"""
This series of functions are used to generate the reference CSV files
used by the accuracy tests.  Running this as a comand-line script will
generate them all.
"""
from __future__ import (absolute_import, division, print_function,
                        unicode_literals)

import os

import numpy as np

from ....table import Table, Column
from ....extern.six.moves import range


def ref_fk4_no_e_fk4(fnout='fk4_no_e_fk4.csv'):
    """
    Accuracy tests for the FK4 (with no E-terms of aberration) to/from FK4
    conversion, with arbitrary equinoxes and epoch of observation.
    """

    import starlink.Ast as Ast

    np.random.seed(12345)

    N = 200

    # Sample uniformly on the unit sphere. These will be either the FK4
    # coordinates for the transformation to FK5, or the FK5 coordinates for the
    # transformation to FK4.
    ra = np.random.uniform(0., 360., N)
    dec = np.degrees(np.arcsin(np.random.uniform(-1., 1., N)))

    # Generate random observation epoch and equinoxes
    obstime = ["B{0:7.2f}".format(x) for x in np.random.uniform(1950., 2000., N)]

    ra_fk4ne, dec_fk4ne = [], []
    ra_fk4, dec_fk4 = [], []

    for i in range(N):

        # Set up frames for AST
        frame_fk4ne = Ast.SkyFrame('System=FK4-NO-E,Epoch={epoch},Equinox=B1950'.format(epoch=obstime[i]))
        frame_fk4 = Ast.SkyFrame('System=FK4,Epoch={epoch},Equinox=B1950'.format(epoch=obstime[i]))

        # FK4 to FK4 (no E-terms)
        frameset = frame_fk4.convert(frame_fk4ne)
        coords = np.degrees(frameset.tran([[np.radians(ra[i])], [np.radians(dec[i])]]))
        ra_fk4ne.append(coords[0, 0])
        dec_fk4ne.append(coords[1, 0])

        # FK4 (no E-terms) to FK4
        frameset = frame_fk4ne.convert(frame_fk4)
        coords = np.degrees(frameset.tran([[np.radians(ra[i])], [np.radians(dec[i])]]))
        ra_fk4.append(coords[0, 0])
        dec_fk4.append(coords[1, 0])

    # Write out table to a CSV file
    t = Table()
    t.add_column(Column(name='obstime', data=obstime))
    t.add_column(Column(name='ra_in', data=ra))
    t.add_column(Column(name='dec_in', data=dec))
    t.add_column(Column(name='ra_fk4ne', data=ra_fk4ne))
    t.add_column(Column(name='dec_fk4ne', data=dec_fk4ne))
    t.add_column(Column(name='ra_fk4', data=ra_fk4))
    t.add_column(Column(name='dec_fk4', data=dec_fk4))
    f = open(fnout, 'wb')
    f.write("# This file was generated with the {0} script, and the reference "
            "values were computed using AST\n".format(os.path.basename(__file__)))
    t.write(f, format='ascii', delimiter=',')


def ref_fk4_no_e_fk5(fnout='fk4_no_e_fk5.csv'):
    """
    Accuracy tests for the FK4 (with no E-terms of aberration) to/from FK5
    conversion, with arbitrary equinoxes and epoch of observation.
    """

    import starlink.Ast as Ast

    np.random.seed(12345)

    N = 200

    # Sample uniformly on the unit sphere. These will be either the FK4
    # coordinates for the transformation to FK5, or the FK5 coordinates for the
    # transformation to FK4.
    ra = np.random.uniform(0., 360., N)
    dec = np.degrees(np.arcsin(np.random.uniform(-1., 1., N)))

    # Generate random observation epoch and equinoxes
    obstime = ["B{0:7.2f}".format(x) for x in np.random.uniform(1950., 2000., N)]
    equinox_fk4 = ["B{0:7.2f}".format(x) for x in np.random.uniform(1925., 1975., N)]
    equinox_fk5 = ["J{0:7.2f}".format(x) for x in np.random.uniform(1975., 2025., N)]

    ra_fk4, dec_fk4 = [], []
    ra_fk5, dec_fk5 = [], []

    for i in range(N):

        # Set up frames for AST
        frame_fk4 = Ast.SkyFrame('System=FK4-NO-E,Epoch={epoch},Equinox={equinox_fk4}'.format(epoch=obstime[i], equinox_fk4=equinox_fk4[i]))
        frame_fk5 = Ast.SkyFrame('System=FK5,Epoch={epoch},Equinox={equinox_fk5}'.format(epoch=obstime[i], equinox_fk5=equinox_fk5[i]))

        # FK4 to FK5
        frameset = frame_fk4.convert(frame_fk5)
        coords = np.degrees(frameset.tran([[np.radians(ra[i])], [np.radians(dec[i])]]))
        ra_fk5.append(coords[0, 0])
        dec_fk5.append(coords[1, 0])

        # FK5 to FK4
        frameset = frame_fk5.convert(frame_fk4)
        coords = np.degrees(frameset.tran([[np.radians(ra[i])], [np.radians(dec[i])]]))
        ra_fk4.append(coords[0, 0])
        dec_fk4.append(coords[1, 0])

    # Write out table to a CSV file
    t = Table()
    t.add_column(Column(name='equinox_fk4', data=equinox_fk4))
    t.add_column(Column(name='equinox_fk5', data=equinox_fk5))
    t.add_column(Column(name='obstime', data=obstime))
    t.add_column(Column(name='ra_in', data=ra))
    t.add_column(Column(name='dec_in', data=dec))
    t.add_column(Column(name='ra_fk5', data=ra_fk5))
    t.add_column(Column(name='dec_fk5', data=dec_fk5))
    t.add_column(Column(name='ra_fk4', data=ra_fk4))
    t.add_column(Column(name='dec_fk4', data=dec_fk4))
    f = open(fnout, 'wb')
    f.write("# This file was generated with the {0} script, and the reference "
            "values were computed using AST\n".format(os.path.basename(__file__)))
    t.write(f, format='ascii', delimiter=',')


def ref_galactic_fk4(fnout='galactic_fk4.csv'):
    """
    Accuracy tests for the ICRS (with no E-terms of aberration) to/from FK5
    conversion, with arbitrary equinoxes and epoch of observation.
    """

    import starlink.Ast as Ast

    np.random.seed(12345)

    N = 200

    # Sample uniformly on the unit sphere. These will be either the ICRS
    # coordinates for the transformation to FK5, or the FK5 coordinates for the
    # transformation to ICRS.
    lon = np.random.uniform(0., 360., N)
    lat = np.degrees(np.arcsin(np.random.uniform(-1., 1., N)))

    # Generate random observation epoch and equinoxes
    obstime = ["B{0:7.2f}".format(x) for x in np.random.uniform(1950., 2000., N)]
    equinox_fk4 = ["J{0:7.2f}".format(x) for x in np.random.uniform(1975., 2025., N)]

    lon_gal, lat_gal = [], []
    ra_fk4, dec_fk4 = [], []

    for i in range(N):

        # Set up frames for AST
        frame_gal = Ast.SkyFrame('System=Galactic,Epoch={epoch}'.format(epoch=obstime[i]))
        frame_fk4 = Ast.SkyFrame('System=FK4,Epoch={epoch},Equinox={equinox_fk4}'.format(epoch=obstime[i], equinox_fk4=equinox_fk4[i]))

        # ICRS to FK5
        frameset = frame_gal.convert(frame_fk4)
        coords = np.degrees(frameset.tran([[np.radians(lon[i])], [np.radians(lat[i])]]))
        ra_fk4.append(coords[0, 0])
        dec_fk4.append(coords[1, 0])

        # FK5 to ICRS
        frameset = frame_fk4.convert(frame_gal)
        coords = np.degrees(frameset.tran([[np.radians(lon[i])], [np.radians(lat[i])]]))
        lon_gal.append(coords[0, 0])
        lat_gal.append(coords[1, 0])

    # Write out table to a CSV file
    t = Table()
    t.add_column(Column(name='equinox_fk4', data=equinox_fk4))
    t.add_column(Column(name='obstime', data=obstime))
    t.add_column(Column(name='lon_in', data=lon))
    t.add_column(Column(name='lat_in', data=lat))
    t.add_column(Column(name='ra_fk4', data=ra_fk4))
    t.add_column(Column(name='dec_fk4', data=dec_fk4))
    t.add_column(Column(name='lon_gal', data=lon_gal))
    t.add_column(Column(name='lat_gal', data=lat_gal))
    f = open(fnout, 'wb')
    f.write("# This file was generated with the {0} script, and the reference "
            "values were computed using AST\n".format(os.path.basename(__file__)))
    t.write(f, format='ascii', delimiter=',')


def ref_icrs_fk5(fnout='icrs_fk5.csv'):
    """
    Accuracy tests for the ICRS (with no E-terms of aberration) to/from FK5
    conversion, with arbitrary equinoxes and epoch of observation.
    """

    import starlink.Ast as Ast

    np.random.seed(12345)

    N = 200

    # Sample uniformly on the unit sphere. These will be either the ICRS
    # coordinates for the transformation to FK5, or the FK5 coordinates for the
    # transformation to ICRS.
    ra = np.random.uniform(0., 360., N)
    dec = np.degrees(np.arcsin(np.random.uniform(-1., 1., N)))

    # Generate random observation epoch and equinoxes
    obstime = ["B{0:7.2f}".format(x) for x in np.random.uniform(1950., 2000., N)]
    equinox_fk5 = ["J{0:7.2f}".format(x) for x in np.random.uniform(1975., 2025., N)]

    ra_icrs, dec_icrs = [], []
    ra_fk5, dec_fk5 = [], []

    for i in range(N):

        # Set up frames for AST
        frame_icrs = Ast.SkyFrame('System=ICRS,Epoch={epoch}'.format(epoch=obstime[i]))
        frame_fk5 = Ast.SkyFrame('System=FK5,Epoch={epoch},Equinox={equinox_fk5}'.format(epoch=obstime[i], equinox_fk5=equinox_fk5[i]))

        # ICRS to FK5
        frameset = frame_icrs.convert(frame_fk5)
        coords = np.degrees(frameset.tran([[np.radians(ra[i])], [np.radians(dec[i])]]))
        ra_fk5.append(coords[0, 0])
        dec_fk5.append(coords[1, 0])

        # FK5 to ICRS
        frameset = frame_fk5.convert(frame_icrs)
        coords = np.degrees(frameset.tran([[np.radians(ra[i])], [np.radians(dec[i])]]))
        ra_icrs.append(coords[0, 0])
        dec_icrs.append(coords[1, 0])

    # Write out table to a CSV file
    t = Table()
    t.add_column(Column(name='equinox_fk5', data=equinox_fk5))
    t.add_column(Column(name='obstime', data=obstime))
    t.add_column(Column(name='ra_in', data=ra))
    t.add_column(Column(name='dec_in', data=dec))
    t.add_column(Column(name='ra_fk5', data=ra_fk5))
    t.add_column(Column(name='dec_fk5', data=dec_fk5))
    t.add_column(Column(name='ra_icrs', data=ra_icrs))
    t.add_column(Column(name='dec_icrs', data=dec_icrs))
    f = open(fnout, 'wb')
    f.write("# This file was generated with the {0} script, and the reference "
            "values were computed using AST\n".format(os.path.basename(__file__)))
    t.write(f, format='ascii', delimiter=',')

if __name__ == '__main__':
    ref_fk4_no_e_fk4()
    ref_fk4_no_e_fk5()
    ref_galactic_fk4()
    ref_icrs_fk5()