Exemplo n.º 1
0
def main(args):
    date = args.date.split(' ')
    leap_secs = 37
    epoc_hip = 2448349.0625
    # Date to convert the catalog to
    jd_utc = novas.julian_date(int(date[0]), int(date[1]), int(date[2]),
                               float(date[3]))
    jd_tt = jd_utc + (leap_secs + 32.184) / 86400
    # jd_tt = novas.julian_date(1991, 4, 2, 12.5)
    converted = []

    # Read the original catalog content
    with open(args.input, 'r') as raw:
        content = [[field.strip() for field in line.split()] for line in raw]

    for line in content:
        if not data_complete(line):
            continue
        ra_degrees = float(line[4]) * 180 / math.pi
        ra_hours = deg_to_decimal_time(ra_degrees)
        dec_degrees = float(line[5]) * 180 / math.pi
        parallax = float(line[6]) if float(line[6]) > 0 else 0.0
        vmag = float(line[19])
        star = novas.make_cat_entry(line[0], "HIP", int(line[0]),
                                    ra_hours, dec_degrees, float(line[7]),
                                    float(line[8]), parallax, 0.0)

        star_con = novas.transform_cat(1, epoc_hip, star, jd_tt, "HP2")
        star_entry = CatEntry(star_con.starname, star_con.catalog,
                              star_con.starnumber, star_con.ra, star_con.dec,
                              star_con.promora, star_con.promodec,
                              star_con.parallax, star_con.radialvelocity, vmag)
        converted.append(star_entry)

    # Write new catalog into a file
    with open(args.output, mode='w') as csv_file:
        fieldnames = [
            'HIP_number', 'ra_degrees', 'dec_degrees', 'promora', 'promodec',
            'parallax', 'vmag'
        ]
        writer = csv.DictWriter(csv_file, fieldnames=fieldnames)
        writer.writeheader()
        for star in converted:
            writer.writerow({
                'HIP_number':
                star.starnumber,
                'ra_degrees':
                "{0:.8f}".format(decimal_time_to_degrees(star.ra)),
                'dec_degrees':
                "{0:.8f}".format(star.dec),
                'promora':
                "{0:.8f}".format(star.promora),
                'promodec':
                "{0:.8f}".format(star.promodec),
                'parallax':
                "{0:.8f}".format(star.parallax),
                'vmag':
                "{0:.2f}".format(star.vmag),
            })
def test_setup_Sun():

    test_cat_entry = make_cat_entry('DUMMY', 'xxx', 0, 0.0, 0.0, 0.0, 0.0, 0.0,
                                    0.0)

    test_sun = make_object(0, 10, 'Sun', test_cat_entry)

    sun = lsst_visibility_calculator.setup_Sun()

    assert type(sun) == type(test_sun)
Exemplo n.º 3
0
def setup_Sun():
    """
    Function to establish a NOVAS-object for the Sun
    """

    star = make_cat_entry('DUMMY', 'xxx', 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0)

    sun = make_object(0, 10, 'Sun', star)

    return sun
Exemplo n.º 4
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def V_LSR(RA, dec, dss, timedate):
    """
  Computes the velocity of the local standard of rest w.r.t. the observer
  
  @param ra : J2000 right ascension as a float or as "12h34m56.78s"
  @type  ra : float or str
  
  @param dec : J2000 declination as a float or as "-12d34m56.78s"
  @type  dec : float or str
  
  @param observer : DSN station
  @type  observer : int
  
  @param timedate : date/time of the observation
  @type  timedate : datetime object
  """
    logger.debug("V_LSR: entered with coord types %s and %s", type(RA),
                 type(dec))
    if type(RA) == str and type(dec) == str:
        skypos = coord.SkyCoord(RA, dec, unit=(u.hourangle, u.deg))
    elif type(RA) == float and type(dec) == float:
        skypos = coord.SkyCoord(RA * u.hour, dec * u.degree)
    else:
        raise RuntimeError(RA, dec, "cannot be parsed")
    logger.debug("V_LSR: sky pos: %s", skypos)
    ra2000, dec2000 = skypos.ra.hour, skypos.dec.deg
    logger.debug("V_LSR: J2000 coordinates are %f, %f", ra2000, dec2000)
    sourcename = "%5.2f%+5.2f" % (ra2000, dec2000)
    cat_entry = novas.make_cat_entry(sourcename, "", 0, ra2000, dec2000, 0, 0,
                                     0, 0)
    source = novas.make_object(2, 0, sourcename, cat_entry)
    station = Astronomy.DSN_coordinates.DSS(dss)
    logger.debug("V_LSR: station lat=%f", station.lat * 180 / math.pi)
    logger.debug("V_LSR: station long=%f", station.lon * 180 / math.pi)
    if station.long > math.pi:
        longitude = station.long - 2 * math.pi
    elif station.long < math.pi:
        longitude = station.long + 2 * math.pi
    else:
        longitude = station.long
    observer = novas.make_observer_on_surface(station.lat * 180 / math.pi,
                                              longitude * 180 / math.pi,
                                              station.elev, 0, 0)
    jd = novas.julian_date(timedate.year, timedate.month, timedate.day,
                           timedate.hour + timedate.minute / 60.)
    mjd = DatesTimes.MJD(timedate.year, timedate.month, timedate.day)
    earth = novas.make_object(0, 3, 'Earth', None)
    urthpos, urthvel = novas.ephemeris((jd, 0), earth, origin=0)
    (obspos, obsvel) = novas.geo_posvel(jd, 0, observer, 0)
    totvel = tuple(numpy.array(urthvel) + numpy.array(obsvel))
    (srcpos, srcvel) = novas.starvectors(cat_entry)
    V = novas.rad_vel(source, srcpos, srcvel, totvel, 0, 0, 0)
    logger.debug("V_LSR: velocity of observer w.r.t. Sun= %.2f", V)
    return V + Astronomy.v_sun(mjd, ra2000 / 15., dec2000)
Exemplo n.º 5
0
def test_starvectors():
    epsilon = 1e-10

    p, v = c.starvectors(c.make_cat_entry(
            'POLARIS', 'HIP', 0, 2.530301028, 89.264109444,
            44.22, -11.75, 7.56, -17.4))

    star = starlib.Star(2.530301028, 89.264109444,
                        44.22, -11.75, 7.56, -17.4)

    eq(p, star._position.reshape(3), epsilon)
    eq(v, star._velocity.reshape(3), epsilon)
def test_setup_pointing():

    pointing = ('Vega', '18:36:56.33635', '+38:47:01.2802')

    vega = SkyCoord(pointing[1], pointing[2], unit=(u.hourangle, u.deg))

    test_target = make_cat_entry(pointing[0], 'FK5', 0, vega.ra.hourangle,
                                 vega.dec.deg, 0, 0.0, 0.0, 0.0)

    target = lsst_visibility_calculator.setup_pointing(pointing)

    assert type(target) == type(test_target)
Exemplo n.º 7
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def test_starvectors():
    p, v = c.starvectors(c.make_cat_entry(
            'POLARIS', 'HIP', 0, 2.530301028, 89.264109444,
            44.22, -11.75, 7.56, -17.4))

    star = starlib.Star(2.530301028, 89.264109444,
                        44.22, -11.75, 7.56, -17.4)

    p_epsilon = 1e-10  # AU; 16 digits of agreement
    v_epsilon = 1e-17  # AU/day; 15 digits of agreement

    eq(p, star._position, p_epsilon)
    eq(v, star._velocity, v_epsilon)
Exemplo n.º 8
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def setup_pointing(pointing):
    """Function to establish the field center pointing as a NOVAS-format
    celestial catalog entry.
    
    Proper motion, parallax and radial motion are not yet supported.
    """

    s = SkyCoord(pointing[1], pointing[2], unit=(u.hourangle, u.deg))

    target = make_cat_entry(pointing[0], 'FK5', 0, s.ra.hourangle, s.dec.deg,
                            0, 0.0, 0.0, 0.0)

    # In NOVAS notation, (2,0) indicates a star. (0,10) is the Sun
    #target = make_object(2, 0, pointing[0], field)

    return target
Exemplo n.º 9
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 def __init__(self, 
              latitude, 
              longitude, 
              height = HEIGHT_DEFAULT, 
              ephem_filepath = None,
              deltat_preds_filepath = None
             ):
     ephem_open(ephem_filepath)  #locate the ephemeris data, needed for subsequent NOVAS calls
     dummy_star = make_cat_entry('DUMMY', 'xxx', 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0) 
     self._sun = make_object(0, 10, 'Sun', dummy_star) #type 0, number 10 denotes the Sun
     self._latitude  = latitude 
     self._longitude = longitude
     self._height    = height
     self._temperature = TEMPERATURE_DEFAULT
     self._pressure  = PRESSURE_DEFAULT
     self._update_geo_loc()
     self._julian_clock = JulianClock(deltat_preds_filepath)
Exemplo n.º 10
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def output_catalog_tests(dates):
    polaris1991 = novas.make_cat_entry('11767', 'HIP', 0, 0.0, 89.26413805,
                                       44.22, -11.74, 7.56, 0.0)
    polaris1991.ra = 37.94614689  # HIP uses degrees, not hours
    polaris = novas.transform_hip(polaris1991)
    for i, jd in enumerate(dates):
        ra, dec = call(novas.astro_star, jd, polaris)
        output(
            locals(), r"""

        def test_hipparcos_conversion{i}(earth):
            line = b'H|       11767| |02 31 47.08|+89 15 50.9| 1.97|1|H|037.94614689|+89.26413805| |   7.56|   44.22|  -11.74|  0.39|  0.45|  0.48|  0.47|  0.55|-0.16| 0.05| 0.27|-0.01| 0.08| 0.05| 0.04|-0.12|-0.09|-0.36|  1| 1.22| 11767| 2.756|0.003| 2.067|0.003| | 0.636|0.003|T|0.70|0.00|L| | 2.1077|0.0021|0.014|102| | 2.09| 2.13|   3.97|P|1|A|02319+8915|I| 1| 1| | | |  |   |       |     |     |    |S| |P|  8890|B+88    8 |          |          |0.68|F7:Ib-IIv SB|G\n'
            df = hipparcos.load_dataframe(BytesIO(line))
            star = starlib.Star.from_dataframe(df.iloc[0])
            ra, dec, distance = earth.at(load.timescale().tt_jd({jd})).observe(star).radec()
            compare(ra.hours, {ra!r}, 0.00001 * ra_arcsecond)
            compare(dec.degrees, {dec!r}, 0.00001 * arcsecond)

        """)
Exemplo n.º 11
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def test_star_deflected_by_jupiter(jd):
    star = c.make_cat_entry(
        star_name='Star', catalog='cat', star_num=101,
        ra=1.59132070233, dec=8.5958876464,
        pm_ra=0.0, pm_dec=0.0,
        parallax=0.0, rad_vel=0.0,
        )
    ra0, dec0 = c.app_star(jd.tt, star)

    earth = de405.earth
    star = starlib.Star(
        ra=1.59132070233, dec=8.5958876464,
        pm_ra=0.0, pm_dec=0.0,
        parallax=0.0, radial_velocity=0.0,
        )
    ra, dec, distance = earth(jd).observe(star).apparent().radec(epoch=jd)

    eq(ra0, ra.hours(), 1e-9 * arcsecond_in_hours)
    eq(dec0, dec.degrees(), 1e-9 * arcsecond_in_degrees)
Exemplo n.º 12
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def output_catalog_tests(dates):
    polaris1991 = novas.make_cat_entry(
        '11767', 'HIP', 0, 0.0, 89.26413805,
        44.22, -11.74, 7.56, 0.0)
    polaris1991.ra = 37.94614689  # HIP uses degrees, not hours
    polaris = novas.transform_hip(polaris1991)
    for i, jd in enumerate(dates):
        ra, dec = call(novas.astro_star, jd, polaris)
        output(locals(), r"""

        def test_hipparcos_conversion{i}():
            line = 'H|       11767| |02 31 47.08|+89 15 50.9| 1.97|1|H|037.94614689|+89.26413805| |   7.56|   44.22|  -11.74|  0.39|  0.45|  0.48|  0.47|  0.55|-0.16| 0.05| 0.27|-0.01| 0.08| 0.05| 0.04|-0.12|-0.09|-0.36|  1| 1.22| 11767| 2.756|0.003| 2.067|0.003| | 0.636|0.003|T|0.70|0.00|L| | 2.1077|0.0021|0.014|102| | 2.09| 2.13|   3.97|P|1|A|02319+8915|I| 1| 1| | | |  |   |       |     |     |    |S| |P|  8890|B+88    8 |          |          |0.68|F7:Ib-IIv SB|G\n'
            star = hipparcos.parse(line)
            compare(star.ra.hours, {polaris.ra!r}, 0.001 * ra_arcsecond)
            compare(star.dec.degrees, {polaris.dec!r}, 0.001 * arcsecond)
            ra, dec, distance = de405.earth(tt={jd}).observe(star).radec()
            compare(ra.hours, {ra!r}, 0.001 * ra_arcsecond)
            compare(dec.degrees, {dec!r}, 0.001 * arcsecond)

        """)
Exemplo n.º 13
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    def test_star_deflected_by_jupiter(self):
        for jd_tt in [T0, TA, TB]:
            star = c.make_cat_entry(
                star_name='Star', catalog='cat', star_num=101,
                ra=1.59132070233, dec=8.5958876464,
                pm_ra=0.0, pm_dec=0.0,
                parallax=0.0, rad_vel=0.0,
                )
            ra, dec = c.app_star(jd_tt, star)

            earth = self.e.earth
            star = starlib.Star(
                ra=1.59132070233, dec=8.5958876464,
                pm_ra=0.0, pm_dec=0.0,
                parallax=0.0, radial_velocity=0.0,
                )
            jd = JulianDate(tt=jd_tt)
            g = star.observe_from(earth(jd)).apparent()

            self.eq(ra * tau / 24.0, g.ra, 0.001 * arcsecond)
            self.eq(dec * tau / 360.0, g.dec, 0.001 * arcsecond)
Exemplo n.º 14
0
def test_new_star_deflected_by_jupiter(timepairs):
    """ Tests of generating a stellar position. """
    jd_tt = timepairs[0]
    star = c.make_cat_entry(
        star_name='Star', catalog='cat', star_num=101,
        ra=1.59132070233, dec=8.5958876464,
        pm_ra=0.0, pm_dec=0.0,
        parallax=0.0, rad_vel=0.0,
        )
    ra, dec = c.app_star(jd_tt, star)
        
    earth = emp.earth
    star = starlib.Star(
        ra=1.59132070233, dec=8.5958876464,
        pm_ra=0.0, pm_dec=0.0,
        parallax=0.0, radial_velocity=0.0,
        )
    jd = JulianDate(tt=jd_tt)
    g = star.observe_from(earth(jd)).apparent()
    
    eq(ra * TAU / 24.0, g.ra, 0.001 * arcsecond)
    eq(dec * TAU / 360.0, g.dec, 0.001 * arcsecond)
Exemplo n.º 15
0
def output_subroutine_tests(dates):
    date_floats = [d for d in dates if not isinstance(d, list)]
    delta_t_floats = [+39.707, +57.1136, +63.8285, +66.7846]

    def shorter_cal_date(jd):
        y, m, d, h = novas.cal_date(jd)
        return y, m, d + h / 24.0 - 0.5

    for i, jd in enumerate(date_floats):
        cal_date = call(shorter_cal_date, jd)
        output(locals(), """\
            def test_calendar_date_{i}():
                compare(timelib.calendar_date({jd!r}), array({cal_date}), 0.0)
            """)

    for i, jd in enumerate(date_floats):
        angle = novas.era(jd)
        output(locals(), """\
            def test_earth_rotation_angle_date{i}():
                compare(earthlib.earth_rotation_angle({jd!r}), {angle},
                        0.000001 * arcsecond)
            """)

    for i, jd in enumerate(date_floats):
        angles = novas.e_tilt(jd)
        output(locals(), """\
            def test_earth_tilt_date{i}():
                compare(nutationlib.earth_tilt(JulianDate(tdb={jd!r})),
                        array({angles}), 0.00001 * arcsecond)
            """)

    for i, jd in enumerate(date_floats):
        terms = novas.ee_ct(jd, 0.0, 0)
        output(locals(), """\
            def test_equation_of_the_equinoxes_complimentary_terms_date{i}():
                compare(nutationlib.equation_of_the_equinoxes_complimentary_terms({jd!r}),
                        array({terms}), 0.0000000000000001 * arcsecond)
            """)

    vector = (1.1, 1.2, 1.3)
    tie1 = novas.frame_tie(vector, 0)
    tie2 = novas.frame_tie(vector, -1)
    output(locals(), """\
        def test_forward_frame_tie():
            compare(framelib.ICRS_to_J2000.dot({vector}), {tie1}, 1e-15)

        def test_reverse_frame_tie():
            compare(framelib.ICRS_to_J2000.T.dot({vector}), {tie2}, 1e-15)
        """)

    for i, jd in enumerate(date_floats):
        jcentury = (jd - T0) / 36525.0
        arguments = novas.fund_args(jcentury)
        output(locals(), """\
            def test_fundamental_arguments_date{i}():
                compare(nutationlib.fundamental_arguments({jcentury!r}),
                        array({arguments}), 0.000000001 * arcsecond)
            """)

    for i, jd in enumerate(date_floats):
        psi, eps = nutation_module.iau2000a(jd, 0.0)
        psi *= 1e7 / ASEC2RAD
        eps *= 1e7 / ASEC2RAD
        output(locals(), """\
            def test_iau2000a_date{i}():
                compare(nutationlib.iau2000a({jd!r}),
                        array([{psi}, {eps}]), 0.001)
            """)

    for i, args in enumerate([
          (-4712, 1, 1, 0.0),
          (-4712, 3, 1, 0.0),
          (-4712, 12, 31, 0.5),
          (-241, 3, 25, 19.0),
          (530, 9, 27, 23.5),
          (1976, 3, 7, 12.5),
          (2000, 1, 1, 0.0),
          ]):
        jd = novas.julian_date(*args)
        output(locals(), """\
            def test_julian_date_function_date{i}():
                compare(timelib.julian_date{args}, {jd!r}, 0.0)
            """)

    for i, jd in enumerate(date_floats):
        angle = novas.mean_obliq(jd)
        output(locals(), """\
            def test_mean_obliquity_date{i}():
                compare(nutationlib.mean_obliquity({jd!r}),
                        {angle!r}, 0.0)  # arcseconds
            """)

    for i, jd in enumerate(date_floats):
        vector = [1.1, 1.2, 1.3]
        result = nutation_function(jd, vector)
        output(locals(), """\
            def test_nutation_date{i}():
                matrix = nutationlib.compute_nutation(JulianDate(tdb={jd!r}))
                result = einsum('ij...,j...->i...', matrix, [1.1, 1.2, 1.3])
                compare({result},
                        result, 1e-14)
            """)

    for i, jd in enumerate(date_floats):
        vector = [1.1, 1.2, 1.3]
        result = novas.precession(T0, vector, jd)
        output(locals(), """\
            def test_precession_date{i}():
                matrix = precessionlib.compute_precession({jd!r})
                result = einsum('ij...,j...->i...', matrix, [1.1, 1.2, 1.3])
                compare({result},
                        result, 1e-15)
            """)

    for i, jd in enumerate(date_floats):
        result1 = novas.sidereal_time(jd, 0.0, 0.0, False, True)
        result2 = novas.sidereal_time(jd, 0.0, 99.9, False, True)
        output(locals(), """\
            def test_sidereal_time_on_date{i}():
                jd = JulianDate(tt={jd!r})
                compare(earthlib.sidereal_time(jd), {result1!r}, 1e-13)

            def test_sidereal_time_with_nonzero_delta_t_on_date{i}():
                jd = JulianDate(tt={jd!r} + 99.9 * one_second, delta_t=99.9)
                compare(earthlib.sidereal_time(jd), {result2!r}, 1e-13)
            """)

    p, v = novas.starvectors(novas.make_cat_entry(
        'POLARIS', 'HIP', 0, 2.530301028, 89.264109444,
        44.22, -11.75, 7.56, -17.4))
    output(locals(), """\
        def test_star_vector():
            star = starlib.Star(ra_hours=2.530301028, dec_degrees=89.264109444,
                                ra_mas_per_year=44.22, dec_mas_per_year=-11.75,
                                parallax_mas=7.56, radial_km_per_s=-17.4)
            compare(star._position,
                    {p},
                    1e3 * meter)
            compare(star._velocity,
                    {v},
                    1e-6 * meter)
        """)

    for i, (tt, delta_t) in enumerate(zip(date_floats, delta_t_floats)):
        jd_low = xp = yp = 0.0
        vector = [1.1, 1.2, 1.3]
        ut1 = tt - delta_t * one_second
        result = novas.ter2cel(ut1, jd_low, delta_t, xp, yp, vector)
        output(locals(), """\
            def test_ITRF_to_GCRS_conversion_on_date{i}():
                jd = JulianDate(tt={tt!r}, delta_t={delta_t!r})
                position = positionlib.ITRF_to_GCRS(jd, {vector!r})
                compare(position, {result!r}, 1e-13)
            """)

    for i, jd_tdb in enumerate(date_floats):
        result = novas.tdb2tt(jd_tdb)[1]
        output(locals(), """\
            def test_tdb_minus_tt_on_date{i}():
                result = timelib.tdb_minus_tt({jd_tdb!r})
                compare(result, {result!r}, 1e-16)
            """)
Exemplo n.º 16
0
def output_geocentric_tests(dates):
    for (planet, code), (i, jd) in product(planets, enumerate(dates)):
        obj = novas.make_object(0, code, 'planet{}'.format(code), None)

        ra1, dec1, distance1 = call(novas.astro_planet, jd, obj)
        ra2, dec2, distance2 = call(novas.virtual_planet, jd, obj)
        ra3, dec3, distance3 = call(novas.app_planet, jd, obj)

        assert distance1 == distance2 == distance3

        output(
            locals(), """\

        def test_{planet}_geocentric_date{i}():
            jd = JulianDate(tt={jd!r})
            e = de405.earth(jd)

            distance = length_of((e - de405.{planet}(jd)).position.au)
            compare(distance * OLD_AU, {distance1!r}, 0.5 * meter)

            astrometric = e.observe(de405.{planet})
            ra, dec, distance = astrometric.radec()
            compare(ra.hours, {ra1!r}, 0.001 * ra_arcsecond)
            compare(dec.degrees, {dec1!r}, 0.001 * arcsecond)

            apparent = astrometric.apparent()
            ra, dec, distance = apparent.radec()
            compare(ra.hours, {ra2!r}, 0.001 * ra_arcsecond)
            compare(dec.degrees, {dec2!r}, 0.001 * arcsecond)

            ra, dec, distance = apparent.radec(epoch='date')
            compare(ra.hours, {ra3!r}, 0.001 * ra_arcsecond)
            compare(dec.degrees, {dec3!r}, 0.001 * arcsecond)

        """)

    # And, one star.

    polaris = novas.make_cat_entry('POLARIS', 'HIP', 0, 2.530301028,
                                   89.264109444, 44.22, -11.75, 7.56, -17.4)

    starlist = [('polaris', polaris)]

    for (name, star), (i, jd) in product(starlist, enumerate(dates)):

        ra1, dec1 = call(novas.astro_star, jd, star)
        ra2, dec2 = call(novas.virtual_star, jd, star)
        ra3, dec3 = call(novas.app_star, jd, star)

        output(
            locals(), """\

        def test_{name}_geocentric_date{i}():
            jd = JulianDate(tt={jd!r})
            e = de405.earth(jd)
            star = starlib.Star(ra_hours=2.530301028, dec_degrees=89.264109444,
                                ra_mas_per_year=44.22, dec_mas_per_year=-11.75,
                                parallax_mas=7.56, radial_km_per_s=-17.4)

            astrometric = e.observe(star)
            ra, dec, distance = astrometric.radec()
            compare(ra.hours, {ra1!r}, 0.001 * ra_arcsecond)
            compare(dec.degrees, {dec1!r}, 0.001 * arcsecond)

            apparent = astrometric.apparent()
            ra, dec, distance = apparent.radec()
            compare(ra.hours, {ra2!r}, 0.001 * ra_arcsecond)
            compare(dec.degrees, {dec2!r}, 0.001 * arcsecond)

            ra, dec, distance = apparent.radec(epoch='date')
            compare(ra.hours, {ra3!r}, 0.001 * ra_arcsecond)
            compare(dec.degrees, {dec3!r}, 0.001 * arcsecond)

        """)
def output_geocentric_tests(dates):
    for (planet, code), (i, jd) in product(planets, enumerate(dates)):
        slug = slugify(planet)
        obj = novas.make_object(0, code, 'planet{0}'.format(code), None)

        ra1, dec1, distance1 = call(novas.astro_planet, jd, obj)
        ra2, dec2, distance2 = call(novas.virtual_planet, jd, obj)
        ra3, dec3, distance3 = call(novas.app_planet, jd, obj)

        assert distance1 == distance2 == distance3

        output(
            locals(), """\

        def test_{slug}_geocentric_date{i}(de405, ts):
            t = ts.tt_jd({jd!r})
            reduce_precision(t)

            e = de405['earth'].at(t)
            p = de405[{planet!r}]

            distance = length_of((e - p.at(t)).position.au)
            compare(distance * OLD_AU, {distance1!r}, 0.014 * meter)

            astrometric = e.observe(p)
            ra, dec, distance = astrometric.radec()
            compare(ra.hours, {ra1!r}, 0.0002 * ra_arcsecond)
            compare(dec.degrees, {dec1!r}, 0.0001 * arcsecond)

            apparent = astrometric.apparent()
            ra, dec, distance = apparent.radec()
            compare(ra.hours, {ra2!r}, 0.0002 * ra_arcsecond)
            compare(dec.degrees, {dec2!r}, 0.0001 * arcsecond)

            ra, dec, distance = apparent.radec(epoch='date')
            compare(ra.hours, {ra3!r}, 0.0002 * ra_arcsecond)
            compare(dec.degrees, {dec3!r}, 0.0001 * arcsecond)

        """)

    # And, one star.

    polaris = novas.make_cat_entry('POLARIS', 'HIP', 0, 2.530301028,
                                   89.264109444, 44.22, -11.75, 7.56, -17.4)

    starlist = [('polaris', polaris)]

    for (name, star), (i, jd) in product(starlist, enumerate(dates)):

        ra1, dec1 = call(novas.astro_star, jd, star)
        ra2, dec2 = call(novas.virtual_star, jd, star)
        ra3, dec3 = call(novas.app_star, jd, star)

        output(
            locals(), """\

        def test_{name}_geocentric_date{i}(earth):
            e = earth.at(load.timescale().tt_jd({jd!r}))
            star = starlib.Star(ra_hours=2.530301028, dec_degrees=89.264109444,
                                ra_mas_per_year=44.22, dec_mas_per_year=-11.75,
                                parallax_mas=7.56, radial_km_per_s=-17.4)

            astrometric = e.observe(star)
            ra, dec, distance = astrometric.radec()
            compare(ra.hours, {ra1!r}, 0.00001 * ra_arcsecond)
            compare(dec.degrees, {dec1!r}, 0.00001 * arcsecond)

            apparent = astrometric.apparent()
            ra, dec, distance = apparent.radec()
            compare(ra.hours, {ra2!r}, 0.00001 * ra_arcsecond)
            compare(dec.degrees, {dec2!r}, 0.00001 * arcsecond)

            ra, dec, distance = apparent.radec(epoch='date')
            compare(ra.hours, {ra3!r}, 0.00001 * ra_arcsecond)
            compare(dec.degrees, {dec3!r}, 0.00001 * arcsecond)

        """)
Exemplo n.º 18
0
def output_subroutine_tests(dates):
    date_floats = [d for d in dates if not isinstance(d, list)]
    delta_t_floats = [+39.707, +57.1136, +63.8285, +66.7846]

    def shorter_cal_date(jd):
        y, m, d, h = novas.cal_date(jd)
        return y, m, d + h / 24.0 - 0.5

    for i, jd in enumerate(date_floats):
        cal_date = call(shorter_cal_date, jd)
        output(locals(), """\
            def test_calendar_date_{i}():
                compare(timelib.calendar_date({jd!r}), array({cal_date}), 0.0)
            """)

    for i, jd in enumerate(date_floats):
        angle = novas.era(jd)
        output(locals(), """\
            def test_earth_rotation_angle_date{i}():
                compare(earthlib.earth_rotation_angle({jd!r}) * 360.0, {angle},
                        0.000001 * arcsecond)
            """)

    for i, jd in enumerate(date_floats):
        angles = novas.e_tilt(jd)
        output(locals(), """\
            def test_earth_tilt_date{i}():
                compare(nutationlib.earth_tilt(JulianDate(tdb={jd!r})),
                        array({angles}), 0.00001 * arcsecond)
            """)

    for i, jd in enumerate(date_floats):
        terms = novas.ee_ct(jd, 0.0, 0)
        output(locals(), """\
            def test_equation_of_the_equinoxes_complimentary_terms_date{i}():
                compare(nutationlib.equation_of_the_equinoxes_complimentary_terms({jd!r}),
                        array({terms}), 0.0000000000000001 * arcsecond)
            """)

    vector = (1.1, 1.2, 1.3)
    tie1 = novas.frame_tie(vector, 0)
    tie2 = novas.frame_tie(vector, -1)
    output(locals(), """\
        def test_forward_frame_tie():
            compare(framelib.ICRS_to_J2000.dot({vector}), {tie1}, 1e-15)

        def test_reverse_frame_tie():
            compare(framelib.ICRS_to_J2000.T.dot({vector}), {tie2}, 1e-15)
        """)

    for i, jd in enumerate(date_floats):
        jcentury = (jd - T0) / 36525.0
        arguments = novas.fund_args(jcentury)
        output(locals(), """\
            def test_fundamental_arguments_date{i}():
                compare(nutationlib.fundamental_arguments({jcentury!r}),
                        array({arguments}), 0.000000002 * arcsecond)
            """)

    for i, jd in enumerate(date_floats):
        psi, eps = nutation_module.iau2000a(jd, 0.0)
        psi *= 1e7 / ASEC2RAD
        eps *= 1e7 / ASEC2RAD
        output(locals(), """\
            def test_iau2000a_date{i}():
                compare(nutationlib.iau2000a({jd!r}),
                        array([{psi}, {eps}]), 0.001)
            """)

    for i, args in enumerate([
          (-4712, 1, 1, 0.0),
          (-4712, 3, 1, 0.0),
          (-4712, 12, 31, 0.5),
          (-241, 3, 25, 19.0),
          (530, 9, 27, 23.5),
          (1976, 3, 7, 12.5),
          (2000, 1, 1, 0.0),
          ]):
        jd = novas.julian_date(*args)
        output(locals(), """\
            def test_julian_date_function_date{i}():
                compare(timelib.julian_date{args}, {jd!r}, 0.0)
            """)

    for i, jd in enumerate(date_floats):
        angle = novas.mean_obliq(jd)
        output(locals(), """\
            def test_mean_obliquity_date{i}():
                compare(nutationlib.mean_obliquity({jd!r}),
                        {angle!r}, 0.0)  # arcseconds
            """)

    for i, jd in enumerate(date_floats):
        vector = [1.1, 1.2, 1.3]
        result = nutation_function(jd, vector)
        output(locals(), """\
            def test_nutation_date{i}():
                matrix = nutationlib.compute_nutation(JulianDate(tdb={jd!r}))
                result = einsum('ij...,j...->i...', matrix, [1.1, 1.2, 1.3])
                compare({result},
                        result, 1e-14)
            """)

    for i, jd in enumerate(date_floats):
        vector = [1.1, 1.2, 1.3]
        result = novas.precession(T0, vector, jd)
        output(locals(), """\
            def test_precession_date{i}():
                matrix = precessionlib.compute_precession({jd!r})
                result = einsum('ij...,j...->i...', matrix, [1.1, 1.2, 1.3])
                compare({result},
                        result, 1e-15)
            """)

    for i, jd in enumerate(date_floats):
        result1 = novas.sidereal_time(jd, 0.0, 0.0, False, True)
        result2 = novas.sidereal_time(jd, 0.0, 99.9, False, True)
        output(locals(), """\
            def test_sidereal_time_on_date{i}():
                jd = JulianDate(tt={jd!r})
                compare(earthlib.sidereal_time(jd), {result1!r}, 1e-13)

            def test_sidereal_time_with_nonzero_delta_t_on_date{i}():
                jd = JulianDate(tt={jd!r} + 99.9 * one_second, delta_t=99.9)
                compare(earthlib.sidereal_time(jd), {result2!r}, 1e-13)
            """)

    p, v = novas.starvectors(novas.make_cat_entry(
        'POLARIS', 'HIP', 0, 2.530301028, 89.264109444,
        44.22, -11.75, 7.56, -17.4))
    output(locals(), """\
        def test_star_vector():
            star = starlib.Star(ra_hours=2.530301028, dec_degrees=89.264109444,
                                ra_mas_per_year=44.22, dec_mas_per_year=-11.75,
                                parallax_mas=7.56, radial_km_per_s=-17.4)
            star.au_km = de405.jplephemeris.AU
            star._compute_vectors()
            compare(star._position_au,
                    {p!r},
                    1e3 * meter)
            compare(star._velocity_au_per_d,
                    {v!r},
                    1e-3 * meter)  # TODO: was 1e-6 before switch to modern au
        """)

    atp = product([-5, -1, 15, 89.95], [10, 25], [1010, 1013.25])

    for i, (angle, temperature, pressure) in enumerate(atp):
        location = novas.make_on_surface(0.0, 0.0, 0, temperature, pressure)
        r = novas.refract(location, 90 - angle, 2)
        output(locals(), """\
            def test_refraction{i}():
                r = earthlib.refraction({angle}, {temperature}, {pressure})
                compare(r, {r}, 0.001 * arcsecond)
            """)

    northpole = novas.make_on_surface(90.0, 0.0, 0.0, 10.0, 1010.0)

    for i, angle in enumerate([-90, -2, -1, 0, 1, 3, 9, 90]):
        alt, az = altaz_maneuver(T0, northpole, 0.0, angle, ref=2)
        output(locals(), """\
            def test_refract{i}():
                alt = earthlib.refract({angle!r}, 10.0, 1010.0)
                compare(alt, {alt!r}, 0.000000001 * arcsecond)
            """)

    usno = novas.make_on_surface(38.9215, -77.0669, 92.0, 10.0, 1010.0)

    ra = 12.34
    for i, (tt, dec) in enumerate(product(date_floats, [56.78, -67.89])):
        alt, az = altaz_maneuver(tt, usno, ra, dec, ref=0)
        output(locals(), """\
            def test_from_altaz_{i}():
                jd = JulianDate(tt={tt!r})
                usno = de405.earth.topos(
                    '38.9215 N', '77.0669 W', elevation_m=92.0)
                a = usno(jd).from_altaz(alt_degrees={alt!r}, az_degrees={az!r})
                ra, dec, distance = a.radec(epoch=jd)
                compare(ra.hours, {ra!r}, 0.000000001 * arcsecond)
                compare(dec.degrees, {dec!r}, 0.000000001 * arcsecond)
            """)

    for i, (tt, delta_t) in enumerate(zip(date_floats, delta_t_floats)):
        jd_low = xp = yp = 0.0
        vector = [1.1, 1.2, 1.3]
        ut1 = tt - delta_t * one_second
        result = novas.ter2cel(ut1, jd_low, delta_t, xp, yp, vector)
        output(locals(), """\
            def test_ITRF_to_GCRS_conversion_on_date{i}():
                jd = JulianDate(tt={tt!r}, delta_t={delta_t!r})
                position = positionlib.ITRF_to_GCRS(jd, {vector!r})
                compare(position, {result!r}, 1e-13)
            """)

    for i, jd_tdb in enumerate(date_floats):
        result = novas.tdb2tt(jd_tdb)[1]
        output(locals(), """\
            def test_tdb_minus_tt_on_date{i}():
                result = timelib.tdb_minus_tt({jd_tdb!r})
                compare(result, {result!r}, 1e-16)
            """)
def output_subroutine_tests(dates):
    date_floats = [d for d in dates if not isinstance(d, list)]
    delta_t_floats = [+39.707, +57.1136, +63.8285, +66.7846]

    def shorter_cal_date(jd):
        y, m, d, h = novas.cal_date(jd)
        return y, m, d + h / 24.0 - 0.5

    for i, jd in enumerate(date_floats):
        cal_date = call(shorter_cal_date, jd)
        output(
            locals(), """\
            def test_calendar_date_{i}():
                compare(timelib.calendar_date({jd!r}), array({cal_date}), 0.0)
            """)

    for i, jd in enumerate(date_floats):
        angle = novas.era(jd)
        output(
            locals(), """\
            def test_earth_rotation_angle_date{i}():
                compare(earthlib.earth_rotation_angle({jd!r}) * 360.0, {angle!r},
                        0.000001 * arcsecond)
            """)

    for i, jd in enumerate(date_floats):
        angles = novas.e_tilt(jd)
        output(
            locals(), """\
            def test_earth_tilt_date{i}(ts):
                compare(nutationlib.earth_tilt(ts.tdb_jd({jd!r})),
                        array({angles}), 0.00001 * arcsecond)
            """)

    for i, jd in enumerate(date_floats):
        terms = novas.ee_ct(jd, 0.0, 0)
        output(
            locals(), """\
            def test_equation_of_the_equinoxes_complimentary_terms_date{i}():
                compare(nutationlib.equation_of_the_equinoxes_complimentary_terms({jd!r}),
                        array({terms!r}), 0.0000000000000001 * arcsecond)
            """)

    vector = (1.1, 1.2, 1.3)
    tie1 = novas.frame_tie(vector, 0)
    tie2 = novas.frame_tie(vector, -1)
    output(
        locals(), """\
        def test_forward_frame_tie():
            compare(framelib.ICRS_to_J2000.dot({vector}), {tie1}, 1e-15)

        def test_reverse_frame_tie():
            compare(framelib.ICRS_to_J2000.T.dot({vector}), {tie2}, 1e-15)
        """)

    for i, jd in enumerate(date_floats):
        jcentury = (jd - T0) / 36525.0
        arguments = novas.fund_args(jcentury)
        output(
            locals(), """\
            def test_fundamental_arguments_date{i}():
                compare(nutationlib.fundamental_arguments({jcentury!r}),
                        array({arguments}), 0.000000002 * arcsecond)
            """)

    for i, jd in enumerate(date_floats):
        psi, eps = nutation_module.iau2000a(jd, 0.0)
        psi *= 1e7 / ASEC2RAD
        eps *= 1e7 / ASEC2RAD
        output(
            locals(), """\
            def test_iau2000a_date{i}():
                compare(nutationlib.iau2000a({jd!r}),
                        array([{psi!r}, {eps!r}]), 0.001)
            """)

    for i, jd in enumerate(date_floats):
        psi, eps = nutation_module.iau2000b(jd, 0.0)
        psi *= 1e7 / ASEC2RAD
        eps *= 1e7 / ASEC2RAD
        output(
            locals(), """\
            def test_iau2000b_date{i}():
                compare(nutationlib.iau2000b({jd!r}),
                        array([{psi!r}, {eps!r}]), 0.001)
            """)

    for i, args in enumerate([
        (-4712, 1, 1, 0.0),
        (-4712, 3, 1, 0.0),
        (-4712, 12, 31, 0.5),
        (-241, 3, 25, 19.0),
        (530, 9, 27, 23.5),
        (1976, 3, 7, 12.5),
        (2000, 1, 1, 0.0),
    ]):
        jd = novas.julian_date(*args)
        output(
            locals(), """\
            def test_julian_date_function_date{i}():
                compare(timelib.julian_date{args}, {jd!r}, 0.0)
            """)

    for i, jd in enumerate(date_floats):
        angle = novas.mean_obliq(jd)
        output(
            locals(), """\
            def test_mean_obliquity_date{i}():
                compare(nutationlib.mean_obliquity({jd!r}),
                        {angle!r}, 0.0)  # arcseconds
            """)

    for i, jd in enumerate(date_floats):
        vector = [1.1, 1.2, 1.3]
        result = nutation_function(jd, vector)
        output(
            locals(), """\
            def test_nutation_date{i}(ts):
                matrix = nutationlib.compute_nutation(ts.tdb_jd({jd!r}))
                result = einsum('ij...,j...->i...', matrix, [1.1, 1.2, 1.3])
                compare({result},
                        result, 1e-14)
            """)

    for i, jd in enumerate(date_floats):
        vector = [1.1, 1.2, 1.3]
        result = novas.precession(T0, vector, jd)
        output(
            locals(), """\
            def test_precession_date{i}():
                matrix = precessionlib.compute_precession({jd!r})
                result = einsum('ij...,j...->i...', matrix, [1.1, 1.2, 1.3])
                compare({result},
                        result, 1e-15)
            """)

    for i, jd in enumerate(date_floats):
        result1 = novas.sidereal_time(jd, 0.0, 0.0, False, True)
        result2 = novas.sidereal_time(jd, 0.0, 99.9, False, True)
        output(
            locals(), """\
            def test_sidereal_time_on_date{i}():
                jd = load.timescale(delta_t=0.0).tt_jd({jd!r})
                compare(earthlib.sidereal_time(jd), {result1!r}, 1e-13)

            def test_sidereal_time_with_nonzero_delta_t_on_date{i}():
                jd = load.timescale(delta_t=99.9).tt_jd({jd!r} + 99.9 * one_second)
                compare(earthlib.sidereal_time(jd), {result2!r}, 1e-13)
            """)

    p, v = novas.starvectors(
        novas.make_cat_entry('POLARIS', 'HIP', 0, 2.530301028, 89.264109444,
                             44.22, -11.75, 7.56, -17.4))
    output(
        locals(), """\
        def test_star_vector():
            star = starlib.Star(ra_hours=2.530301028, dec_degrees=89.264109444,
                                ra_mas_per_year=44.22, dec_mas_per_year=-11.75,
                                parallax_mas=7.56, radial_km_per_s=-17.4)
            star.au_km = OLD_AU_KM
            star._compute_vectors()
            compare(star._position_au,
                    {p!r},
                    1e3 * meter)
            compare(star._velocity_au_per_d,
                    {v!r},
                    1e-3 * meter)  # TODO: was 1e-6 before switch to modern au
        """)

    atp = product([-5, -1, 15, 89.95], [10, 25], [1010, 1013.25])

    for i, (angle, temperature, pressure) in enumerate(atp):
        location = novas.make_on_surface(0.0, 0.0, 0, temperature, pressure)
        r = novas.refract(location, 90 - angle, 2)
        output(
            locals(), """\
            def test_refraction{i}():
                r = earthlib.refraction({angle}, {temperature}, {pressure})
                compare(r, {r!r}, 1e-9 * arcsecond)
            """)

    northpole = novas.make_on_surface(90.0, 0.0, 0.0, 10.0, 1010.0)

    for i, angle in enumerate([-90, -2, -1, 0, 1, 3, 9, 90]):
        alt, az = altaz_maneuver(T0, northpole, 0.0, angle, ref=2)
        output(
            locals(), """\
            def test_refract{i}():
                alt = earthlib.refract({angle!r}, 10.0, 1010.0)
                compare(alt, {alt!r}, 1e-9 * arcsecond)
            """)

    usno = novas.make_on_surface(38.9215, -77.0669, 92.0, 10.0, 1010.0)

    ra = 12.34
    for i, (tt, dec) in enumerate(product(date_floats, [56.78, -67.89])):
        alt, az = altaz_maneuver(tt, usno, ra, dec, ref=0)
        output(
            locals(), """\
            def test_from_altaz_{i}(earth):
                jd = load.timescale(delta_t=0.0).tt_jd({tt!r})
                usno = earth + Topos(
                    '38.9215 N', '77.0669 W', elevation_m=92.0)
                a = usno.at(jd).from_altaz(alt_degrees={alt!r}, az_degrees={az!r})
                ra, dec, distance = a.radec(epoch=jd)
                compare(ra.hours, {ra!r}, 1e-9 * arcsecond)
                compare(dec.degrees, {dec!r}, 1e-9 * arcsecond)
            """)

    for i, (tt, delta_t) in enumerate(zip(date_floats, delta_t_floats)):
        jd_low = xp = yp = 0.0
        vector = [1.1, 1.2, 1.3]
        ut1 = tt - delta_t * one_second
        result = novas.ter2cel(ut1, jd_low, delta_t, xp, yp, vector)
        output(
            locals(), """\
            def test_ITRF_to_GCRS_conversion_on_date{i}():
                jd = load.timescale(delta_t={delta_t!r}).tt_jd({tt!r})
                position = positionlib.ITRF_to_GCRS(jd, {vector!r})
                compare(position, {result!r}, 1e-13)
            """)

    for i, jd_tdb in enumerate(date_floats):
        result = novas.tdb2tt(jd_tdb)[1]
        output(
            locals(), """\
            def test_tdb_minus_tt_on_date{i}():
                result = timelib.tdb_minus_tt({jd_tdb!r})
                compare(result, {result!r}, 1e-16)
            """)
Exemplo n.º 20
0
def output_geocentric_tests(dates):
    for (planet, code), (i, jd) in product(planets, enumerate(dates)):
        obj = novas.make_object(0, code, 'planet{}'.format(code), None)

        ra1, dec1, distance1 = call(novas.astro_planet, jd, obj)
        ra2, dec2, distance2 = call(novas.virtual_planet, jd, obj)
        ra3, dec3, distance3 = call(novas.app_planet, jd, obj)

        assert distance1 == distance2 == distance3

        output(locals(), """\

        def test_{planet}_geocentric_date{i}():
            jd = JulianDate(tt={jd!r})
            e = de405.earth(jd)

            distance = length_of((e - de405.{planet}(jd)).position.au)
            compare(distance * OLD_AU, {distance1!r}, 0.5 * meter)

            astrometric = e.observe(de405.{planet})
            ra, dec, distance = astrometric.radec()
            compare(ra.hours, {ra1!r}, 0.001 * ra_arcsecond)
            compare(dec.degrees, {dec1!r}, 0.001 * arcsecond)

            apparent = astrometric.apparent()
            ra, dec, distance = apparent.radec()
            compare(ra.hours, {ra2!r}, 0.001 * ra_arcsecond)
            compare(dec.degrees, {dec2!r}, 0.001 * arcsecond)

            ra, dec, distance = apparent.radec(epoch='date')
            compare(ra.hours, {ra3!r}, 0.001 * ra_arcsecond)
            compare(dec.degrees, {dec3!r}, 0.001 * arcsecond)

        """)

    # And, one star.

    polaris = novas.make_cat_entry(
        'POLARIS', 'HIP', 0, 2.530301028, 89.264109444,
        44.22, -11.75, 7.56, -17.4)

    starlist = [('polaris', polaris)]

    for (name, star), (i, jd) in product(starlist, enumerate(dates)):

        ra1, dec1 = call(novas.astro_star, jd, star)
        ra2, dec2 = call(novas.virtual_star, jd, star)
        ra3, dec3 = call(novas.app_star, jd, star)

        output(locals(), """\

        def test_{name}_geocentric_date{i}():
            jd = JulianDate(tt={jd!r})
            e = de405.earth(jd)
            star = starlib.Star(ra_hours=2.530301028, dec_degrees=89.264109444,
                                ra_mas_per_year=44.22, dec_mas_per_year=-11.75,
                                parallax_mas=7.56, radial_km_per_s=-17.4)

            astrometric = e.observe(star)
            ra, dec, distance = astrometric.radec()
            compare(ra.hours, {ra1!r}, 0.001 * ra_arcsecond)
            compare(dec.degrees, {dec1!r}, 0.001 * arcsecond)

            apparent = astrometric.apparent()
            ra, dec, distance = apparent.radec()
            compare(ra.hours, {ra2!r}, 0.001 * ra_arcsecond)
            compare(dec.degrees, {dec2!r}, 0.001 * arcsecond)

            ra, dec, distance = apparent.radec(epoch='date')
            compare(ra.hours, {ra3!r}, 0.001 * ra_arcsecond)
            compare(dec.degrees, {dec3!r}, 0.001 * arcsecond)

        """)