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# -*- coding: utf-8 -*-
# Licensed under a 3-clause BSD style license - see LICENSE.rst
from __future__ import (absolute_import, division, print_function,
unicode_literals)
from copy import deepcopy
import numpy as np
from ... import units as u
from ...extern import six
from ...tests.helper import (pytest, quantity_allclose as allclose,
assert_quantity_allclose as assert_allclose)
from ...utils import OrderedDescriptorContainer
from .. import representation
from ..representation import REPRESENTATION_CLASSES
def setup_function(func):
func.REPRESENTATION_CLASSES_ORIG = deepcopy(REPRESENTATION_CLASSES)
def teardown_function(func):
REPRESENTATION_CLASSES.clear()
REPRESENTATION_CLASSES.update(func.REPRESENTATION_CLASSES_ORIG)
def test_frame_attribute_descriptor():
""" Unit tests of the FrameAttribute descriptor """
from ..baseframe import FrameAttribute
@six.add_metaclass(OrderedDescriptorContainer)
class TestFrameAttributes(object):
attr_none = FrameAttribute()
attr_2 = FrameAttribute(default=2)
attr_3_attr2 = FrameAttribute(default=3, secondary_attribute='attr_2')
attr_none_attr2 = FrameAttribute(default=None, secondary_attribute='attr_2')
attr_none_nonexist = FrameAttribute(default=None, secondary_attribute='nonexist')
t = TestFrameAttributes()
# Defaults
assert t.attr_none is None
assert t.attr_2 == 2
assert t.attr_3_attr2 == 3
assert t.attr_none_attr2 == t.attr_2
assert t.attr_none_nonexist is None # No default and non-existent secondary attr
# Setting values via '_'-prefixed internal vars (as would normally done in __init__)
t._attr_none = 10
assert t.attr_none == 10
t._attr_2 = 20
assert t.attr_2 == 20
assert t.attr_3_attr2 == 3
assert t.attr_none_attr2 == t.attr_2
t._attr_none_attr2 = 40
assert t.attr_none_attr2 == 40
# Make sure setting values via public attribute fails
with pytest.raises(AttributeError) as err:
t.attr_none = 5
assert 'Cannot set frame attribute' in str(err)
def test_frame_subclass_attribute_descriptor():
from ..builtin_frames import FK4
from ..baseframe import FrameAttribute, TimeFrameAttribute
from astropy.time import Time
_EQUINOX_B1980 = Time('B1980', scale='tai')
class MyFK4(FK4):
# equinox inherited from FK4, obstime overridden, and newattr is new
obstime = TimeFrameAttribute(default=_EQUINOX_B1980)
newattr = FrameAttribute(default='newattr')
mfk4 = MyFK4()
assert mfk4.equinox.value == 'B1950.000'
assert mfk4.obstime.value == 'B1980.000'
assert mfk4.newattr == 'newattr'
assert set(mfk4.get_frame_attr_names()) == set(['equinox', 'obstime', 'newattr'])
mfk4 = MyFK4(equinox='J1980.0', obstime='J1990.0', newattr='world')
assert mfk4.equinox.value == 'J1980.000'
assert mfk4.obstime.value == 'J1990.000'
assert mfk4.newattr == 'world'
def test_create_data_frames():
from ..builtin_frames import ICRS
#from repr
i1 = ICRS(representation.SphericalRepresentation(1*u.deg, 2*u.deg, 3*u.kpc))
i2 = ICRS(representation.UnitSphericalRepresentation(lon=1*u.deg, lat=2*u.deg))
#from preferred name
i3 = ICRS(ra=1*u.deg, dec=2*u.deg, distance=3*u.kpc)
i4 = ICRS(ra=1*u.deg, dec=2*u.deg)
assert i1.data.lat == i3.data.lat
assert i1.data.lon == i3.data.lon
assert i1.data.distance == i3.data.distance
assert i2.data.lat == i4.data.lat
assert i2.data.lon == i4.data.lon
#now make sure the preferred names work as properties
assert_allclose(i1.ra, i3.ra)
assert_allclose(i2.ra, i4.ra)
assert_allclose(i1.distance, i3.distance)
with pytest.raises(AttributeError):
i1.ra = [11.]*u.deg
def test_create_orderered_data():
from ..builtin_frames import ICRS, Galactic, AltAz
TOL = 1e-10*u.deg
i = ICRS(1*u.deg, 2*u.deg)
assert (i.ra - 1*u.deg) < TOL
assert (i.dec - 2*u.deg) < TOL
g = Galactic(1*u.deg, 2*u.deg)
assert (g.l - 1*u.deg) < TOL
assert (g.b - 2*u.deg) < TOL
a = AltAz(1*u.deg, 2*u.deg)
assert (a.az - 1*u.deg) < TOL
assert (a.alt - 2*u.deg) < TOL
with pytest.raises(TypeError):
ICRS(1*u.deg, 2*u.deg, 1*u.deg, 2*u.deg)
with pytest.raises(TypeError):
sph = representation.SphericalRepresentation(1*u.deg, 2*u.deg, 3*u.kpc)
ICRS(sph, 1*u.deg, 2*u.deg)
def test_create_nodata_frames():
from ..builtin_frames import ICRS, FK4, FK5
i = ICRS()
assert len(i.get_frame_attr_names()) == 0
f5 = FK5()
assert f5.equinox == FK5.get_frame_attr_names()['equinox']
f4 = FK4()
assert f4.equinox == FK4.get_frame_attr_names()['equinox']
#obstime is special because it's a property that uses equinox if obstime is not set
assert f4.obstime in (FK4.get_frame_attr_names()['obstime'],
FK4.get_frame_attr_names()['equinox'])
def test_no_data_nonscalar_frames():
from ..builtin_frames import AltAz
from astropy.time import Time
a1 = AltAz(obstime=Time('2012-01-01') + np.arange(10.) * u.day,
temperature=np.ones((3, 1)) * u.deg_C)
assert a1.obstime.shape == (3, 10)
assert a1.temperature.shape == (3, 10)
assert a1.shape == (3, 10)
with pytest.raises(ValueError) as exc:
AltAz(obstime=Time('2012-01-01') + np.arange(10.) * u.day,
temperature=np.ones((3,)) * u.deg_C)
assert 'inconsistent shapes' in str(exc)
def test_frame_repr():
from ..builtin_frames import ICRS, FK5
i = ICRS()
assert repr(i) == '<ICRS Frame>'
f5 = FK5()
assert repr(f5).startswith('<FK5 Frame (equinox=')
i2 = ICRS(ra=1*u.deg, dec=2*u.deg)
i3 = ICRS(ra=1*u.deg, dec=2*u.deg, distance=3*u.kpc)
assert repr(i2) == ('<ICRS Coordinate: (ra, dec) in deg\n'
' ( 1., 2.)>')
assert repr(i3) == ('<ICRS Coordinate: (ra, dec, distance) in (deg, deg, kpc)\n'
' ( 1., 2., 3.)>')
# try with arrays
i2 = ICRS(ra=[1.1,2.1]*u.deg, dec=[2.1,3.1]*u.deg)
i3 = ICRS(ra=[1.1,2.1]*u.deg, dec=[-15.6,17.1]*u.deg, distance=[11.,21.]*u.kpc)
assert repr(i2) == ('<ICRS Coordinate: (ra, dec) in deg\n'
' [( 1.1, 2.1), ( 2.1, 3.1)]>')
assert repr(i3) == ('<ICRS Coordinate: (ra, dec, distance) in (deg, deg, kpc)\n'
' [( 1.1, -15.6, 11.), ( 2.1, 17.1, 21.)]>')
def test_converting_units():
import re
from ..baseframe import RepresentationMapping
from ..builtin_frames import ICRS, FK5
# this is a regular expression that with split (see below) removes what's
# the decimal point to fix rounding problems
rexrepr = re.compile(r'(.*?=\d\.).*?( .*?=\d\.).*?( .*)')
# Use values that aren't subject to rounding down to X.9999...
i2 = ICRS(ra=2.*u.deg, dec=2.*u.deg)
i2_many = ICRS(ra=[2.,4.]*u.deg, dec=[2.,-8.1]*u.deg)
#converting from FK5 to ICRS and back changes the *internal* representation,
# but it should still come out in the preferred form
i4 = i2.transform_to(FK5).transform_to(ICRS)
i4_many = i2_many.transform_to(FK5).transform_to(ICRS)
ri2 = ''.join(rexrepr.split(repr(i2)))
ri4 = ''.join(rexrepr.split(repr(i4)))
assert ri2 == ri4
assert i2.data.lon.unit != i4.data.lon.unit # Internal repr changed
ri2_many = ''.join(rexrepr.split(repr(i2_many)))
ri4_many = ''.join(rexrepr.split(repr(i4_many)))
assert ri2_many == ri4_many
assert i2_many.data.lon.unit != i4_many.data.lon.unit # Internal repr changed
#but that *shouldn't* hold if we turn off units for the representation
class FakeICRS(ICRS):
frame_specific_representation_info = {
'spherical': {'names': ('ra', 'dec', 'distance'),
'units': (None, None, None)},
'unitspherical': {'names': ('ra', 'dec'),
'units': (None, None)}
}
frame_specific_representation_info = {
'spherical': [RepresentationMapping('lon', 'ra', u.hourangle),
RepresentationMapping('lat', 'dec', None),
RepresentationMapping('distance', 'distance')] # should fall back to default of None unit
}
frame_specific_representation_info['unitspherical'] = \
frame_specific_representation_info['spherical']
fi = FakeICRS(i4.data)
ri2 = ''.join(rexrepr.split(repr(i2)))
rfi = ''.join(rexrepr.split(repr(fi)))
rfi = re.sub('FakeICRS', 'ICRS', rfi) # Force frame name to match
assert ri2 != rfi
# the attributes should also get the right units
assert i2.dec.unit == i4.dec.unit
# unless no/explicitly given units
assert i2.dec.unit != fi.dec.unit
assert i2.ra.unit != fi.ra.unit
assert fi.ra.unit == u.hourangle
def test_realizing():
from ..builtin_frames import ICRS, FK5
from ...time import Time
rep = representation.SphericalRepresentation(1*u.deg, 2*u.deg, 3*u.kpc)
i = ICRS()
i2 = i.realize_frame(rep)
assert not i.has_data
assert i2.has_data
f = FK5(equinox=Time('J2001', scale='utc'))
f2 = f.realize_frame(rep)
assert not f.has_data
assert f2.has_data
assert f2.equinox == f.equinox
assert f2.equinox != FK5.get_frame_attr_names()['equinox']
def test_getitem():
from ..builtin_frames import ICRS
rep = representation.SphericalRepresentation(
[1, 2, 3]*u.deg, [4, 5, 6]*u.deg, [7, 8, 9]*u.kpc)
i = ICRS(rep)
assert len(i.ra) == 3
iidx = i[1:]
assert len(iidx.ra) == 2
iidx2 = i[0]
assert iidx2.ra.isscalar
def test_transform():
"""
This test just makes sure the transform architecture works, but does *not*
actually test all the builtin transforms themselves are accurate
"""
from ..builtin_frames import ICRS, FK4, FK5, Galactic
from ...time import Time
i = ICRS(ra=[1, 2]*u.deg, dec=[3, 4]*u.deg)
f = i.transform_to(FK5)
i2 = f.transform_to(ICRS)
assert i2.data.__class__ == representation.UnitSphericalRepresentation
assert_allclose(i.ra, i2.ra)
assert_allclose(i.dec, i2.dec)
i = ICRS(ra=[1, 2]*u.deg, dec=[3, 4]*u.deg, distance=[5, 6]*u.kpc)
f = i.transform_to(FK5)
i2 = f.transform_to(ICRS)
assert i2.data.__class__ != representation.UnitSphericalRepresentation
f = FK5(ra=1*u.deg, dec=2*u.deg, equinox=Time('J2001', scale='utc'))
f4 = f.transform_to(FK4)
f4_2 = f.transform_to(FK4(equinox=f.equinox))
#make sure attributes are copied over correctly
assert f4.equinox == FK4.get_frame_attr_names()['equinox']
assert f4_2.equinox == f.equinox
#make sure self-transforms also work
i = ICRS(ra=[1, 2]*u.deg, dec=[3, 4]*u.deg)
i2 = i.transform_to(ICRS)
assert_allclose(i.ra, i2.ra)
assert_allclose(i.dec, i2.dec)
f = FK5(ra=1*u.deg, dec=2*u.deg, equinox=Time('J2001', scale='utc'))
f2 = f.transform_to(FK5) # default equinox, so should be *different*
assert f2.equinox == FK5().equinox
with pytest.raises(AssertionError):
assert_allclose(f.ra, f2.ra)
with pytest.raises(AssertionError):
assert_allclose(f.dec, f2.dec)
#finally, check Galactic round-tripping
i1 = ICRS(ra=[1, 2]*u.deg, dec=[3, 4]*u.deg)
i2 = i1.transform_to(Galactic).transform_to(ICRS)
assert_allclose(i1.ra, i2.ra)
assert_allclose(i1.dec, i2.dec)
def test_transform_to_nonscalar_nodata_frame():
# https://github.com/astropy/astropy/pull/5254#issuecomment-241592353
from ..builtin_frames import ICRS, FK5
from ...time import Time
times = Time('2016-08-23') + np.linspace(0,10,12)*u.day
coo1 = ICRS(ra=[[0.], [10.], [20.]]*u.deg,
dec=[[-30.], [30.], [60.]]*u.deg)
coo2 = coo1.transform_to(FK5(equinox=times))
assert coo2.shape == (3, 12)
def test_sep():
from ..builtin_frames import ICRS
i1 = ICRS(ra=0*u.deg, dec=1*u.deg)
i2 = ICRS(ra=0*u.deg, dec=2*u.deg)
sep = i1.separation(i2)
assert sep.deg == 1
i3 = ICRS(ra=[1, 2]*u.deg, dec=[3, 4]*u.deg, distance=[5, 6]*u.kpc)
i4 = ICRS(ra=[1, 2]*u.deg, dec=[3, 4]*u.deg, distance=[4, 5]*u.kpc)
sep3d = i3.separation_3d(i4)
assert_allclose(sep3d.to(u.kpc), np.array([1, 1])*u.kpc)
def test_time_inputs():
"""
Test validation and conversion of inputs for equinox and obstime attributes.
"""
from ...time import Time
from ..builtin_frames import FK4
c = FK4(1 * u.deg, 2 * u.deg, equinox='J2001.5', obstime='2000-01-01 12:00:00')
assert c.equinox == Time('J2001.5')
assert c.obstime == Time('2000-01-01 12:00:00')
with pytest.raises(ValueError) as err:
c = FK4(1 * u.deg, 2 * u.deg, equinox=1.5)
assert 'Invalid time input' in str(err)
with pytest.raises(ValueError) as err:
c = FK4(1 * u.deg, 2 * u.deg, obstime='hello')
assert 'Invalid time input' in str(err)
# A vector time should work if the shapes match, but we don't automatically
# broadcast the basic data (just like time).
FK4([1, 2]* u.deg, [2, 3] * u.deg, obstime=['J2000', 'J2001'])
with pytest.raises(ValueError) as err:
FK4(1 * u.deg, 2 * u.deg, obstime=['J2000', 'J2001'])
assert 'shape' in str(err)
def test_is_frame_attr_default():
"""
Check that the `is_frame_attr_default` machinery works as expected
"""
from ...time import Time
from ..builtin_frames import FK5
c1 = FK5(ra=1*u.deg, dec=1*u.deg)
c2 = FK5(ra=1*u.deg, dec=1*u.deg, equinox=FK5.get_frame_attr_names()['equinox'])
c3 = FK5(ra=1*u.deg, dec=1*u.deg, equinox=Time('J2001.5'))
assert c1.equinox == c2.equinox
assert c1.equinox != c3.equinox
assert c1.is_frame_attr_default('equinox')
assert not c2.is_frame_attr_default('equinox')
assert not c3.is_frame_attr_default('equinox')
c4 = c1.realize_frame(representation.UnitSphericalRepresentation(3*u.deg, 4*u.deg))
c5 = c2.realize_frame(representation.UnitSphericalRepresentation(3*u.deg, 4*u.deg))
assert c4.is_frame_attr_default('equinox')
assert not c5.is_frame_attr_default('equinox')
def test_altaz_attributes():
from ...time import Time
from .. import EarthLocation, AltAz
aa = AltAz(1*u.deg, 2*u.deg)
assert aa.obstime is None
assert aa.location is None
aa2 = AltAz(1*u.deg, 2*u.deg, obstime='J2000')
assert aa2.obstime == Time('J2000')
aa3 = AltAz(1*u.deg, 2*u.deg, location=EarthLocation(0*u.deg, 0*u.deg, 0*u.m))
assert isinstance(aa3.location, EarthLocation)
def test_representation():
"""
Test the getter and setter properties for `representation`
"""
from ..builtin_frames import ICRS
# Create the frame object.
icrs = ICRS(ra=1*u.deg, dec=1*u.deg)
data = icrs.data
# Create some representation objects.
icrs_cart = icrs.cartesian
icrs_spher = icrs.spherical
# Testing when `_representation` set to `CartesianRepresentation`.
icrs.representation = representation.CartesianRepresentation
assert icrs.representation == representation.CartesianRepresentation
assert icrs_cart.x == icrs.x
assert icrs_cart.y == icrs.y
assert icrs_cart.z == icrs.z
assert icrs.data == data
# Testing that an ICRS object in CartesianRepresentation must not have spherical attributes.
for attr in ('ra', 'dec', 'distance'):
with pytest.raises(AttributeError) as err:
getattr(icrs, attr)
assert 'object has no attribute' in str(err)
# Testing when `_representation` set to `CylindricalRepresentation`.
icrs.representation = representation.CylindricalRepresentation
assert icrs.representation == representation.CylindricalRepresentation
assert icrs.data == data
# Testing setter input using text argument for spherical.
icrs.representation = 'spherical'
assert icrs.representation is representation.SphericalRepresentation
assert icrs_spher.lat == icrs.dec
assert icrs_spher.lon == icrs.ra
assert icrs_spher.distance == icrs.distance
assert icrs.data == data
# Testing that an ICRS object in SphericalRepresentation must not have cartesian attributes.
for attr in ('x', 'y', 'z'):
with pytest.raises(AttributeError) as err:
getattr(icrs, attr)
assert 'object has no attribute' in str(err)
# Testing setter input using text argument for cylindrical.
icrs.representation = 'cylindrical'
assert icrs.representation is representation.CylindricalRepresentation
assert icrs.data == data
with pytest.raises(ValueError) as err:
icrs.representation = 'WRONG'
assert 'but must be a BaseRepresentation class' in str(err)
with pytest.raises(ValueError) as err:
icrs.representation = ICRS
assert 'but must be a BaseRepresentation class' in str(err)
def test_represent_as():
from ..builtin_frames import ICRS
icrs = ICRS(ra=1*u.deg, dec=1*u.deg)
cart1 = icrs.represent_as('cartesian')
cart2 = icrs.represent_as(representation.CartesianRepresentation)
cart1.x == cart2.x
cart1.y == cart2.y
cart1.z == cart2.z
def test_dynamic_attrs():
from ..builtin_frames import ICRS
c = ICRS(1*u.deg, 2*u.deg)
assert 'ra' in dir(c)
assert 'dec' in dir(c)
with pytest.raises(AttributeError) as err:
c.blahblah
assert "object has no attribute 'blahblah'" in str(err)
with pytest.raises(AttributeError) as err:
c.ra = 1
assert "Cannot set any frame attribute" in str(err)
c.blahblah = 1
assert c.blahblah == 1
def test_nodata_error():
from ..builtin_frames import ICRS
i = ICRS()
with pytest.raises(ValueError) as excinfo:
i.data
assert 'does not have associated data' in str(excinfo.value)
def test_len0_data():
from ..builtin_frames import ICRS
i = ICRS([]*u.deg, []*u.deg)
assert i.has_data
repr(i)
def test_quantity_attributes():
from ..builtin_frames import GCRS
#make sure we can create a GCRS frame with valid inputs
GCRS(obstime='J2002', obsgeoloc=[1, 2, 3]*u.km, obsgeovel=[4, 5, 6]*u.km/u.s)
#make sure it fails for invalid lovs or vels
with pytest.raises(TypeError):
GCRS(obsgeoloc=[1, 2, 3]) #no unit
with pytest.raises(u.UnitsError):
GCRS(obsgeoloc=[1, 2, 3]*u.km/u.s) #incorrect unit
with pytest.raises(ValueError):
GCRS(obsgeoloc=[1, 3]*u.km) #incorrect shape
def test_eloc_attributes():
from .. import AltAz, ITRS, GCRS, EarthLocation
el = EarthLocation(lon=12.3*u.deg, lat=45.6*u.deg, height=1*u.km)
it = ITRS(representation.SphericalRepresentation(lon=12.3*u.deg, lat=45.6*u.deg, distance=1*u.km))
gc = GCRS(ra=12.3*u.deg, dec=45.6*u.deg, distance=6375*u.km)
el1 = AltAz(location=el).location
assert isinstance(el1, EarthLocation)
# these should match *exactly* because the EarthLocation
assert el1.latitude == el.latitude
assert el1.longitude == el.longitude
assert el1.height == el.height
el2 = AltAz(location=it).location
assert isinstance(el2, EarthLocation)
# these should *not* match because giving something in Spherical ITRS is
# *not* the same as giving it as an EarthLocation: EarthLocation is on an
# elliptical geoid. So the longitude should match (because flattening is
# only along the z-axis), but latitude should not. Also, height is relative
# to the *surface* in EarthLocation, but the ITRS distance is relative to
# the center of the Earth
assert not allclose(el2.latitude, it.spherical.lat)
assert allclose(el2.longitude, it.spherical.lon)
assert el2.height < -6000*u.km
el3 = AltAz(location=gc).location
# GCRS inputs implicitly get transformed to ITRS and then onto
# EarthLocation's elliptical geoid. So both lat and lon shouldn't match
assert isinstance(el3, EarthLocation)
assert not allclose(el3.latitude, gc.dec)
assert not allclose(el3.longitude, gc.ra)
assert np.abs(el3.height) < 500*u.km
def test_equivalent_frames():
from .. import SkyCoord
from ..builtin_frames import ICRS, FK4, FK5, AltAz
i = ICRS()
i2 = ICRS(1*u.deg, 2*u.deg)
assert i.is_equivalent_frame(i)
assert i.is_equivalent_frame(i2)
with pytest.raises(TypeError):
assert i.is_equivalent_frame(10)
with pytest.raises(TypeError):
assert i2.is_equivalent_frame(SkyCoord(i2))
f1 = FK5()
f2 = FK5(1*u.deg, 2*u.deg, equinox='J2000')
f3 = FK5(equinox='J2010')
f4 = FK4(equinox='J2010')
assert f1.is_equivalent_frame(f1)
assert not i.is_equivalent_frame(f1)
assert f1.is_equivalent_frame(f2)
assert not f1.is_equivalent_frame(f3)
assert not f3.is_equivalent_frame(f4)
aa1 = AltAz()
aa2 = AltAz(obstime='J2010')
assert aa2.is_equivalent_frame(aa2)
assert not aa1.is_equivalent_frame(i)
assert not aa1.is_equivalent_frame(aa2)
def test_representation_subclass():
# Regression test for #3354
from ..builtin_frames import FK5
# Normally when instantiating a frame without a distance the frame will try
# and use UnitSphericalRepresentation internally instead of
# SphericalRepresentation.
frame = FK5(representation=representation.SphericalRepresentation, ra=32 * u.deg, dec=20 * u.deg)
assert type(frame._data) == representation.UnitSphericalRepresentation
assert frame.representation == representation.SphericalRepresentation
# If using a SphericalRepresentation class this used to not work, so we
# test here that this is now fixed.
class NewSphericalRepresentation(representation.SphericalRepresentation):
attr_classes = representation.SphericalRepresentation.attr_classes
frame = FK5(representation=NewSphericalRepresentation, lon=32 * u.deg, lat=20 * u.deg)
assert type(frame._data) == representation.UnitSphericalRepresentation
assert frame.representation == NewSphericalRepresentation
# A similar issue then happened in __repr__ with subclasses of
# SphericalRepresentation.
assert repr(frame) == ("<FK5 Coordinate (equinox=J2000.000): (lon, lat) in deg\n"
" ( 32., 20.)>")
# A more subtle issue is when specifying a custom
# UnitSphericalRepresentation subclass for the data and
# SphericalRepresentation or a subclass for the representation.
class NewUnitSphericalRepresentation(representation.UnitSphericalRepresentation):
attr_classes = representation.UnitSphericalRepresentation.attr_classes
def __repr__(self):
return "<NewUnitSphericalRepresentation: spam spam spam>"
frame = FK5(NewUnitSphericalRepresentation(lon=32 * u.deg, lat=20 * u.deg),
representation=NewSphericalRepresentation)
assert repr(frame) == "<FK5 Coordinate (equinox=J2000.000): spam spam spam>"
def test_getitem_representation():
"""
Make sure current representation survives __getitem__ even if different
from data representation.
"""
from ..builtin_frames import ICRS
c = ICRS([1, 1] * u.deg, [2, 2] * u.deg)
c.representation = 'cartesian'
assert c[0].representation is representation.CartesianRepresentation
def test_component_error_useful():
"""
Check that a data-less frame gives useful error messages about not having
data when the attributes asked for are possible coordinate components
"""
from ..builtin_frames import ICRS
i = ICRS()
with pytest.raises(ValueError) as excinfo:
i.ra
assert 'does not have associated data' in str(excinfo.value)
with pytest.raises(AttributeError) as excinfo1:
i.foobar
with pytest.raises(AttributeError) as excinfo2:
i.lon # lon is *not* the component name despite being the underlying representation's name
assert "object has no attribute 'foobar'" in str(excinfo1.value)
assert "object has no attribute 'lon'" in str(excinfo2.value)
def test_cache_clear():
from ..builtin_frames import ICRS
i = ICRS(1*u.deg, 2*u.deg)
# Add an in frame units version of the rep to the cache.
repr(i)
assert len(i.cache['representation']) == 2
i.cache.clear()
assert len(i.cache['representation']) == 0
def test_inplace_array():
from ..builtin_frames import ICRS
i = ICRS([[1, 2], [3, 4]]*u.deg, [[10, 20], [30, 40]]*u.deg)
# Add an in frame units version of the rep to the cache.
repr(i)
# Check that repr() has added a rep to the cache
assert len(i.cache['representation']) == 2
# Modify the data
i.data.lon[:, 0] = [100, 200]*u.deg
# Clear the cache
i.cache.clear()
# This will use a second (potentially cached rep)
assert_allclose(i.ra, [[100, 2], [200, 4]]*u.deg)
assert_allclose(i.dec, [[10, 20], [30, 40]]*u.deg)
def test_inplace_change():
from ..builtin_frames import ICRS
i = ICRS(1*u.deg, 2*u.deg)
# Add an in frame units version of the rep to the cache.
repr(i)
# Check that repr() has added a rep to the cache
assert len(i.cache['representation']) == 2
# Modify the data
i.data.lon[()] = 10*u.deg
# Clear the cache
i.cache.clear()
# This will use a second (potentially cached rep)
assert i.ra == 10 * u.deg
assert i.dec == 2 * u.deg
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