コード例 #1
0
    def apci(self, frame_or_coord):
        '''
        Wrapper for ``erfa.apci``, used in conversions CIRS <-> ICRS

        Arguments
        ---------
        frame_or_coord: ``astropy.coordinates.BaseCoordinateFrame`` or ``astropy.coordinates.SkyCoord``
            Frame or coordinate instance in the corresponding frame
            for which to calculate the calculate the astrom values.
            For this function, a CIRS frame is expected.
        '''
        obstime = frame_or_coord.obstime
        # no point in interpolating for a single value
        if obstime.size == 1:
            return super().apci(frame_or_coord)

        support = self._get_support_points(obstime)

        cip = self._get_cip(support, obstime)
        earth_pv, earth_heliocentric = self._prepare_earth_position_vel(
            support, obstime)

        jd1_tt, jd2_tt = get_jd12(obstime, 'tt')
        astrom = erfa.apci(jd1_tt, jd2_tt, earth_pv, earth_heliocentric, *cip)
        return astrom
コード例 #2
0
def icrs_to_cirs(icrs_coo, cirs_frame):
    # first set up the astrometry context for ICRS<->CIRS
    jd1, jd2 = get_jd12(cirs_frame.obstime, 'tt')
    x, y, s = get_cip(jd1, jd2)
    earth_pv, earth_heliocentric = prepare_earth_position_vel(
        cirs_frame.obstime)
    # erfa.apci requests TDB but TT can be used instead of TDB without any significant impact on accuracy
    astrom = erfa.apci(jd1, jd2, earth_pv, earth_heliocentric, x, y, s)

    if icrs_coo.data.get_name(
    ) == 'unitspherical' or icrs_coo.data.to_cartesian().x.unit == u.one:
        # if no distance, just do the infinite-distance/no parallax calculation
        usrepr = icrs_coo.represent_as(UnitSphericalRepresentation)
        i_ra = usrepr.lon.to_value(u.radian)
        i_dec = usrepr.lat.to_value(u.radian)
        cirs_ra, cirs_dec = atciqz(i_ra, i_dec, astrom)

        newrep = UnitSphericalRepresentation(lat=u.Quantity(cirs_dec,
                                                            u.radian,
                                                            copy=False),
                                             lon=u.Quantity(cirs_ra,
                                                            u.radian,
                                                            copy=False),
                                             copy=False)
    else:
        # When there is a distance,  we first offset for parallax to get the
        # astrometric coordinate direction and *then* run the ERFA transform for
        # no parallax/PM. This ensures reversibility and is more sensible for
        # inside solar system objects
        astrom_eb = CartesianRepresentation(astrom['eb'],
                                            unit=u.au,
                                            xyz_axis=-1,
                                            copy=False)
        newcart = icrs_coo.cartesian - astrom_eb

        srepr = newcart.represent_as(SphericalRepresentation)
        i_ra = srepr.lon.to_value(u.radian)
        i_dec = srepr.lat.to_value(u.radian)
        cirs_ra, cirs_dec = atciqz(i_ra, i_dec, astrom)

        newrep = SphericalRepresentation(lat=u.Quantity(cirs_dec,
                                                        u.radian,
                                                        copy=False),
                                         lon=u.Quantity(cirs_ra,
                                                        u.radian,
                                                        copy=False),
                                         distance=srepr.distance,
                                         copy=False)

    return cirs_frame.realize_frame(newrep)
コード例 #3
0
    def apci(frame_or_coord):
        '''
        Wrapper for ``erfa.apci``, used in conversions CIRS <-> ICRS

        Arguments
        ---------
        frame_or_coord: ``astropy.coordinates.BaseCoordinateFrame`` or ``astropy.coordinates.SkyCoord``
            Frame or coordinate instance in the corresponding frame
            for which to calculate the calculate the astrom values.
            For this function, a CIRS frame is expected.
        '''
        jd1_tt, jd2_tt = get_jd12(frame_or_coord.obstime, 'tt')
        cip = get_cip(jd1_tt, jd2_tt)
        earth_pv, earth_heliocentric = prepare_earth_position_vel(
            frame_or_coord.obstime)
        return erfa.apci(jd1_tt, jd2_tt, earth_pv, earth_heliocentric, *cip)
コード例 #4
0
def cirs_to_icrs(cirs_coo, icrs_frame):
    srepr = cirs_coo.represent_as(SphericalRepresentation)
    cirs_ra = srepr.lon.to_value(u.radian)
    cirs_dec = srepr.lat.to_value(u.radian)

    # set up the astrometry context for ICRS<->cirs and then convert to
    # astrometric coordinate direction
    jd1, jd2 = get_jd12(cirs_coo.obstime, 'tt')
    x, y, s = get_cip(jd1, jd2)
    earth_pv, earth_heliocentric = prepare_earth_position_vel(cirs_coo.obstime)
    # erfa.apci requests TDB but TT can be used instead of TDB without any significant impact on accuracy
    astrom = erfa.apci(jd1, jd2, earth_pv, earth_heliocentric, x, y, s)
    i_ra, i_dec = aticq(cirs_ra, cirs_dec, astrom)

    if cirs_coo.data.get_name(
    ) == 'unitspherical' or cirs_coo.data.to_cartesian().x.unit == u.one:
        # if no distance, just use the coordinate direction to yield the
        # infinite-distance/no parallax answer
        newrep = UnitSphericalRepresentation(lat=u.Quantity(i_dec,
                                                            u.radian,
                                                            copy=False),
                                             lon=u.Quantity(i_ra,
                                                            u.radian,
                                                            copy=False),
                                             copy=False)
    else:
        # When there is a distance, apply the parallax/offset to the SSB as the
        # last step - ensures round-tripping with the icrs_to_cirs transform

        # the distance in intermedrep is *not* a real distance as it does not
        # include the offset back to the SSB
        intermedrep = SphericalRepresentation(lat=u.Quantity(i_dec,
                                                             u.radian,
                                                             copy=False),
                                              lon=u.Quantity(i_ra,
                                                             u.radian,
                                                             copy=False),
                                              distance=srepr.distance,
                                              copy=False)

        astrom_eb = CartesianRepresentation(astrom['eb'],
                                            unit=u.au,
                                            xyz_axis=-1,
                                            copy=False)
        newrep = intermedrep + astrom_eb

    return icrs_frame.realize_frame(newrep)
コード例 #5
0
ファイル: ex_ast.py プロジェクト: nirinA/erfa_numpy
        )
    ]
)

# era 2000A CIP.
r = erfa.pnm00a(tt1, tt2)
x, y = erfa.bpn2xy(r)

# Apply IERS corrections.
x += dx
y += dy
# SOFA CIO locator. */
s = erfa.s06(tt1, tt2, x, y)

# Populate the context.
astrom = erfa.apci(tt1, tt2, pvb, pvh, x, y, s)

# Carry out the transformation and report the results.
ri, di = erfa.atciq(rc, dc, pr, pd, px, rv, astrom)
reprd("ICRS -> CIRS (JPL, IERS):", ri, di)

# The same but with Saturn then Jupiter then Sun light deflection.
b0 = erfa.LDBODY(
    (
        0.00028574,
        3e-10,
        np.array(
            (
                (-7.8101442680818964, -5.6095668114887358, -1.9807981923749924),
                (0.0030723248971152, -0.0040699547707598, -0.0018133584165345),
            )
コード例 #6
0
ファイル: ex_ast.py プロジェクト: nirinA/erfa_python
# JPL DE405 barycentric Earth ephemeris.
pvb = ((-0.9741704366519668, -0.2115201000882231, -0.0917583114068277),
       (0.0036436589347388, -0.0154287318503146, -0.0066892203821059))

# era 2000A CIP.
r = erfa.pnm00a(tt1, tt2)
x, y = erfa.bpn2xy(r)

# Apply IERS corrections.
x += dx
y += dy
# SOFA CIO locator. */
s = erfa.s06(tt1, tt2, x, y)

# Populate the context.
astrom = erfa.apci(tt1, tt2, pvb, pvh[0], x, y, s)

# Carry out the transformation and report the results.
ri, di = erfa.atciq(rc, dc, pr, pd, px, rv, *astrom)
reprd("ICRS -> CIRS (JPL, IERS):", ri, di)

# The same but with Saturn then Jupiter then Sun light deflection.
b0 = erfa.LDBODY(
    (0.00028574, 3e-10,
     ((-7.8101442680818964, -5.6095668114887358, -1.9807981923749924),
      (0.0030723248971152, -0.0040699547707598, -0.0018133584165345))))
b1 = erfa.LDBODY(
    (0.00095435, 3e-9,
     ((0.7380987962351833, .6365869247538951, 1.9693136030111202),
      (-0.0075581692172088, 0.0012691372216750, 0.0007279990012801))))
b2 = erfa.LDBODY(