_quantity_allclose(new.lon, -65.736793*u.deg, atol=0.5*u.arcsec, rtol=0)
assert_quantity_allclose(new.lat, old.lat)
assert_quantity_allclose(new.distance, old.radius)
def test_hci_hci():
# Test HCI loopback transformation
obstime = Time('2001-01-01')
old = SkyCoord(90*u.deg, 10*u.deg, 0.7*u.AU, frame=HeliocentricInertial(obstime=obstime))
new = old.transform_to(HeliocentricInertial)
assert_quantity_allclose(new.lon, old.lon)
assert_quantity_allclose(new.lat, old.lat)
assert_quantity_allclose(new.distance, old.distance)
new = old.transform_to(HeliocentricInertial(obstime=obstime + 1*u.day))
assert_quantity_allclose(new.lon, old.lon, atol=0.1*u.deg) # due to Earth motion
assert_quantity_allclose(new.lat, old.lat, atol=1e-3*u.deg)
assert_quantity_allclose(new.distance, old.distance, atol=1e-5*u.AU)
def test_hme_gei_sunspice():
# Compare our HME->GEI transformation against SunSPICE
# "HAE" is equivalent to Astropy's Heliocentric Mean Ecliptic, and defaults to J2000.0
#
# IDL> coord = [1.d, 120.d, 10.d]
# IDL> convert_sunspice_lonlat, '2019-06-01', coord, 'HAE', 'GEI', /au, /degrees
# IDL> print, coord
# 1.8197210 95.230617 28.830109
old = SkyCoord(120*u.deg, 10*u.deg, 1*u.AU,
frame=HeliocentricMeanEcliptic(obstime='2019-06-01'))
new = old.transform_to(GeocentricEarthEquatorial)
assert_quantity_allclose(new.lon, Longitude(95.230617*u.deg), atol=0.01*u.arcsec, rtol=0)
assert_quantity_allclose(new.lat, 28.830109*u.deg, atol=0.05*u.arcsec, rtol=0)
assert_quantity_allclose(new.distance, 1.8197210*u.AU)
# Transform from HAE precessed to the mean ecliptic of date instead of J2000.0
# IDL> coord = [1.d, 120.d, 10.d]
# IDL> convert_sunspice_lonlat, '2019-06-01', coord, 'HAE', 'GEI', /au, /degrees, /precess
# IDL> print, coord
# 1.8217103 95.079030 28.827750
old = SkyCoord(120*u.deg, 10*u.deg, 1*u.AU,
frame=HeliocentricMeanEcliptic(obstime='2019-06-01', equinox='2019-06-01'))
new = old.transform_to(GeocentricEarthEquatorial(equinox=_J2000))
assert_quantity_allclose(new.lon, Longitude(95.079030*u.deg), atol=0.05*u.arcsec, rtol=0)
assert_quantity_allclose(new.lat, 28.827750*u.deg, atol=0.05*u.arcsec, rtol=0)
assert_quantity_allclose(new.distance, 1.8217103*u.AU)
def test_gei_gse_sunspice():
# Compare our GEI->GSE transformation against SunSPICE
# The GEI in SunSPICE is at epoch J2000.0
#
# IDL> coord = [1.d-3, 120.d, 10.d]
# IDL> convert_sunspice_lonlat, '2019-06-01', coord, 'GEI', 'GSE', /degrees
# IDL> print, coord
# 0.0010000000 50.054253 -10.363626
old = SkyCoord(120*u.deg, 10*u.deg, 1*u.m,
frame=GeocentricEarthEquatorial(obstime='2019-06-01', equinox='J2000.0'))
new = old.transform_to(GeocentricSolarEcliptic)
assert_quantity_allclose(new.lon, 50.054253*u.deg, atol=0.02*u.arcsec, rtol=0)
assert_quantity_allclose(new.lat, -10.363626*u.deg, atol=0.03*u.arcsec, rtol=0)
assert_quantity_allclose(new.distance, 1*u.m)
def test_gei_gei():
# Test GEI loopback transformation using the 2017 revision to Franz & Harper 2002
t = Time('1996-08-28 16:46:00', scale='tt')
gei_j2000 = CartesianRepresentation([-5.7840451, -4.1082375, 1.9146822] * (6378.14*u.km))
gei_d = CartesianRepresentation([-5.7864918, -4.1039136, 1.9165612] * (6378.14*u.km))
old = SkyCoord(gei_j2000, frame=GeocentricEarthEquatorial(obstime=t))
new = old.transform_to(GeocentricEarthEquatorial(equinox=t, obstime=t)).cartesian
assert_quantity_allclose(new.xyz, gei_d.xyz)
# Coordinate transformations from the example in the 2017 revision to Franz & Harper 2002
_franz_harper_example_data = [
(ITRS, [6.9027400, -1.6362400, 1.9166900]),
(GeocentricEarthEquatorial, [-5.7864918, -4.1039136, 1.9165612]),
(GeocentricSolarEcliptic, [4.0378470, 5.1182566, 3.3908764]),
(Geomagnetic, [3.3344557, 6.0215108, 2.5732497]),
(SolarMagnetic, [3.3601371, 6.0071917, 2.5733108]),
(GeocentricSolarMagnetospheric, [4.0378470, 6.0071917, 1.2681645]),
]
@pytest.mark.remote_data
@pytest.mark.parametrize(("start_class", "start_vector"), _franz_harper_example_data)
@pytest.mark.parametrize(("end_class", "end_vector"), _franz_harper_example_data)
def test_geocentric_franz_harper(start_class, start_vector, end_class, end_vector):
t = Time('1996-08-28 16:46:00', scale='tt')
start_repr = CartesianRepresentation(start_vector * (6378.14*u.km))
end_repr = CartesianRepresentation(end_vector * (6378.14*u.km))
start_kwargs = {'equinox': t} if hasattr(start_class, 'equinox') else {}
end_kwargs = {'equinox': t} if hasattr(end_class, 'equinox') else {}
start = SkyCoord(start_repr, frame=start_class(obstime=t, **start_kwargs))
if end_class == start_class:
start = start.itrs
end = start.transform_to(end_class(obstime=t, **end_kwargs))
assert_quantity_allclose(end.cartesian.xyz, end_repr.xyz, rtol=2e-2)
# Coordinate transformations from SunSPICE for the date 2023-10-30
#
# Example for MAG, substitute SM and GSM as appropriate:
# IDL> coord = [0.7d, -20.d, 10.d]
# IDL> convert_sunspice_lonlat, '2017-10-30', coord, 'GEO', 'MAG', /itrf93, /au, /degrees
# IDL> print, coord
_sunspice_data = [
(ITRS, (-20*u.deg, 10*u.deg, 0.7*u.AU)),
(Geomagnetic, (54.400820*u.deg, 15.674828*u.deg, 0.7*u.AU)),
(SolarMagnetic, (163.35062*u.deg, 15.674828*u.deg, 0.7*u.AU)),
(GeocentricSolarMagnetospheric, (163.98552*u.deg, -0.71263503*u.deg, 0.7*u.AU)),
]
@pytest.mark.remote_data
@pytest.mark.parametrize(("start_class", "start_vector"), _sunspice_data)
@pytest.mark.parametrize(("end_class", "end_vector"), _sunspice_data)
def test_magnetic_sunspice(start_class, start_vector, end_class, end_vector):
# Test all magnetic-model frames (MAG, SM, GSM) using the SunSPICE results
t = Time('2017-10-30')
start_repr = SphericalRepresentation(*start_vector)
end_repr = SphericalRepresentation(*end_vector)
start = SkyCoord(start_repr, frame=start_class(obstime=t))
if end_class == start_class:
start = start.itrs
end = start.transform_to(end_class)
assert_quantity_allclose(end.spherical.lon, end_repr.lon, atol=1e-2*u.deg)
assert_quantity_allclose(end.spherical.lat, end_repr.lat, atol=2e-3*u.deg)
assert_quantity_allclose(end.spherical.distance, end_repr.distance)
def test_no_observer():
# Tests transformations to and from observer-based frames with no observer defined
frames_in = [Heliocentric(0*u.km, 0*u.km, 0*u.km, observer=None),
Heliocentric(0*u.km, 0*u.km, 0*u.km, observer=None, obstime='2001-01-01'),
Helioprojective(0*u.deg, 0*u.deg, observer=None),
Helioprojective(0*u.deg, 0*u.deg, observer=None, obstime='2001-01-01')]
frames_out = frames_in + [
HeliographicStonyhurst(0*u.deg, 0*u.deg, obstime=None),
HeliographicStonyhurst(0*u.deg, 0*u.deg, obstime='2001-01-01'),
Heliocentric(0*u.km, 0*u.km, 0*u.km, observer=None, obstime='2012-12-12'),
Heliocentric(0*u.km, 0*u.km, 0*u.km, observer="earth", obstime=None),
Heliocentric(0*u.km, 0*u.km, 0*u.km, observer="earth", obstime='2001-01-01'),
Helioprojective(0*u.deg, 0*u.deg, observer=None, obstime='2012-12-12'),
Helioprojective(0*u.deg, 0*u.deg, observer="earth", obstime=None),
Helioprojective(0*u.deg, 0*u.deg, observer="earth", obstime='2001-01-01')]
# Self-transformations should succeed
for f in frames_in:
f.transform_to(f.replicate_without_data())
# All other transformations should error
for i, f1 in enumerate(frames_in):
for f2 in frames_out[i + 1:]:
with pytest.raises(ConvertError):
f1.transform_to(f2)
with pytest.raises(ConvertError):
f2.transform_to(f1)
def test_array_obstime():
# Validate that you can transform from an array of obstimes to no obstimes,
# or different obstimes.
a = SkyCoord([10]*2, [10]*2, unit=u.deg,
observer="earth",
obstime=["2019-01-01", "2019-01-02"],
frame="heliographic_carrington")
t = a.transform_to(Helioprojective)
assert isinstance(t.frame, Helioprojective)
t2 = a.transform_to(Helioprojective(obstime=["2019-01-03", "2019-01-04"]))
assert isinstance(t2.frame, Helioprojective)
_frames_wo_observer = [HeliographicStonyhurst, HeliocentricInertial,
HeliocentricEarthEcliptic, GeocentricSolarEcliptic,
GeocentricEarthEquatorial]
@pytest.mark.parametrize("frame_class", _frames_wo_observer)
def test_convert_error_with_no_obstime(frame_class):
# For most transformations, we do not allow `obstime` to be `None`
frame = frame_class(CartesianRepresentation(0, 0, 0)*u.km, obstime=None)
with pytest.raises(ConvertError, match=r".*obstime.*"):
ICRS(0*u.deg, 0*u.deg, 0*u.AU).transform_to(frame)
with pytest.raises(ConvertError, match=r".*obstime.*"):
frame.transform_to(ICRS())
# Convenience function to check whether a transformation succeeds if the target `obstime` is `None`
def assert_no_obstime_on_target_end(start_class, end_class):
start_obstime = Time("2001-01-01")
if hasattr(start_class, 'observer'):
coord = start_class(CartesianRepresentation(0, 0, 0)*u.km,
obstime=start_obstime, observer="earth")
else:
coord = start_class(CartesianRepresentation(0, 0, 0)*u.km, obstime=start_obstime)
result = coord.transform_to(end_class(obstime=None))
assert result.obstime == start_obstime
# We currently allow the target `obstime` to be `None` for the transformation subgraph
# below `HeliographicStonyhurst`, but this may change in the future
_frameset1 = [HeliographicStonyhurst, HeliocentricInertial]
_frameset2 = [HeliographicCarrington, Heliocentric, Helioprojective]
@pytest.mark.parametrize("start_class", _frameset1 + _frameset2)
@pytest.mark.parametrize("end_class", _frameset1)
def test_no_obstime_on_target_end_hgs_subgraph(start_class, end_class):
assert_no_obstime_on_target_end(start_class, end_class)
# We currently allow the target `obstime` to be `None` for the HEE loopback,
# but this may change in the future
def test_no_obstime_on_target_end_hee():
assert_no_obstime_on_target_end(HeliocentricEarthEcliptic, HeliocentricEarthEcliptic)
_frameset_geocentric = [
ITRS,
Geomagnetic,
SolarMagnetic,
GeocentricSolarMagnetospheric,
GeocentricEarthEquatorial,
GeocentricSolarEcliptic,
]
@pytest.mark.parametrize("start_class", _frameset_geocentric)
@pytest.mark.parametrize("end_class", _frameset_geocentric)
def test_earth_stays_at_origin_between_geocentric(start_class, end_class):
obstime = Time("2001-01-01")
coord = start_class(CartesianRepresentation(0, 0, 0)*u.km, obstime=obstime)
result = coord.transform_to(end_class(obstime=obstime))
assert_quantity_allclose(result.cartesian.xyz, 0*u.km)
@pytest.mark.parametrize("start_class", _frameset_geocentric)
@pytest.mark.parametrize("end_class", _frameset_geocentric)
def test_no_aberration_between_geocentric(start_class, end_class):
obstime = Time("2001-01-01")
vx = start_class(CartesianRepresentation(1, 0, 0)*u.km, obstime=obstime)
vy = start_class(CartesianRepresentation(0, 1, 0)*u.km, obstime=obstime)
vz = start_class(CartesianRepresentation(0, 0, 1)*u.km, obstime=obstime)
tvx = vx.transform_to(end_class(obstime=obstime)).cartesian
tvy = vy.transform_to(end_class(obstime=obstime)).cartesian
tvz = vz.transform_to(end_class(obstime=obstime)).cartesian
# Verify all vector lengths have not changed
assert_quantity_allclose(tvx.norm(), 1*u.km)
assert_quantity_allclose(tvy.norm(), 1*u.km)
assert_quantity_allclose(tvz.norm(), 1*u.km)
# Verify all vectors are still orthogonal
assert_quantity_allclose(tvx.cross(tvy).norm(), 1*u.km**2)
assert_quantity_allclose(tvy.cross(tvz).norm(), 1*u.km**2)
assert_quantity_allclose(tvx.cross(tvz).norm(), 1*u.km**2)
def test_transform_with_sun_center():
sun_center = SkyCoord(0*u.deg, 0*u.deg, 0*u.AU,
frame=HeliographicStonyhurst(obstime="2001-01-01"))
with transform_with_sun_center():
result1 = sun_center.transform_to(HeliographicStonyhurst(obstime="2001-02-01"))
# The coordinate should stay pointing at Sun center
assert_quantity_allclose(result1.lon, sun_center.lon)
assert_quantity_allclose(result1.lat, sun_center.lat)
assert_quantity_allclose(result1.radius, sun_center.radius)
other = SkyCoord(10*u.deg, 20*u.deg, 1*u.AU,
frame=HeliographicStonyhurst(obstime="2001-01-01"))
with transform_with_sun_center():
result2 = other.transform_to(HeliographicCarrington(observer='earth', obstime="2001-02-01"))
# The coordinate should stay at the same latitude and the same distance from Sun center
assert_quantity_allclose(result2.lat, other.lat)
assert_quantity_allclose(result2.radius, other.radius)
def test_transform_with_sun_center_reset():
# This test sequence ensures that the context manager resets properly
sun_center = SkyCoord(0*u.deg, 0*u.deg, 0*u.AU,
frame=HeliographicStonyhurst(obstime="2001-01-01"))
end_frame = HeliocentricInertial(obstime="2001-02-01")
# Without the context manager, the coordinate should not point at Sun center
result1 = sun_center.transform_to(end_frame)
assert result1.lon != sun_center.lon
assert result1.lat != sun_center.lat
assert result1.distance != sun_center.radius
# Using the context manager, the coordinate should point at Sun center
with transform_with_sun_center():
result2 = sun_center.transform_to(end_frame)
assert_quantity_allclose(result2.lon, sun_center.lon)
assert_quantity_allclose(result2.lat, sun_center.lat)
assert_quantity_allclose(result2.distance, sun_center.radius)
# Exiting a nested context manager should not affect the outer context manager
with transform_with_sun_center():
with transform_with_sun_center():
pass
result2a = sun_center.transform_to(end_frame)
assert_quantity_allclose(result2a.lon, result2.lon)
assert_quantity_allclose(result2a.lat, result2.lat)
assert_quantity_allclose(result2a.distance, result2.distance)
# After the context manager, the coordinate should have the same result as the first transform
result3 = sun_center.transform_to(end_frame)
assert_quantity_allclose(result3.lon, result1.lon)
assert_quantity_allclose(result3.lat, result1.lat)
assert_quantity_allclose(result3.distance, result1.distance)
def test_rsun_preservation():
# Check that rsun is preserved when transforming between any two frames with that attribute
args_in = {'obstime': '2001-01-01', 'rsun': 690*u.Mm}
args_out = {'obstime': '2001-02-01', 'rsun': 700*u.Mm}
coords_in = [Helioprojective(0*u.deg, 0*u.deg, 1*u.AU, observer='earth', **args_in),
HeliographicStonyhurst(0*u.deg, 0*u.deg, 1*u.AU, **args_in),
HeliographicCarrington(0*u.deg, 0*u.deg, 1*u.AU, observer='earth', **args_in)]
for coord in coords_in:
for frame in coords_in:
out_coord = coord.transform_to(frame.replicate(**args_out))
assert_quantity_allclose(out_coord.rsun, args_out['rsun'])
_framepairs = [
('hcrs', 'heliographic_stonyhurst'),
('heliographic_stonyhurst', 'heliographic_carrington'),
('heliographic_stonyhurst', 'heliocentricinertial'),
('heliographic_stonyhurst', 'heliocentric'),
('heliocentric', 'helioprojective'),
('heliocentricmeanecliptic', 'heliocentricearthecliptic'),
('heliocentricearthecliptic', 'geocentricsolarecliptic'),
('heliocentricmeanecliptic', 'geocentricearthequatorial'),
('itrs', 'geomagnetic'),
('geomagnetic', 'solarmagnetic'),
('solarmagnetic', 'geocentricsolarmagnetospheric'),
]
@pytest.mark.parametrize(("frame1", "frame2"), _framepairs)
@pytest.mark.parametrize("unit", [u.m, u.AU])
@pytest.mark.remote_data
def test_unit_preservation(frame1, frame2, unit):
coord = SkyCoord(CartesianRepresentation(0, 0, 0) * unit,
frame=frame1, obstime="2001-01-01", observer="earth")
# Transform one direction and verify the unit is preserved
result1 = coord.transform_to(frame2)
assert result1.cartesian.xyz.unit == unit
# Transform back and verify the unit is preserved
result2 = result1.transform_to(frame1)
assert result2.cartesian.xyz.unit == unit
def test_propagate_with_solar_surface():
# Test propagating the meridian by 6 days of solar rotation
meridian = SkyCoord(0*u.deg, np.arange(0, 90, 10)*u.deg, 1*u.AU,
frame=HeliocentricInertial, obstime='2001-01-01')
dt = 6*u.day
end_frame = HeliocentricInertial(obstime=meridian.obstime + dt)
# Without the context manager
result1 = meridian.transform_to(end_frame)
assert u.allclose(result1.lon, 0*u.deg, atol=1e-1*u.deg) # no rotation with the solar surface
assert not u.allclose(result1.lon, 0*u.deg, atol=1e-3*u.deg) # some change due to translation
assert u.allclose(result1.lat, meridian.lat, atol=1e-2*u.deg)
# Using the context manager (also test default rotation model is 'howard')
with propagate_with_solar_surface():
result2 = meridian.transform_to(end_frame)
assert u.allclose(result2.lon, differential_rotation(dt, meridian.lat, model='howard'))
# Check that nesting the context manager doesn't confuse anything (also test other models)
with propagate_with_solar_surface('snodgrass'):
with propagate_with_solar_surface('allen'):
pass
result3 = meridian.transform_to(end_frame) # should use 'snodgrass', not 'allen'
assert u.allclose(result3.lon, differential_rotation(dt, meridian.lat, model='snodgrass'))
# After the context manager, the coordinate should have the same result as the first transform
result4 = meridian.transform_to(end_frame)
assert_quantity_allclose(result4.lon, result1.lon)
assert_quantity_allclose(result4.lat, result1.lat)
assert_quantity_allclose(result4.distance, result1.distance)
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