def testpm(self):
"""Proper motion => apply PM to position."""
import math
ra = tpm.d2r(269.45402305)
de = tpm.d2r(4.66828815)
px = 549.01 / 1000.0 # To Arc seconds
rv = 0.0
# pmra * cos(de) into pmra
pmra = (-797.84 / 1000.0 ) / math.cos(de)
pmra *= 100.0 # To Arcseconds per century.
pmde = (10326.93 / 1000.0)
pmde *= 100.0 # To Arcseconds per century.
C = tpm.CJ
v6 = tpm.cat2v6(ra, de, pmra, pmde, px, rv, C)
v6 = tpm.proper_motion(v6, tpm.J2000, tpm.jyear2jd(1991.25))
v6 = v6.c2s()
hms = tpm.HMS(r=v6.alpha)
dms = tpm.DMS(r=v6.delta)
hms.normalize()
dms.normalize()
self.assertAlmostEqual(hms.hh, -7.0)
self.assertAlmostEqual(hms.mm, 57.0)
self.assertAlmostEqual(hms.ss, 48.4986, 3)
self.assertAlmostEqual(dms.dd, 4.0)
self.assertAlmostEqual(dms.mm, 41.0)
self.assertAlmostEqual(dms.ss, 36.1980, 3)
def testv62cat(self):
"""v62cat => Cartesian to catalog; testing cat2v6 <-> v62cat."""
# See pytpm/tests/c_tests/cat2v6_v62cat_test.c.
# Barnard's star from Hipparcos catalog.
# ICRS Epoch J1991.25
import math
alpha = tpm.d2r(269.45402305)
delta = tpm.d2r(4.66828815)
px = 549.01 / 1000.0 # To Arc seconds
rv = 0.0
# pmra * cos(de) into pmra
pma = (-797.84 / 1000.0) / math.cos(delta)
pma *= 100.0 # To Arcseconds per century.
pmd = 10326.93 / 1000.0
pmd *= 100.0 # To Arcseconds per century.
C = tpm.CJ
v6 = tpm.cat2v6(alpha, delta, pma, pmd, px, rv, C)
p = tpm.v62cat(v6, C)
self.assertAlmostEqual(tpm.r2r(p["alpha"]), alpha)
self.assertAlmostEqual(p["delta"], delta)
self.assertAlmostEqual(p["pma"], pma)
self.assertAlmostEqual(p["pmd"], pmd)
self.assertAlmostEqual(p["px"], px)
self.assertAlmostEqual(p["rv"], rv)
def test_slalib_hip_galeq(self):
"""convertv6(x,s1=4,s=6) + PM <=> SLALIB galeq HIP"""
v6l = []
for r, d in zip(self.hip_tab['glon'], self.hip_tab['glat']):
v6 = tpm.V6S()
v6.r = 1e9
v6.alpha = tpm.d2r(r)
v6.delta = tpm.d2r(d)
v6l.append(v6.s2c())
# The epoch of galactic data is J2000. But in SLALIB
# the input is taken to be B1950.0. I can't apply proper_motion
# from J2000 to B1950 before input to SLALIB since, I don't
# have galactic velocities. In essence, the SLALIB input has a
# proper_motion for the period B1950 to J2000, which is also
# present in the output. By setting
# epoch=tpm.B1950 PyTPM will return FK5 values at eq. J2000
# but at epoch B1950, which should match the results from
# SLALIB. The velocities for this conversion show up during
# FK4-FK5 frame conversion.
v6o = convert.convertv6(v6l, s1=4, s2=6, epoch=tpm.B1950)
cat = (tpm.v62cat(v, tpm.CJ) for v in v6o)
tab = get_sla("slalib_hip_galeq.txt")
for v, s in zip(cat, tab):
ra = math.degrees(tpm.r2r(v['alpha']))
dec = math.degrees(v['delta'])
ra_diff = abs(ra - s[0]) * 3600.0
dec_diff = abs(dec - s[1]) * 3600.0
self.assertTrue(ra_diff <= 0.001 )
self.assertTrue(dec_diff <= 0.001 )
def test_slalib_hip_eqgal(self):
"""convertv6(x,s1=6,s=4) + PM <=> SLALIB eqgal HIP"""
v6l = []
for r, d in zip(self.hip_tab['raj2'], self.hip_tab['decj2']):
v6 = tpm.V6S()
v6.r = 1e9
v6.alpha = tpm.d2r(r)
v6.delta = tpm.d2r(d)
v6l.append(v6.s2c())
v6o = convert.convertv6(v6l, s1=6, s2=4)
# The galactic coordinates are at epoch J2000. But SLALIB
# results are for B1950. So apply proper motion here.
v6o = convert.proper_motion(v6o, tpm.B1950, tpm.J2000)
cat = (tpm.v62cat(v, tpm.CJ) for v in v6o)
tab = get_sla("slalib_hip_eqgal.txt")
for v, s in zip(cat, tab):
ra = math.degrees(tpm.r2r(v['alpha']))
dec = math.degrees(v['delta'])
ra_diff = abs(ra - s[0]) * 3600.0
dec_diff = abs(dec - s[1]) * 3600.0
self.assertTrue(ra_diff <= 0.001 )
self.assertTrue(dec_diff <= 0.001 )
def test_slalib_hip_galeq(self):
"""convertv6(x,s1=4,s=6) + PM <=> SLALIB galeq HIP"""
v6l = []
for r, d in zip(self.hip_tab['glon'], self.hip_tab['glat']):
v6 = tpm.V6S()
v6.r = 1e9
v6.alpha = tpm.d2r(r)
v6.delta = tpm.d2r(d)
v6l.append(v6.s2c())
# The epoch of galactic data is J2000. But in SLALIB
# the input is taken to be B1950.0. I can't apply proper_motion
# from J2000 to B1950 before input to SLALIB since, I don't
# have galactic velocities. In essence, the SLALIB input has a
# proper_motion for the period B1950 to J2000, which is also
# present in the output. By setting
# epoch=tpm.B1950 PyTPM will return FK5 values at eq. J2000
# but at epoch B1950, which should match the results from
# SLALIB. The velocities for this conversion show up during
# FK4-FK5 frame conversion.
v6o = convert.convertv6(v6l, s1=4, s2=6, epoch=tpm.B1950)
cat = (tpm.v62cat(v, tpm.CJ) for v in v6o)
tab = get_sla("slalib_hip_galeq.txt")
for v, s in zip(cat, tab):
ra = math.degrees(tpm.r2r(v['alpha']))
dec = math.degrees(v['delta'])
ra_diff = abs(ra - s[0]) * 3600.0
dec_diff = abs(dec - s[1]) * 3600.0
self.assertTrue(ra_diff <= 0.001)
self.assertTrue(dec_diff <= 0.001)
def testEqu2gal(self):
"""tpm.equ2gal => convert Galactic to FK4 equatorial."""
v6 = tpm.V6S(r=1e9,alpha=tpm.d2r(120.0), delta=tpm.d2r(90.0))
v6 = v6.s2c()
v6 = tpm.gal2equ(v6)
self.verify(v6.c2s(), tpm.V6S(r=1e9, alpha=tpm.d2r(192.25),
delta=tpm.d2r(27.4)))
def testProperMotion(self):
"""Convert.proper_motion: multiple V6C values."""
ra = tpm.d2r(269.45402305)
de = tpm.d2r(4.66828815)
px = 549.01 / 1000.0 # To Arc seconds
rv = 0.0
# pmra * cos(de) into pmra
pmra = (-797.84 / 1000.0) / math.cos(de)
pmra *= 100.0 # To Arcseconds per century.
pmde = (10326.93 / 1000.0)
pmde *= 100.0 # To Arcseconds per century.
C = tpm.CJ
v6 = tpm.cat2v6(ra, de, pmra, pmde, px, rv, C)
v6_out = convert.proper_motion([v6, v6], tpm.J2000,
tpm.jyear2jd(1991.25))
for i in v6_out:
v6 = i.c2s()
hms = tpm.HMS(r=v6.alpha)
dms = tpm.DMS(r=v6.delta)
hms.normalize()
dms.normalize()
self.assertAlmostEqual(hms.hh, -7.0)
self.assertAlmostEqual(hms.mm, 57.0)
self.assertAlmostEqual(hms.ss, 48.4986, 3)
self.assertAlmostEqual(dms.dd, 4.0)
self.assertAlmostEqual(dms.mm, 41.0)
self.assertAlmostEqual(dms.ss, 36.1980, 3)
def testcat2v6(self):
"""cat2v6 => catalog to Cartesian."""
# See pytpm/tests/c_tests/cat2v6_v62cat_test.c.
# Barnard's star from Hipparcos catalog.
# ICRS Epoch J1991.25
import math
alpha = tpm.d2r(269.45402305)
delta = tpm.d2r(4.66828815)
px = 549.01 / 1000.0 # To Arc seconds
rv = 0.0
# pmra * cos(de) into pmra
pma = (-797.84 / 1000.0) / math.cos(delta)
pma *= 100.0 # To Arcseconds per century.
pmd = 10326.93 / 1000.0
pmd *= 100.0 # To Arcseconds per century.
C = tpm.CJ
v6 = tpm.cat2v6(alpha, delta, pma, pmd, px, rv, C)
self.assertAlmostEqual(v6.x, -3568.1807935995)
self.assertAlmostEqual(v6.y, -374439.8219691383)
self.assertAlmostEqual(v6.z, 30577.3105202634)
self.assertAlmostEqual(v6.xdot, -0.0039386179)
self.assertAlmostEqual(v6.ydot, 0.0042290848)
self.assertAlmostEqual(v6.zdot, 0.0513283878)
def test_slalib_nwdfs_fk54z(self):
"""convertv6(x,s1=6,s=5) + PM <=> SLALIB FK5-FK4 (fk54z) NDWFS"""
v6l = []
for r, d in zip(self.ndwfs_tab['raj2'], self.ndwfs_tab['decj2']):
v6 = tpm.V6S()
v6.r = 1e9
v6.alpha = tpm.d2r(r)
v6.delta = tpm.d2r(d)
v6l.append(v6.s2c())
v6o = convert.convertv6(v6l, s1=6, s2=5)
v6o = convert.proper_motion(v6o, tpm.B1950, tpm.J2000)
cat = (tpm.v62cat(v, tpm.CB) for v in v6o)
tab = get_sla("slalib_ndwfs_fk54z.txt")
for v, s in zip(cat, tab):
ra = math.degrees(tpm.r2r(v['alpha']))
dec = math.degrees(v['delta'])
# arcsec/cent to milli-arcsec/year.
pma = v['pma'] * 1000.0 / 100.0
pmd = v['pmd'] * 1000.0 / 100.0
ra_diff = abs(ra - s[0]) * 3600.0
dec_diff = abs(dec - s[1]) * 3600.0
pma_diff = abs(pma - s[2])
pmd_diff = abs(pmd - s[3])
self.assertTrue(ra_diff <= 0.0001)
self.assertTrue(dec_diff <= 0.0001)
self.assertTrue(pma_diff <= 1)
self.assertTrue(pmd_diff <= 1)
def testcat2v6(self):
"""cat2v6 => catalog to Cartesian."""
# See pytpm/tests/c_tests/cat2v6_v62cat_test.c.
# Barnard's star from Hipparcos catalog.
# ICRS Epoch J1991.25
import math
alpha = tpm.d2r(269.45402305)
delta = tpm.d2r(4.66828815)
px = 549.01 / 1000.0 # To Arc seconds
rv = 0.0
# pmra * cos(de) into pmra
pma = (-797.84 / 1000.0 ) / math.cos(delta)
pma *= 100.0 # To Arcseconds per century.
pmd = (10326.93 / 1000.0)
pmd *= 100.0 # To Arcseconds per century.
C = tpm.CJ
v6 = tpm.cat2v6(alpha, delta, pma, pmd, px, rv, C)
self.assertAlmostEqual(v6.x, -3568.1807935995)
self.assertAlmostEqual(v6.y, -374439.8219691383)
self.assertAlmostEqual(v6.z, 30577.3105202634)
self.assertAlmostEqual(v6.xdot, -0.0039386179)
self.assertAlmostEqual(v6.ydot, 0.0042290848)
self.assertAlmostEqual(v6.zdot, 0.0513283878)
def testProperMotion(self):
"""Convert.proper_motion: multiple V6C values."""
ra = tpm.d2r(269.45402305)
de = tpm.d2r(4.66828815)
px = 549.01 / 1000.0 # To Arc seconds
rv = 0.0
# pmra * cos(de) into pmra
pmra = (-797.84 / 1000.0) / math.cos(de)
pmra *= 100.0 # To Arcseconds per century.
pmde = 10326.93 / 1000.0
pmde *= 100.0 # To Arcseconds per century.
C = tpm.CJ
v6 = tpm.cat2v6(ra, de, pmra, pmde, px, rv, C)
v6_out = convert.proper_motion([v6, v6], tpm.J2000, tpm.jyear2jd(1991.25))
for i in v6_out:
v6 = i.c2s()
hms = tpm.HMS(r=v6.alpha)
dms = tpm.DMS(r=v6.delta)
hms.normalize()
dms.normalize()
self.assertAlmostEqual(hms.hh, -7.0)
self.assertAlmostEqual(hms.mm, 57.0)
self.assertAlmostEqual(hms.ss, 48.4986, 3)
self.assertAlmostEqual(dms.dd, 4.0)
self.assertAlmostEqual(dms.mm, 41.0)
self.assertAlmostEqual(dms.ss, 36.1980, 3)
def testEqu2gal(self):
"""tpm.equ2gal => convert FK4 equatorial to Galactic."""
v6 = tpm.V6S(r=1e9, alpha=tpm.d2r(192.25), delta=tpm.d2r(27.4))
v6 = v6.s2c()
v6 = tpm.equ2gal(v6)
v6 = v6.c2s()
self.verify(v6, tpm.V6S(r=1e9, alpha=tpm.d2r(120.866), delta=tpm.d2r(90.0)))
def testpm(self):
"""Proper motion => apply PM to position."""
import math
ra = tpm.d2r(269.45402305)
de = tpm.d2r(4.66828815)
px = 549.01 / 1000.0 # To Arc seconds
rv = 0.0
# pmra * cos(de) into pmra
pmra = (-797.84 / 1000.0) / math.cos(de)
pmra *= 100.0 # To Arcseconds per century.
pmde = 10326.93 / 1000.0
pmde *= 100.0 # To Arcseconds per century.
C = tpm.CJ
v6 = tpm.cat2v6(ra, de, pmra, pmde, px, rv, C)
v6 = tpm.proper_motion(v6, tpm.J2000, tpm.jyear2jd(1991.25))
v6 = v6.c2s()
hms = tpm.HMS(r=v6.alpha)
dms = tpm.DMS(r=v6.delta)
hms.normalize()
dms.normalize()
self.assertAlmostEqual(hms.hh, -7.0)
self.assertAlmostEqual(hms.mm, 57.0)
self.assertAlmostEqual(hms.ss, 48.4986, 3)
self.assertAlmostEqual(dms.dd, 4.0)
self.assertAlmostEqual(dms.mm, 41.0)
self.assertAlmostEqual(dms.ss, 36.1980, 3)
def test_slalib_nwdfs_fk54z(self):
"""convertv6(x,s1=6,s=5) + PM <=> SLALIB FK5-FK4 (fk54z) NDWFS"""
v6l = []
for r, d in zip(self.ndwfs_tab['raj2'], self.ndwfs_tab['decj2']):
v6 = tpm.V6S()
v6.r = 1e9
v6.alpha = tpm.d2r(r)
v6.delta = tpm.d2r(d)
v6l.append(v6.s2c())
v6o = convert.convertv6(v6l, s1=6, s2=5)
v6o = convert.proper_motion(v6o, tpm.B1950, tpm.J2000)
cat = (tpm.v62cat(v, tpm.CB) for v in v6o)
tab = get_sla("slalib_ndwfs_fk54z.txt")
for v, s in zip(cat, tab):
ra = math.degrees(tpm.r2r(v['alpha']))
dec = math.degrees(v['delta'])
# arcsec/cent to milli-arcsec/year.
pma = v['pma'] * 1000.0 / 100.0
pmd = v['pmd'] * 1000.0 / 100.0
ra_diff = abs(ra - s[0]) * 3600.0
dec_diff = abs(dec - s[1]) * 3600.0
pma_diff = abs(pma - s[2])
pmd_diff = abs(pmd - s[3])
self.assertTrue(ra_diff <= 0.0001 )
self.assertTrue(dec_diff <= 0.0001)
self.assertTrue(pma_diff <= 1)
self.assertTrue(pmd_diff <= 1)
def testv62cat(self):
"""v62cat => Cartesian to catalog; testing cat2v6 <-> v62cat."""
# See pytpm/tests/c_tests/cat2v6_v62cat_test.c.
# Barnard's star from Hipparcos catalog.
# ICRS Epoch J1991.25
import math
alpha = tpm.d2r(269.45402305)
delta = tpm.d2r(4.66828815)
px = 549.01 / 1000.0 # To Arc seconds
rv = 0.0
# pmra * cos(de) into pmra
pma = (-797.84 / 1000.0 ) / math.cos(delta)
pma *= 100.0 # To Arcseconds per century.
pmd = (10326.93 / 1000.0)
pmd *= 100.0 # To Arcseconds per century.
C = tpm.CJ
v6 = tpm.cat2v6(alpha, delta, pma, pmd, px, rv, C)
p = tpm.v62cat(v6, C)
self.assertAlmostEqual(tpm.r2r(p['alpha']), alpha)
self.assertAlmostEqual(p['delta'], delta)
self.assertAlmostEqual(p['pma'], pma)
self.assertAlmostEqual(p['pmd'], pmd)
self.assertAlmostEqual(p['px'], px)
self.assertAlmostEqual(p['rv'], rv)
def test_slalib_hip_eqgal(self):
"""convertv6(x,s1=6,s=4) + PM <=> SLALIB eqgal HIP"""
v6l = []
for r, d in zip(self.hip_tab['raj2'], self.hip_tab['decj2']):
v6 = tpm.V6S()
v6.r = 1e9
v6.alpha = tpm.d2r(r)
v6.delta = tpm.d2r(d)
v6l.append(v6.s2c())
v6o = convert.convertv6(v6l, s1=6, s2=4)
# The galactic coordinates are at epoch J2000. But SLALIB
# results are for B1950. So apply proper motion here.
v6o = convert.proper_motion(v6o, tpm.B1950, tpm.J2000)
cat = (tpm.v62cat(v, tpm.CJ) for v in v6o)
tab = get_sla("slalib_hip_eqgal.txt")
for v, s in zip(cat, tab):
ra = math.degrees(tpm.r2r(v['alpha']))
dec = math.degrees(v['delta'])
ra_diff = abs(ra - s[0]) * 3600.0
dec_diff = abs(dec - s[1]) * 3600.0
self.assertTrue(ra_diff <= 0.001)
self.assertTrue(dec_diff <= 0.001)
def testD2R(self):
"""tpm.d2r() => convert degrees into radians."""
import math
self.assertAlmostEqual(tpm.d2r(180.0), math.pi)
self.assertAlmostEqual(tpm.d2r(360.0), 2*math.pi)
self.assertAlmostEqual(tpm.d2r(-360.0), -2*math.pi)
self.assertAlmostEqual(tpm.d2r(720.0), 4*math.pi)
self.assertAlmostEqual(tpm.d2r(-720.0), -4*math.pi)
def testEqu2gal(self):
"""tpm.equ2gal => convert FK4 equatorial to Galactic."""
v6 = tpm.V6S(r=1e9,alpha=tpm.d2r(192.25), delta=tpm.d2r(27.4))
v6 = v6.s2c()
v6 = tpm.equ2gal(v6)
v6 = v6.c2s()
self.verify(v6, tpm.V6S(r=1e9, alpha=tpm.d2r(120.866),
delta=tpm.d2r(90.0)))
def testNdelta(self):
delta = [-100, 100, 181, 270]
delta_out = [-80.0, 80.0, -1.0, -90.0]
for i,d in enumerate(delta):
j = tpm.ndelta(d, degrees=True)
self.assertAlmostEqual(j, delta_out[i], 1)
k = tpm.ndelta(tpm.d2r(d), degrees=False)
self.assertAlmostEqual(k, tpm.d2r(delta_out[i]), 1)
def testFk425(self):
"""tpm.fk425 => B1950 FK4 to J2000 FK5."""
v6 = tpm.V6S(r=1e9, alpha=tpm.d2r(23.15678), delta=tpm.d2r(54.3892))
v6 = v6.s2c()
v6 = tpm.fk425(v6)
v6 = v6.c2s()
# Why does R change?
self.verify(v6, tpm.V6S(r=1000000000.0008671284, alpha=tpm.d2r(23.9534903408), delta=tpm.d2r(54.6442824316)))
def testNdelta(self):
delta = [-100, 100, 181, 270]
delta_out = [-80.0, 80.0, -1.0, -90.0]
for i, d in enumerate(delta):
j = tpm.ndelta(d, degrees=True)
self.assertAlmostEqual(j, delta_out[i], 1)
k = tpm.ndelta(tpm.d2r(d), degrees=False)
self.assertAlmostEqual(k, tpm.d2r(delta_out[i]), 1)
def testFk524(self):
"""tpm.fk524 => J2000 FK5 to B1950 FK4."""
v6 = tpm.V6S(r=1e9, alpha=tpm.d2r(23.9534903408), delta=tpm.d2r(54.6442824316))
v6 = v6.s2c()
v6 = tpm.fk524(v6)
v6 = v6.c2s()
# Why does R change?
self.verify(v6, tpm.V6S(r=1e9, alpha=tpm.d2r(23.15678), delta=tpm.d2r(54.3892)))
def testD2R(self):
"""tpm.d2r() => convert degrees into radians."""
import math
self.assertAlmostEqual(tpm.d2r(180.0), math.pi)
self.assertAlmostEqual(tpm.d2r(360.0), 2 * math.pi)
self.assertAlmostEqual(tpm.d2r(-360.0), -2 * math.pi)
self.assertAlmostEqual(tpm.d2r(720.0), 4 * math.pi)
self.assertAlmostEqual(tpm.d2r(-720.0), -4 * math.pi)
def testNalpha(self):
"""tpm.nalpha => angle in [0, 360) or [0, 2π)."""
alpha = [361, -361, -180]
alpha_out = [1, 359, 180]
for i, d in enumerate(alpha):
j = tpm.nalpha(d, degrees=True)
self.assertAlmostEqual(j, alpha_out[i], 1)
k = tpm.nalpha(tpm.d2r(d), degrees=False)
self.assertAlmostEqual(k, tpm.d2r(alpha_out[i]), 1)
def testNalpha(self):
"""tpm.nalpha => angle in [0, 360) or [0, 2π)."""
alpha = [361, -361, -180]
alpha_out = [1, 359, 180]
for i,d in enumerate(alpha):
j = tpm.nalpha(d, degrees=True)
self.assertAlmostEqual(j, alpha_out[i], 1)
k = tpm.nalpha(tpm.d2r(d), degrees=False)
self.assertAlmostEqual(k, tpm.d2r(alpha_out[i]), 1)
def testLdelfect(self):
"""tpm.ldeflect => apply GR light deflection."""
v6h = tpm.evp(tpm.J2000)[1]
v6 = tpm.V6S(r=1, alpha=tpm.d2r(34.56), delta=tpm.d2r(46.19))
v6 = v6.s2c()
v6 = tpm.ldeflect(v6, v6h, 1)
self.verify(v6.c2s(), tpm.V6S(r=1.0, alpha=0.6031857970, delta=0.8061675815))
def testazel2hadec(self):
"""tpm.azel2hadec => (AZ,EL) to (HA,DEC)"""
v6 = tpm.V6S(r=1e9)
for i,j,k,l in zip(self.az,self.el,self.ha_c,self.dec_c):
v6.alpha = tpm.d2r(i)
v6.delta = tpm.d2r(j)
v61 = tpm.azel2hadec(v6.s2c(), tpm.d2r(self.lat))
v6 = v61.c2s()
self.assertAlmostEqual(tpm.r2d(tpm.r2r(v6.alpha)), k, 8)
self.assertAlmostEqual(tpm.r2d(tpm.r2r(v6.delta)), l, 8)
def testazel2hadec(self):
"""tpm.azel2hadec => (AZ,EL) to (HA,DEC)"""
v6 = tpm.V6S(r=1e9)
for i, j, k, l in zip(self.az, self.el, self.ha_c, self.dec_c):
v6.alpha = tpm.d2r(i)
v6.delta = tpm.d2r(j)
v61 = tpm.azel2hadec(v6.s2c(), tpm.d2r(self.lat))
v6 = v61.c2s()
self.assertAlmostEqual(tpm.r2d(tpm.r2r(v6.alpha)), k, 8)
self.assertAlmostEqual(tpm.r2d(tpm.r2r(v6.delta)), l, 8)
def testPrecess(self):
"""convert.precess => precess in inertial frame."""
alpha = [34.1592] * 2
delta = [12.9638] * 2
a, d = convert.precess(alpha, delta, tpm.J2000, tpm.J1984, tpm.PRECESS_FK5)
for i, j in zip(a, d):
self.assertAlmostEqual(tpm.d2r(i), 0.5924126644, 5)
self.assertAlmostEqual(tpm.d2r(j), 0.2249726697, 5)
def testLdelfect(self):
"""tpm.ldeflect => apply GR light deflection."""
v6h = tpm.evp(tpm.J2000)[1]
v6 = tpm.V6S(r=1, alpha=tpm.d2r(34.56), delta=tpm.d2r(46.19))
v6 = v6.s2c()
v6 = tpm.ldeflect(v6, v6h, 1)
self.verify(v6.c2s(), tpm.V6S(r=1.0, alpha=0.6031857970,
delta=0.8061675815))
def testPrecess(self):
"""convert.precess => precess in inertial frame."""
alpha = [34.1592] * 2
delta = [12.9638] * 2
a, d = convert.precess(alpha, delta, tpm.J2000, tpm.J1984,
tpm.PRECESS_FK5)
for i, j in zip(a, d):
self.assertAlmostEqual(tpm.d2r(i), 0.5924126644, 5)
self.assertAlmostEqual(tpm.d2r(j), 0.2249726697, 5)
def testHadec2azel(self):
"""tpm.hadec2azel => (HA,DEC) to (AZ,EL)"""
v6 = tpm.V6S(r=1e9)
for i, j, k, l in zip(self.az, self.el, self.ha_c, self.dec_c):
j = tpm.r2d(tpm.r2r(tpm.d2r(j)))
v6.alpha = tpm.d2r(k)
v6.delta = tpm.d2r(l)
v61 = tpm.hadec2azel(v6.s2c(), tpm.d2r(self.lat))
v6 = v61.c2s()
self.assertAlmostEqual(tpm.r2d(tpm.r2r(v6.alpha)), i, 8)
self.assertAlmostEqual(tpm.r2d(tpm.r2r(v6.delta)), j, 8)
def testFk425(self):
"""tpm.fk425 => B1950 FK4 to J2000 FK5."""
v6 = tpm.V6S(r=1e9, alpha=tpm.d2r(23.15678), delta=
tpm.d2r(54.3892))
v6 = v6.s2c()
v6 = tpm.fk425(v6)
v6 = v6.c2s()
# Why does R change?
self.verify(v6, tpm.V6S(r=1000000000.0008671284,
alpha=tpm.d2r(23.9534903408),
delta=tpm.d2r(54.6442824316)))
def testFk524(self):
"""tpm.fk524 => J2000 FK5 to B1950 FK4."""
v6 = tpm.V6S(r=1e9,
alpha=tpm.d2r(23.9534903408),
delta=tpm.d2r(54.6442824316))
v6 = v6.s2c()
v6 = tpm.fk524(v6)
v6 = v6.c2s()
# Why does R change?
self.verify(v6, tpm.V6S(r=1e9, alpha=tpm.d2r(23.15678), delta=
tpm.d2r(54.3892)))
def get_tstate():
tstate = tpm.TSTATE()
tpm.tpm_data(tstate, tpm.TPM_INIT)
tstate.utc = tpm.J2000
tstate.lon = tpm.d2r(-111.598333)
tstate.lat = tpm.d2r(31.956389)
tstate.alt = 2093.093
tstate.delta_at = tpm.delta_AT(tstate.utc)
tstate.delta_ut = tpm.delta_UT(tstate.utc)
tpm.tpm_data(tstate, tpm.TPM_ALL)
return tstate
def testHadec2azel(self):
"""tpm.hadec2azel => (HA,DEC) to (AZ,EL)"""
v6 = tpm.V6S(r=1e9)
for i,j,k,l in zip(self.az,self.el,self.ha_c,self.dec_c):
j = tpm.r2d(tpm.r2r(tpm.d2r(j)))
v6.alpha = tpm.d2r(k)
v6.delta = tpm.d2r(l)
v61 = tpm.hadec2azel(v6.s2c(), tpm.d2r(self.lat))
v6 = v61.c2s()
self.assertAlmostEqual(tpm.r2d(tpm.r2r(v6.alpha)),
i, 8)
self.assertAlmostEqual(tpm.r2d(tpm.r2r(v6.delta)), j, 8)
def testPrecess(self):
"""tpm.precess => precess V6 in inertial frame."""
v6 = tpm.V6S(r=1e9, alpha=tpm.d2r(34.1592),
delta=tpm.d2r(12.9638), rdot=-0.123,
alphadot=0.382, deltadot=1.0)
v6 = v6.s2c()
v6 = tpm.precess(tpm.J2000, tpm.J1984, v6, tpm.PRECESS_FK5)
v6 = v6.c2s()
self.verify(v6,tpm.V6S(r=1e9, alpha=0.5924126644,
delta=0.2249726697,rdot=-0.1229999560,
alphadot=0.3809705204,
deltadot=1.0003321415))
def testGeod2geoc(self):
"""tpm.geod2geoc => Geodetic to geocentric."""
v6 = tpm.geod2geoc(tpm.d2r(30.567), tpm.d2r(46.713), 1500.0)
self.verify(
v6,
tpm.V6C(
x=3773051.892626300,
y=2228444.491846553,
z=4621039.023174386,
xdot=-162.500738326,
ydot=275.135288555,
zdot=0.0,
),
)
def testToObsAzElDateJ2000ep2000(self):
"""P and V: J2000 (~ICRS) 1991.25 => ObsAzEl Date J2000 ep J2000."""
# Set s2=TPM_S13 and ep2=J2000 in
# c_tests/test_conversion_with_pm.c.
ra = []
dec = []
pmra = []
pmdec = []
px = []
f = open(hip_data, "r")
for i in f:
x = [float(j) for j in i.split()]
ra.append(tpm.d2r(x[0]))
dec.append(tpm.d2r(x[1]))
# Milli-arcsec/year to arcsec/century.
pmra.append( ((x[2]/1000.0) / math.cos(tpm.d2r(x[1]))) * 100.0 )
pmdec.append( (x[3]/1000.0) * 100.0)
px.append(x[4])
f.close()
s1 = tpm.TPM_S06
ep = tpm.y2j(1991.25)
eq = tpm.J2000
s2 = tpm.TPM_S13
ep2 = tpm.J2000
f = open(os.path.join(c_tests_dir,
"hipicrsep1991_ObsAzElDateJ2000ep2000.txt"),
"r")
pvec = tpm.PVEC()
tstate = get_tstate()
for i in xrange(len(ra)):
v6 = tpm.cat2v6(ra[i], dec[i], pmra[i], pmdec[i], px[i], 0.0,
tpm.CJ)
pvec[s1] = v6
tpm.tpm(pvec, s1, s2, ep, eq, tstate)
v6 = pvec[s2]
tpm.proper_motion(v6, ep2, ep)
d = tpm.v62cat(v6, tpm.CJ)
x = [float(j) for j in f.readline().strip().split()]
self.assertAlmostEqual(tpm.r2d(tpm.r2r(d['alpha'])), x[0], 8)
self.assertAlmostEqual(tpm.r2d(d['delta']), x[1], 8)
self.assertAlmostEqual(d['pma'], x[2], 4)
self.assertAlmostEqual(d['pmd'], x[3], 4)
self.assertAlmostEqual(d['px'], x[4], 8)
self.assertAlmostEqual(d['rv'], x[5], 2)
f.close()
def testConvertv6(self):
"""ConvertV6: J2000 (~ICRS) 1991.25 => FK4 B1950 ep 1950.0."""
# Set s2=TPM_S05 and ep2=B1950 in
# c_tests/test_conversion_with_pm.c.
ra = []
dec = []
pmra = []
pmdec = []
px = []
f = open(hip_data_icrs, "r")
for i in f:
x = [float(j) for j in i.split()]
ra.append(tpm.d2r(x[0]))
dec.append(tpm.d2r(x[1]))
# Milli-arcsec/year to arcsec/century.
pmra.append(((x[2] / 1000.0) / math.cos(tpm.d2r(x[1]))) * 100.0)
pmdec.append((x[3] / 1000.0) * 100.0)
px.append(x[4])
f.close()
s1 = tpm.TPM_S06
ep = tpm.y2j(1991.25)
eq = tpm.J2000
s2 = tpm.TPM_S05
ep2 = tpm.B1950
f = open(os.path.join(c_tests_dir, "hipicrsep1991_fk4B1950ep1950.txt"),
"r")
v6_l = []
for i in range(len(ra)):
v6 = tpm.cat2v6(ra[i], dec[i], pmra[i], pmdec[i], px[i], 0.0,
tpm.CJ)
v6_l.append(v6)
v6_out = convert.convertv6(v6_l, epoch=ep, equinox=eq, s1=s1, s2=s2)
for v in v6_out:
tpm.proper_motion(v, ep2, ep)
d = tpm.v62cat(v, tpm.CJ)
x = [float(j) for j in f.readline().strip().split()]
self.assertAlmostEqual(tpm.r2d(tpm.r2r(d['alpha'])), x[0], 8)
self.assertAlmostEqual(tpm.r2d(d['delta']), x[1], 8)
self.assertAlmostEqual(d['pma'], x[2], 4)
self.assertAlmostEqual(d['pmd'], x[3], 4)
self.assertAlmostEqual(d['px'], x[4], 8)
self.assertAlmostEqual(d['rv'], x[5], 2)
f.close()
def testEcl2equ(self):
"""tpm.equ2ecl => FK5 Equatorial to Ecliptic."""
v6 = tpm.V6C(x=0.5, y=0.173611298, z=0.848445117, xdot=-0.034000000, ydot=0.251873488, zdot=-0.872330067)
v6 = tpm.equ2ecl(v6, tpm.d2r(23.7))
self.verify(v6, tpm.V6C(x=0.5, y=0.499999997, z=0.707106774, xdot=-0.0340, ydot=-0.120, zdot=-0.9))
def testConvertv6(self):
"""ConvertV6: J2000 (~ICRS) 1991.25 => FK4 B1950 ep 1950.0."""
# Set s2=TPM_S05 and ep2=B1950 in
# c_tests/test_conversion_with_pm.c.
ra = []
dec = []
pmra = []
pmdec = []
px = []
f = open(hip_data_icrs, "r")
for i in f:
x = [float(j) for j in i.split()]
ra.append(tpm.d2r(x[0]))
dec.append(tpm.d2r(x[1]))
# Milli-arcsec/year to arcsec/century.
pmra.append(((x[2] / 1000.0) / math.cos(tpm.d2r(x[1]))) * 100.0)
pmdec.append((x[3] / 1000.0) * 100.0)
px.append(x[4])
f.close()
s1 = tpm.TPM_S06
ep = tpm.y2j(1991.25)
eq = tpm.J2000
s2 = tpm.TPM_S05
ep2 = tpm.B1950
f = open(os.path.join(c_tests_dir, "hipicrsep1991_fk4B1950ep1950.txt"), "r")
v6_l = []
for i in range(len(ra)):
v6 = tpm.cat2v6(ra[i], dec[i], pmra[i], pmdec[i], px[i], 0.0, tpm.CJ)
v6_l.append(v6)
v6_out = convert.convertv6(v6_l, epoch=ep, equinox=eq, s1=s1, s2=s2)
for v in v6_out:
tpm.proper_motion(v, ep2, ep)
d = tpm.v62cat(v, tpm.CJ)
x = [float(j) for j in f.readline().strip().split()]
self.assertAlmostEqual(tpm.r2d(tpm.r2r(d["alpha"])), x[0], 8)
self.assertAlmostEqual(tpm.r2d(d["delta"]), x[1], 8)
self.assertAlmostEqual(d["pma"], x[2], 4)
self.assertAlmostEqual(d["pmd"], x[3], 4)
self.assertAlmostEqual(d["px"], x[4], 8)
self.assertAlmostEqual(d["rv"], x[5], 2)
f.close()
def test_slalib_hip_fk524(self):
"""convertv6(x,s1=6,s2=5) + PM <=> SLALIB FK5-FK4 (fk524) HIP"""
v6l = []
for r, d, pa, pd, px in zip(self.hip_tab['raj2'],
self.hip_tab['decj2'],
self.hip_tab['pma'],
self.hip_tab['pmd'],
self.hip_tab['px']):
r = tpm.d2r(r)
d = tpm.d2r(d)
# Milli-arcsec / Jul. yr to milli-arcsec per Jul. century.
pma = pa / math.cos(d) / 1000.0 * 100.0
pmd = pd / 1000.0 * 100.0
px /= 1000.0 # mili-arcsec to arc-sec.
v6 = tpm.cat2v6(r, d, pma, pmd, px, 0.0, tpm.CJ)
v6l.append(v6)
v6o = convert.convertv6(v6l, s1=6, s2=5)
v6o = convert.proper_motion(v6o, tpm.B1950, tpm.J2000)
cat = (tpm.v62cat(v, tpm.CB) for v in v6o)
tab = get_sla("slalib_hip_fk524.txt")
for v, s in zip(cat, tab):
ra = math.degrees(tpm.r2r(v['alpha']))
dec = math.degrees(v['delta'])
# arc-sec/cent. to milli-arcsec/trop. year.
pma = v['pma'] * 1000.0 / 100.0
pmd = v['pmd'] * 1000.0 / 100.0
px = v['px'] * 1e3 # arc-sec to milli-arcsec
ra_diff = abs(ra - s[0]) * 3600.0
dec_diff = abs(dec - s[1]) * 3600.0
px_diff = abs(px - s[2])
pma_diff = abs(pma - s[3])
pmd_diff = abs(pmd - s[4])
rv_diff = abs(v['rv'] - s[5])
self.assertTrue(ra_diff <= 0.001)
self.assertTrue(dec_diff <= 0.001)
self.assertTrue(pma_diff <= 0.001)
self.assertTrue(pmd_diff <= 0.001)
self.assertTrue(px_diff <= 9)
self.assertTrue(rv_diff <= 0.04)
def testEcl2equ(self):
"""tpm.equ2ecl => FK5 Equatorial to Ecliptic."""
v6 = tpm.V6C(x=0.5, y=0.173611298, z=0.848445117,
xdot=-0.034000000, ydot=0.251873488,
zdot=-0.872330067)
v6 = tpm.equ2ecl(v6, tpm.d2r(23.7))
self.verify(v6, tpm.V6C(x=0.5, y=0.499999997, z=0.707106774,
xdot=-0.0340, ydot=-0.120, zdot=-0.9))
def testEllab(self):
"""tpm.ellab => apply elliptic aberration."""
# pytpm/tests/c_tests/ellab_test.c
v6 = tpm.V6S(r=1e9, alpha=tpm.h2r(20), delta=tpm.d2r(40.0))
v6 = v6.s2c()
v6 = tpm.ellab(tpm.J2000, v6, -1)
v6 = v6.c2s()
self.assertAlmostEqual(v6.r, 1e9, 5)
self.assertAlmostEqual(tpm.r2h(tpm.r2r(v6.alpha)), 20.000007838, 8)
self.assertAlmostEqual(tpm.r2d(tpm.r2r(v6.delta)), 39.999987574, 8)
def testPrecess(self):
"""tpm.precess => precess V6 in inertial frame."""
v6 = tpm.V6S(r=1e9, alpha=tpm.d2r(34.1592), delta=tpm.d2r(12.9638), rdot=-0.123, alphadot=0.382, deltadot=1.0)
v6 = v6.s2c()
v6 = tpm.precess(tpm.J2000, tpm.J1984, v6, tpm.PRECESS_FK5)
v6 = v6.c2s()
self.verify(
v6,
tpm.V6S(
r=1e9,
alpha=0.5924126644,
delta=0.2249726697,
rdot=-0.1229999560,
alphadot=0.3809705204,
deltadot=1.0003321415,
),
)
def testEllab(self):
"""tpm.ellab => apply elliptic aberration."""
# pytpm/tests/c_tests/ellab_test.c
v6 = tpm.V6S(r=1e9, alpha=tpm.h2r(20), delta=tpm.d2r(40.0))
v6 = v6.s2c()
v6 = tpm.ellab(tpm.J2000, v6, -1)
v6 = v6.c2s()
self.assertAlmostEqual(v6.r, 1e9,5)
self.assertAlmostEqual(tpm.r2h(tpm.r2r(v6.alpha)), 20.000007838,8)
self.assertAlmostEqual(tpm.r2d(tpm.r2r(v6.delta)), 39.999987574,8)
def test_slalib_hip_fk524(self):
"""convertv6(x,s1=6,s2=5) + PM <=> SLALIB FK5-FK4 (fk524) HIP"""
v6l = []
for r, d, pa, pd, px in zip(self.hip_tab['raj2'],
self.hip_tab['decj2'], self.hip_tab['pma'],
self.hip_tab['pmd'], self.hip_tab['px']):
r = tpm.d2r(r)
d = tpm.d2r(d)
# Milli-arcsec / Jul. yr to milli-arcsec per Jul. century.
pma = pa / math.cos(d) / 1000.0 * 100.0
pmd = pd / 1000.0 * 100.0
px /= 1000.0 # mili-arcsec to arc-sec.
v6 = tpm.cat2v6(r, d, pma, pmd, px, 0.0, tpm.CJ)
v6l.append(v6)
v6o = convert.convertv6(v6l, s1=6, s2=5)
v6o = convert.proper_motion(v6o, tpm.B1950, tpm.J2000)
cat = (tpm.v62cat(v, tpm.CB) for v in v6o)
tab = get_sla("slalib_hip_fk524.txt")
for v, s in zip(cat, tab):
ra = math.degrees(tpm.r2r(v['alpha']))
dec = math.degrees(v['delta'])
# arc-sec/cent. to milli-arcsec/trop. year.
pma = v['pma'] * 1000.0 / 100.0
pmd = v['pmd'] * 1000.0 / 100.0
px = v['px'] * 1e3 # arc-sec to milli-arcsec
ra_diff = abs(ra - s[0]) * 3600.0
dec_diff = abs(dec - s[1]) * 3600.0
px_diff = abs(px - s[2])
pma_diff = abs(pma - s[3])
pmd_diff = abs(pmd - s[4])
rv_diff = abs(v['rv'] - s[5])
self.assertTrue(ra_diff <= 0.001)
self.assertTrue(dec_diff <= 0.001)
self.assertTrue(pma_diff <= 0.001)
self.assertTrue(pmd_diff <= 0.001)
self.assertTrue(px_diff <= 9)
self.assertTrue(rv_diff <= 0.04)
def test_slalib_hip_fk425(self):
"""convertv6(v6,s1=5,s2=6) + PM <=> SLALIB FK4-FK5 (fk425) HIP."""
sla_tabb = get_sla("slalib_hip_fk524.txt")
tab = get_sla("slalib_hip_fk524_fk425.txt")
v6l = []
for r, d, px, pa, pd, rv in sla_tabb:
r = tpm.d2r(r)
d = tpm.d2r(d)
# Milli-arcsec / Trop. yr to arcsec per Trop. century.
pma = pa / 1000.0 * 100.0
pmd = pd / 1000.0 * 100.0
px /= 1000.0 # mili-arcsec to arc-sec.
v6 = tpm.cat2v6(r, d, pma, pmd, px, rv, tpm.CB)
v6l.append(v6)
v6o = convert.convertv6(v6l, s1=5, s2=6, epoch=tpm.B1950)
v6o = convert.proper_motion(v6o, tpm.J2000, tpm.B1950)
cat = (tpm.v62cat(v, tpm.CJ) for v in v6o)
for v, s in zip(cat, tab):
ra = math.degrees(tpm.r2r(v['alpha']))
dec = math.degrees(v['delta'])
# arc-sec/cent. to milli-arcsec/Jul. year.
pma = v['pma'] * 1000.0 / 100.0
pmd = v['pmd'] * 1000.0 / 100.0
px = v['px'] * 1e3 # arc-sec to milli-arcsec
ra_diff = abs(ra - s[0]) * 3600.0
dec_diff = abs(dec - s[1]) * 3600.0
px_diff = abs(px - s[2])
pma_diff = abs(pma - s[3])
pmd_diff = abs(pmd - s[4])
rv_diff = abs(v['rv'] - s[5])
self.assertTrue(ra_diff <= 0.001)
self.assertTrue(dec_diff <= 0.001)
self.assertTrue(pma_diff <= 0.001)
self.assertTrue(pmd_diff <= 0.001)
self.assertTrue(px_diff <= 9)
self.assertTrue(rv_diff <= 0.04)
def test_slalib_hip_fk52appradec(self):
"""convert(x, s1=6, s2=11) + PM => SLALIB sla_map HIP."""
tab = get_sla("slalib_hip_map.txt")
v6l = []
for r, d, pa, pd, px in zip(self.hip_tab['raj2'],
self.hip_tab['decj2'], self.hip_tab['pma'],
self.hip_tab['pmd'], self.hip_tab['px']):
r = tpm.d2r(r)
d = tpm.d2r(d)
# Milli-arcsec / Jul. yr to arcsec per Jul. century.
pma = pa / math.cos(d) / 1000.0 * 100.0
pmd = pd / 1000.0 * 100.0
px /= 1000.0 # mili-arcsec to arc-sec.
v6 = tpm.cat2v6(r, d, pma, pmd, px, 0.0, tpm.CJ)
v6l.append(v6)
utc = tpm.gcal2j(2010, 1, 1) - 0.5 # midnight
tt = tpm.utc2tdb(utc)
v6o = convert.proper_motion(v6l, tt, tpm.J2000)
v6o = convert.convertv6(v6o,
s1=6,
s2=11,
epoch=tt,
equinox=tpm.J2000,
utc=utc,
delta_at=tpm.delta_AT(utc))
cat = (tpm.v62cat(v, tpm.CJ) for v in v6o)
l = len(v6o)
for v, s, i in zip(cat, tab, range(l)):
ra = math.degrees(tpm.r2r(v['alpha']))
dec = math.degrees(v['delta'])
ra_diff = abs(ra - s[0]) * 3600.0
dec_diff = abs(dec - s[1]) * 3600.0
self.assertTrue(ra_diff <= 0.33)
self.assertTrue(dec_diff <= 0.03)
def test_slalib_hip_fk425(self):
"""convertv6(v6,s1=5,s2=6) + PM <=> SLALIB FK4-FK5 (fk425) HIP."""
sla_tabb = get_sla("slalib_hip_fk524.txt")
tab = get_sla("slalib_hip_fk524_fk425.txt")
v6l = []
for r, d, px, pa, pd, rv in sla_tabb:
r = tpm.d2r(r)
d = tpm.d2r(d)
# Milli-arcsec / Trop. yr to arcsec per Trop. century.
pma = pa / 1000.0 * 100.0
pmd = pd / 1000.0 * 100.0
px /= 1000.0 # mili-arcsec to arc-sec.
v6 = tpm.cat2v6(r, d, pma, pmd, px, rv, tpm.CB)
v6l.append(v6)
v6o = convert.convertv6(v6l, s1=5, s2=6, epoch=tpm.B1950)
v6o = convert.proper_motion(v6o, tpm.J2000, tpm.B1950)
cat = (tpm.v62cat(v, tpm.CJ) for v in v6o)
for v, s in zip(cat, tab):
ra = math.degrees(tpm.r2r(v['alpha']))
dec = math.degrees(v['delta'])
# arc-sec/cent. to milli-arcsec/Jul. year.
pma = v['pma'] * 1000.0 / 100.0
pmd = v['pmd'] * 1000.0 / 100.0
px = v['px'] * 1e3 # arc-sec to milli-arcsec
ra_diff = abs(ra - s[0]) * 3600.0
dec_diff = abs(dec - s[1]) * 3600.0
px_diff = abs(px - s[2])
pma_diff = abs(pma - s[3])
pmd_diff = abs(pmd - s[4])
rv_diff = abs(v['rv'] - s[5])
self.assertTrue(ra_diff <= 0.001)
self.assertTrue(dec_diff <= 0.001)
self.assertTrue(pma_diff <= 0.001)
self.assertTrue(pmd_diff <= 0.001)
self.assertTrue(px_diff <= 9)
self.assertTrue(rv_diff <= 0.04)
def testEcl2equ(self):
"""tpm.ecl2equ => Ecliptic to FK5 equatorial."""
v6 = tpm.V6S(r=1.0, alpha=tpm.M_PI / 4.0, delta=tpm.M_PI / 4.0)
v6 = v6.s2c()
v6.xdot = -0.034
v6.ydot = -0.12
v6.zdot = -0.9
v6 = tpm.ecl2equ(v6, tpm.d2r(23.7))
self.verify(
v6, tpm.V6C(x=0.5, y=0.173611298, z=0.848445117, xdot=-0.034000000, ydot=0.251873488, zdot=-0.872330067)
)
def testEcl2equ(self):
"""tpm.ecl2equ => Ecliptic to FK5 equatorial."""
v6 = tpm.V6S(r=1.0,alpha=tpm.M_PI/4.0,delta=tpm.M_PI/4.0)
v6 = v6.s2c()
v6.xdot = -0.034
v6.ydot = -0.12
v6.zdot = -0.9
v6 = tpm.ecl2equ(v6, tpm.d2r(23.7))
self.verify(v6, tpm.V6C(x=0.5, y=0.173611298, z=0.848445117,
xdot=-0.034000000, ydot=0.251873488,
zdot=-0.872330067))
def test_slalib_hip_fk52appradec(self):
"""convert(x, s1=6, s2=11) + PM => SLALIB sla_map HIP."""
tab = get_sla("slalib_hip_map.txt")
v6l = []
for r, d, pa, pd, px in zip(self.hip_tab['raj2'],
self.hip_tab['decj2'],
self.hip_tab['pma'],
self.hip_tab['pmd'],
self.hip_tab['px']):
r = tpm.d2r(r)
d = tpm.d2r(d)
# Milli-arcsec / Jul. yr to arcsec per Jul. century.
pma = pa / math.cos(d) / 1000.0 * 100.0
pmd = pd / 1000.0 * 100.0
px /= 1000.0 # mili-arcsec to arc-sec.
v6 = tpm.cat2v6(r, d, pma, pmd, px, 0.0, tpm.CJ)
v6l.append(v6)
utc = tpm.gcal2j(2010, 1, 1) - 0.5 # midnight
tt = tpm.utc2tdb(utc)
v6o = convert.proper_motion(v6l, tt, tpm.J2000)
v6o = convert.convertv6(v6o, s1=6, s2=11, epoch=tt,
equinox=tpm.J2000,
utc=utc, delta_at=tpm.delta_AT(utc))
cat = (tpm.v62cat(v, tpm.CJ) for v in v6o)
l = len(v6o)
for v, s, i in zip(cat, tab, range(l)):
ra = math.degrees(tpm.r2r(v['alpha']))
dec = math.degrees(v['delta'])
ra_diff = abs(ra - s[0]) * 3600.0
dec_diff = abs(dec - s[1]) * 3600.0
self.assertTrue(ra_diff <= 0.33)
self.assertTrue(dec_diff <= 0.03)
def test_slalib_nwdfs_eqecl(self):
"""convertv6(x,s1=6,s=3) <=> SLALIB eqecl NDWFS"""
v6l = []
for r, d in zip(self.ndwfs_tab['raj2'], self.ndwfs_tab['decj2']):
v6 = tpm.V6S()
v6.r = 1e9
v6.alpha = tpm.d2r(r)
v6.delta = tpm.d2r(d)
v6l.append(v6.s2c())
v6o = convert.convertv6(v6l, s1=6, s2=3)
cat = (tpm.v62cat(v, tpm.CJ) for v in v6o)
tab = get_sla("slalib_ndwfs_eqecl.txt")
for v, s in zip(cat, tab):
ra = math.degrees(tpm.r2r(v['alpha']))
dec = math.degrees(v['delta'])
ra_diff = abs(ra - s[0]) * 3600.0
dec_diff = abs(dec - s[1]) * 3600.0
self.assertTrue(ra_diff <= 0.001 )
self.assertTrue(dec_diff <= 0.001)
def test_slalib_hip_ecleq(self):
"""convertv6(x,s1=3,s=6) <=> SLALIB ecleq HIP"""
v6l = []
for r, d in zip(self.hip_tab['elon2'], self.hip_tab['elat2']):
v6 = tpm.V6S()
v6.r = 1e9
v6.alpha = tpm.d2r(r)
v6.delta = tpm.d2r(d)
v6l.append(v6.s2c())
v6o = convert.convertv6(v6l, s1=3, s2=6)
cat = (tpm.v62cat(v, tpm.CJ) for v in v6o)
tab = get_sla("slalib_hip_ecleq.txt")
for v, s in zip(cat, tab):
ra = math.degrees(tpm.r2r(v['alpha']))
dec = math.degrees(v['delta'])
ra_diff = abs(ra - s[0]) * 3600.0
dec_diff = abs(dec - s[1]) * 3600.0
self.assertTrue(ra_diff <= 0.001)
self.assertTrue(dec_diff <= 0.001)
def test_slalib_nwdfs_eqecl(self):
"""convertv6(x,s1=6,s=3) <=> SLALIB eqecl NDWFS"""
v6l = []
for r, d in zip(self.ndwfs_tab['raj2'], self.ndwfs_tab['decj2']):
v6 = tpm.V6S()
v6.r = 1e9
v6.alpha = tpm.d2r(r)
v6.delta = tpm.d2r(d)
v6l.append(v6.s2c())
v6o = convert.convertv6(v6l, s1=6, s2=3)
cat = (tpm.v62cat(v, tpm.CJ) for v in v6o)
tab = get_sla("slalib_ndwfs_eqecl.txt")
for v, s in zip(cat, tab):
ra = math.degrees(tpm.r2r(v['alpha']))
dec = math.degrees(v['delta'])
ra_diff = abs(ra - s[0]) * 3600.0
dec_diff = abs(dec - s[1]) * 3600.0
self.assertTrue(ra_diff <= 0.001)
self.assertTrue(dec_diff <= 0.001)
def test_slalib_hip_ecleq(self):
"""convertv6(x,s1=3,s=6) <=> SLALIB ecleq HIP"""
v6l = []
for r, d in zip(self.hip_tab['elon2'], self.hip_tab['elat2']):
v6 = tpm.V6S()
v6.r = 1e9
v6.alpha = tpm.d2r(r)
v6.delta = tpm.d2r(d)
v6l.append(v6.s2c())
v6o = convert.convertv6(v6l, s1=3, s2=6)
cat = (tpm.v62cat(v, tpm.CJ) for v in v6o)
tab = get_sla("slalib_hip_ecleq.txt")
for v, s in zip(cat, tab):
ra = math.degrees(tpm.r2r(v['alpha']))
dec = math.degrees(v['delta'])
ra_diff = abs(ra - s[0]) * 3600.0
dec_diff = abs(dec - s[1]) * 3600.0
self.assertTrue(ra_diff <= 0.001)
self.assertTrue(dec_diff <= 0.001)