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# Licensed under a 3-clause BSD style license - see LICENSE.rst
from math import cos, sin
import pytest
import numpy as np
from numpy.testing import assert_allclose
import astropy.units as u
from astropy.tests.helper import assert_quantity_allclose
from astropy.modeling import models
from astropy.wcs import wcs
@pytest.mark.parametrize(('inp'), [(0, 0), (4000, -20.56), (-2001.5, 45.9),
(0, 90), (0, -90), (np.mgrid[:4, :6])])
def test_against_wcslib(inp):
w = wcs.WCS()
crval = [202.4823228, 47.17511893]
w.wcs.crval = crval
w.wcs.ctype = ['RA---TAN', 'DEC--TAN']
lonpole = 180
tan = models.Pix2Sky_TAN()
n2c = models.RotateNative2Celestial(crval[0], crval[1], lonpole)
c2n = models.RotateCelestial2Native(crval[0], crval[1], lonpole)
m = tan | n2c
minv = c2n | tan.inverse
radec = w.wcs_pix2world(inp[0], inp[1], 1)
xy = w.wcs_world2pix(radec[0], radec[1], 1)
assert_allclose(m(*inp), radec, atol=1e-12)
assert_allclose(minv(*radec), xy, atol=1e-12)
@pytest.mark.parametrize(('inp'), [(0, 0), (40, -20.56), (21.5, 45.9)])
def test_roundtrip_sky_rotaion(inp):
lon, lat, lon_pole = 42, 43, 44
n2c = models.RotateNative2Celestial(lon, lat, lon_pole)
c2n = models.RotateCelestial2Native(lon, lat, lon_pole)
assert_allclose(n2c.inverse(*n2c(*inp)), inp, atol=1e-13)
assert_allclose(c2n.inverse(*c2n(*inp)), inp, atol=1e-13)
def test_native_celestial_lat90():
n2c = models.RotateNative2Celestial(1, 90, 0)
alpha, delta = n2c(1, 1)
assert_allclose(delta, 1)
assert_allclose(alpha, 182)
def test_Rotation2D():
model = models.Rotation2D(angle=90)
x, y = model(1, 0)
assert_allclose([x, y], [0, 1], atol=1e-10)
def test_Rotation2D_quantity():
model = models.Rotation2D(angle=90*u.deg)
x, y = model(1*u.deg, 0*u.arcsec)
assert_quantity_allclose([x, y], [0, 1]*u.deg, atol=1e-10*u.deg)
def test_Rotation2D_inverse():
model = models.Rotation2D(angle=234.23494)
x, y = model.inverse(*model(1, 0))
assert_allclose([x, y], [1, 0], atol=1e-10)
def test_euler_angle_rotations():
x = (0, 0)
y = (90, 0)
z = (0, 90)
negx = (180, 0)
negy = (-90, 0)
# rotate y into minus z
model = models.EulerAngleRotation(0, 90, 0, 'zxz')
assert_allclose(model(*z), y, atol=10**-12)
# rotate z into minus x
model = models.EulerAngleRotation(0, 90, 0, 'zyz')
assert_allclose(model(*z), negx, atol=10**-12)
# rotate x into minus y
model = models.EulerAngleRotation(0, 90, 0, 'yzy')
assert_allclose(model(*x), negy, atol=10**-12)
euler_axes_order = ['zxz', 'zyz', 'yzy', 'yxy', 'xyx', 'xzx']
@pytest.mark.parametrize(('axes_order'), euler_axes_order)
def test_euler_angles(axes_order):
"""
Tests against all Euler sequences.
The rotation matrices definitions come from Wikipedia.
"""
phi = np.deg2rad(23.4)
theta = np.deg2rad(12.2)
psi = np.deg2rad(34)
c1 = cos(phi)
c2 = cos(theta)
c3 = cos(psi)
s1 = sin(phi)
s2 = sin(theta)
s3 = sin(psi)
matrices = {'zxz': np.array([[(c1*c3 - c2*s1*s3), (-c1*s3 - c2*c3*s1), (s1*s2)],
[(c3*s1 + c1*c2*s3), (c1*c2*c3 - s1*s3), (-c1*s2)],
[(s2*s3), (c3*s2), (c2)]]),
'zyz': np.array([[(c1*c2*c3 - s1*s3), (-c3*s1 - c1*c2*s3), (c1*s2)],
[(c1*s3 + c2*c3*s1), (c1*c3 - c2*s1*s3), (s1*s2)],
[(-c3*s2), (s2*s3), (c2)]]),
'yzy': np.array([[(c1*c2*c3 - s1*s3), (-c1*s2), (c3*s1+c1*c2*s3)],
[(c3*s2), (c2), (s2*s3)],
[(-c1*s3 - c2*c3*s1), (s1*s2), (c1*c3-c2*s1*s3)]]),
'yxy': np.array([[(c1*c3 - c2*s1*s3), (s1*s2), (c1*s3+c2*c3*s1)],
[(s2*s3), (c2), (-c3*s2)],
[(-c3*s1 - c1*c2*s3), (c1*s2), (c1*c2*c3 - s1*s3)]]),
'xyx': np.array([[(c2), (s2*s3), (c3*s2)],
[(s1*s2), (c1*c3 - c2*s1*s3), (-c1*s3 - c2*c3*s1)],
[(-c1*s2), (c3*s1 + c1*c2*s3), (c1*c2*c3 - s1*s3)]]),
'xzx': np.array([[(c2), (-c3*s2), (s2*s3)],
[(c1*s2), (c1*c2*c3 - s1*s3), (-c3*s1 - c1*c2*s3)],
[(s1*s2), (c1*s3 + c2*c3*s1), (c1*c3 - c2*s1*s3)]])
}
model = models.EulerAngleRotation(23.4, 12.2, 34, axes_order)
mat = model._create_matrix(phi, theta, psi, axes_order)
assert_allclose(mat.T, matrices[axes_order]) # get_rotation_matrix(axes_order))