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 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 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 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 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 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 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 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 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_fk52obs(self): """convert(x, s1=6, s2=19) (+ s2=20) + PM => SLALIB sla_aop HIP.""" tab = get_sla("slalib_hip_aop.txt") az_sla = [] zd_sla = [] ha_sla = [] dec_sla = [] ra_sla = [] for i in tab: # Convert longitude values to 0 - 360 az_sla.append(i[0] if i[0] >= 0 else i[0] + 360.0) zd_sla.append(i[1]) ha_sla.append(i[2] if i[2] >= 0 else i[2] + 360.0) dec_sla.append(i[3]) ra_sla.append(i[4] if i[4] >= 0 else i[4] + 360.0) 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) # Convert to Az-EL. v6o = convert.proper_motion(v6l, tt, tpm.J2000) v6o = convert.convertv6(v6o, s1=6, s2=19, utc=utc) cat = (tpm.v62cat(v, tpm.CJ) for v in v6o) az = [] zd = [] for i in cat: az.append(tpm.r2d(i['alpha'])) zd.append(90.0 - tpm.r2d(i['delta'])) # Convert Az-El to HA-Dec. v6o = convert.convertv6(v6o, s1=19, s2=20, utc=utc) cat = (tpm.v62cat(v, tpm.CJ) for v in v6o) # Find LAST. tstate = tpm.TSTATE() tpm.tpm_data(tstate, tpm.TPM_INIT) tstate.utc = utc tstate.delta_ut = tpm.delta_UT(utc) tstate.delta_at = tpm.delta_AT(utc) tstate.lon = tpm.d2r(-111.598333) tstate.lat = tpm.d2r(31.956389) tpm.tpm_data(tstate, tpm.TPM_ALL) last = tpm.r2d(tstate.last) ha = [] dec = [] ra = [] for i in cat: ha.append(tpm.r2d(i['alpha'])) dec.append(tpm.r2d(i['delta'])) # RA = LAST - HA and convert to 0 - 360. x = last - tpm.r2d(i['alpha']) ra.append(x if x >= 0 else x + 360.0) for i in range(len(az)): # Test only the coordinates with ZD < 75.0. if zd[i] < 75.0: self.assertTrue(abs(az[i] - az_sla[i]) * 3600.0 <= 0.25) self.assertTrue(abs(zd[i] - zd_sla[i]) * 3600.0 <= 0.04) self.assertTrue(abs(ha[i] - ha_sla[i]) * 3600.0 <= 0.28) self.assertTrue(abs(dec[i] - dec_sla[i]) * 3600.0 <= 0.04) self.assertTrue(abs(ra[i] - ra_sla[i]) * 3600.0 <= 0.33)