コード例 #1
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ファイル: time.py プロジェクト: hirax-array/caput
def unix_to_era(unix_time):
    """Calculate the Earth Rotation Angle for a given time.

    The Earth Rotation Angle is the angle between the Celetial and Terrestrial
    Intermediate origins, and is a modern replacement for the Greenwich Sidereal
    Time.

    Parameters
    ----------
    unix_time : float or array of.
        Unix/POSIX time.

    Returns
    -------
    era : float or array of
        The Earth Rotation Angle in degrees.
    """

    from skyfield import earthlib

    t = unix_to_skyfield_time(unix_time)

    era = earthlib.earth_rotation_angle(t.ut1)  # in cycles

    return 360.0 * era
コード例 #2
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ファイル: time.py プロジェクト: radiocosmology/caput
def unix_to_era(unix_time):
    """Calculate the Earth Rotation Angle for a given time.

    The Earth Rotation Angle is the angle between the Celetial and Terrestrial
    Intermediate origins, and is a modern replacement for the Greenwich Sidereal
    Time.

    Parameters
    ----------
    unix_time : float or array of.
        Unix/POSIX time.

    Returns
    -------
    era : float or array of
        The Earth Rotation Angle in degrees.
    """

    from skyfield import earthlib

    t = unix_to_skyfield_time(unix_time)

    era = earthlib.earth_rotation_angle(t.ut1)  # in cycles

    return (360.0 * era)
コード例 #3
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def test_earth_rotation_angle():
    epsilon = 1e-12

    a0 = c.era(T0)
    aA = c.era(TA)
    aB = c.era(TB)

    t = array([T0, TA, TB])
    v = earthlib.earth_rotation_angle(t)
    eq(v, [a0, aA, aB], epsilon)
コード例 #4
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    def test_earth_rotation_angle(self):
        self.delta = 1e-12

        a0 = c.era(T0)
        aA = c.era(TA)
        aB = c.era(TB)

        t = array([T0, TA, TB])
        v = earthlib.earth_rotation_angle(t)
        self.eq(v, [a0, aA, aB])
コード例 #5
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ファイル: test_time.py プロジェクト: radiocosmology/caput
    def test_lsa_skyfield(self):
        # Check an lsa calculated by caput.time against one calculated by PyEphem

        from skyfield import earthlib, api

        dt = datetime(2014, 10, 2, 13, 4, 5)
        dt_utc = dt.replace(tzinfo=api.utc)

        t1 = ctime.datetime_to_unix(dt)
        obs = ctime.Observer(42.8, 4.7)
        lsa1 = obs.unix_to_lsa(t1)

        t = ctime.skyfield_wrapper.timescale.utc(dt_utc)
        lsa2 = (earthlib.earth_rotation_angle(t.ut1) * 360.0 + obs.longitude) % 360.0

        self.assertAlmostEqual(lsa1, lsa2, 4)
コード例 #6
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    def test_lsa_skyfield(self):
        # Check an lsa calculated by caput.time against one calculated by PyEphem

        from skyfield import earthlib, api

        dt = datetime(2014, 10, 2, 13, 4, 5)
        dt_utc = dt.replace(tzinfo=api.utc)

        t1 = ctime.datetime_to_unix(dt)
        obs = ctime.Observer(42.8, 4.7)
        lsa1 = obs.unix_to_lsa(t1)

        t = ctime.skyfield_wrapper.timescale.utc(dt_utc)
        lsa2 = (earthlib.earth_rotation_angle(t.ut1) * 360.0 +
                obs.longitude) % 360.0

        self.assertAlmostEqual(lsa1, lsa2, 4)
コード例 #7
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def test_cirs_era():

    ts = api.load.timescale()
    st = ts.utc(year=np.arange(1951, 2051))

    planets = api.load('de421.bsp')
    pos = planets['earth'] + api.Topos(longitude_degrees=0.0, latitude_degrees=0.0)

    # Get the TIO
    tio = pos.at(st).from_altaz(alt_degrees=90, az_degrees=180)

    # Get the TIOs RA in CIRS coordinates, and the Earth Rotation Angle
    tio_ra, tio_dec, _ = tio.cirs_radec(st)
    era = 360.0 * earth_rotation_angle(st.ut1)

    tol = (1e-8 / 3600.0)  # 10 nano arc-second precision
    assert np.allclose(tio_ra._degrees, era, rtol=0.0, atol=tol)
    assert np.allclose(tio_dec._degrees, 0.0, rtol=0.0, atol=tol)
コード例 #8
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def test_cirs_era():

    ts = api.load.timescale()
    st = ts.utc(year=np.arange(1951, 2051))

    planets = api.load('de421.bsp')
    pos = planets['earth'] + api.Topos(longitude_degrees=0.0, latitude_degrees=0.0)

    # Get the TIO
    tio = pos.at(st).from_altaz(alt_degrees=90, az_degrees=180)

    # Get the TIOs RA in CIRS coordinates, and the Earth Rotation Angle
    tio_ra, tio_dec, _ = tio.cirs_radec(st)
    era = 360.0 * earth_rotation_angle(st.ut1)

    tol = (1e-8 / 3600.0)  # 10 nano arc-second precision
    assert np.allclose(tio_ra._degrees, era, rtol=0.0, atol=tol)
    assert np.allclose(tio_dec._degrees, 0.0, rtol=0.0, atol=tol)
コード例 #9
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def test_cirs_meridian():

    ts = api.load.timescale()
    st = ts.utc(year=2051)

    planets = api.load('de421.bsp')
    pos = planets['earth'] + api.Topos(longitude_degrees=0.0, latitude_degrees=0.0)

    # Get a series of points along the meridian
    alt = np.arange(1, 90)
    meridian = pos.at(st).from_altaz(alt_degrees=alt, az_degrees=0.0)

    # Get the TIOs RA in CIRS coordinates, and the Earth Rotation Angle
    md_ra, md_dec, _ = meridian.cirs_radec(st)
    era = 360.0 * earth_rotation_angle(st.ut1)

    tol = (1e-7 / 3600.0)  # 100 nano arc-second precision
    assert np.allclose(md_ra._degrees, era, rtol=0.0, atol=tol)
    assert np.allclose(md_dec._degrees, 90 - alt, rtol=0.0, atol=tol)
コード例 #10
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def test_cirs_meridian():

    ts = api.load.timescale()
    st = ts.utc(year=2051)

    planets = api.load('de421.bsp')
    pos = planets['earth'] + api.Topos(longitude_degrees=0.0, latitude_degrees=0.0)

    # Get a series of points along the meridian
    alt = np.arange(1, 90)
    meridian = pos.at(st).from_altaz(alt_degrees=alt, az_degrees=0.0)

    # Get the TIOs RA in CIRS coordinates, and the Earth Rotation Angle
    md_ra, md_dec, _ = meridian.cirs_radec(st)
    era = 360.0 * earth_rotation_angle(st.ut1)

    tol = (1e-7 / 3600.0)  # 100 nano arc-second precision
    assert np.allclose(md_ra._degrees, era, rtol=0.0, atol=tol)
    assert np.allclose(md_dec._degrees, 90 - alt, rtol=0.0, atol=tol)
コード例 #11
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def test_earth_rotation_angle(jd_float_or_vector):
    jd_ut1 = jd_float_or_vector
    u = c.era(jd_ut1)
    v = earthlib.earth_rotation_angle(jd_ut1)
    epsilon = 1e-12  # degrees; 14 to 15 digits of agreement
    eq(u, v, epsilon)