def dominant_frequency(self, darray, sample_rate=4, preview=None):
        """
        Description
        -----------
        Compute the Dominant Frequency of the input data
        
        Parameters
        ----------
        darray : Array-like, acceptable inputs include Numpy, HDF5, or Dask Arrays
        
        Keywork Arguments
        -----------------  
        sample_rate : Number, sample rate in milliseconds (ms)
        preview : str, enables or disables preview mode and specifies direction
            Acceptable inputs are (None, 'inline', 'xline', 'z')
            Optimizes chunk size in different orientations to facilitate rapid
            screening of algorithm output
        
        Returns
        -------
        result : Dask Array
        """

        darray, chunks_init = self.create_array(darray, preview=preview)
        inst_freq = self.instantaneous_frequency(darray, sample_rate)
        inst_band = self.instantaneous_bandwidth(darray)
        result = da.hypot(inst_freq, inst_band)

        return (result)
Пример #2
0
def CartesianToEquatorial(pos, observer=[0,0,0]):
    """
    Convert Cartesian position coordinates to equatorial right ascension
    and declination, using the specified observer location.

    .. note::
        RA and DEC will be returned in degrees, with RA in the range [0,360]
        and DEC in the range [-90, 90].

    Parameters
    ----------
    pos : array_like
        a N x 3 array holding the Cartesian position coordinates
    observer : array_like
        a length 3 array holding the observer location

    Returns
    -------
    ra, dec : array_like
        the right ascension and declination coordinates, in degrees. RA
        will be in the range [0,360] and DEC in the range [-90, 90]
    """
    # recenter based on observer
    pos = pos - observer

    s = da.hypot(pos[:,0], pos[:,1])
    lon = da.arctan2(pos[:,1], pos[:,0])
    lat = da.arctan2(pos[:,2], s)

    # convert to degrees
    lon = da.rad2deg(lon)
    lat = da.rad2deg(lat)

    # wrap lon to [0,360]
    lon = da.mod(lon-360., 360.)

    return lon, lat
Пример #3
0
def test_arithmetic():
    x = np.arange(5).astype('f4') + 2
    y = np.arange(5).astype('i8') + 2
    z = np.arange(5).astype('i4') + 2
    a = da.from_array(x, chunks=(2,))
    b = da.from_array(y, chunks=(2,))
    c = da.from_array(z, chunks=(2,))
    assert eq(a + b, x + y)
    assert eq(a * b, x * y)
    assert eq(a - b, x - y)
    assert eq(a / b, x / y)
    assert eq(b & b, y & y)
    assert eq(b | b, y | y)
    assert eq(b ^ b, y ^ y)
    assert eq(a // b, x // y)
    assert eq(a ** b, x ** y)
    assert eq(a % b, x % y)
    assert eq(a > b, x > y)
    assert eq(a < b, x < y)
    assert eq(a >= b, x >= y)
    assert eq(a <= b, x <= y)
    assert eq(a == b, x == y)
    assert eq(a != b, x != y)

    assert eq(a + 2, x + 2)
    assert eq(a * 2, x * 2)
    assert eq(a - 2, x - 2)
    assert eq(a / 2, x / 2)
    assert eq(b & True, y & True)
    assert eq(b | True, y | True)
    assert eq(b ^ True, y ^ True)
    assert eq(a // 2, x // 2)
    assert eq(a ** 2, x ** 2)
    assert eq(a % 2, x % 2)
    assert eq(a > 2, x > 2)
    assert eq(a < 2, x < 2)
    assert eq(a >= 2, x >= 2)
    assert eq(a <= 2, x <= 2)
    assert eq(a == 2, x == 2)
    assert eq(a != 2, x != 2)

    assert eq(2 + b, 2 + y)
    assert eq(2 * b, 2 * y)
    assert eq(2 - b, 2 - y)
    assert eq(2 / b, 2 / y)
    assert eq(True & b, True & y)
    assert eq(True | b, True | y)
    assert eq(True ^ b, True ^ y)
    assert eq(2 // b, 2 // y)
    assert eq(2 ** b, 2 ** y)
    assert eq(2 % b, 2 % y)
    assert eq(2 > b, 2 > y)
    assert eq(2 < b, 2 < y)
    assert eq(2 >= b, 2 >= y)
    assert eq(2 <= b, 2 <= y)
    assert eq(2 == b, 2 == y)
    assert eq(2 != b, 2 != y)

    assert eq(-a, -x)
    assert eq(abs(a), abs(x))
    assert eq(~(a == b), ~(x == y))
    assert eq(~(a == b), ~(x == y))

    assert eq(da.logaddexp(a, b), np.logaddexp(x, y))
    assert eq(da.logaddexp2(a, b), np.logaddexp2(x, y))
    assert eq(da.exp(b), np.exp(y))
    assert eq(da.log(a), np.log(x))
    assert eq(da.log10(a), np.log10(x))
    assert eq(da.log1p(a), np.log1p(x))
    assert eq(da.expm1(b), np.expm1(y))
    assert eq(da.sqrt(a), np.sqrt(x))
    assert eq(da.square(a), np.square(x))

    assert eq(da.sin(a), np.sin(x))
    assert eq(da.cos(b), np.cos(y))
    assert eq(da.tan(a), np.tan(x))
    assert eq(da.arcsin(b/10), np.arcsin(y/10))
    assert eq(da.arccos(b/10), np.arccos(y/10))
    assert eq(da.arctan(b/10), np.arctan(y/10))
    assert eq(da.arctan2(b*10, a), np.arctan2(y*10, x))
    assert eq(da.hypot(b, a), np.hypot(y, x))
    assert eq(da.sinh(a), np.sinh(x))
    assert eq(da.cosh(b), np.cosh(y))
    assert eq(da.tanh(a), np.tanh(x))
    assert eq(da.arcsinh(b*10), np.arcsinh(y*10))
    assert eq(da.arccosh(b*10), np.arccosh(y*10))
    assert eq(da.arctanh(b/10), np.arctanh(y/10))
    assert eq(da.deg2rad(a), np.deg2rad(x))
    assert eq(da.rad2deg(a), np.rad2deg(x))

    assert eq(da.logical_and(a < 1, b < 4), np.logical_and(x < 1, y < 4))
    assert eq(da.logical_or(a < 1, b < 4), np.logical_or(x < 1, y < 4))
    assert eq(da.logical_xor(a < 1, b < 4), np.logical_xor(x < 1, y < 4))
    assert eq(da.logical_not(a < 1), np.logical_not(x < 1))
    assert eq(da.maximum(a, 5 - a), np.maximum(a, 5 - a))
    assert eq(da.minimum(a, 5 - a), np.minimum(a, 5 - a))
    assert eq(da.fmax(a, 5 - a), np.fmax(a, 5 - a))
    assert eq(da.fmin(a, 5 - a), np.fmin(a, 5 - a))

    assert eq(da.isreal(a + 1j * b), np.isreal(x + 1j * y))
    assert eq(da.iscomplex(a + 1j * b), np.iscomplex(x + 1j * y))
    assert eq(da.isfinite(a), np.isfinite(x))
    assert eq(da.isinf(a), np.isinf(x))
    assert eq(da.isnan(a), np.isnan(x))
    assert eq(da.signbit(a - 3), np.signbit(x - 3))
    assert eq(da.copysign(a - 3, b), np.copysign(x - 3, y))
    assert eq(da.nextafter(a - 3, b), np.nextafter(x - 3, y))
    assert eq(da.ldexp(c, c), np.ldexp(z, z))
    assert eq(da.fmod(a * 12, b), np.fmod(x * 12, y))
    assert eq(da.floor(a * 0.5), np.floor(x * 0.5))
    assert eq(da.ceil(a), np.ceil(x))
    assert eq(da.trunc(a / 2), np.trunc(x / 2))

    assert eq(da.degrees(b), np.degrees(y))
    assert eq(da.radians(a), np.radians(x))

    assert eq(da.rint(a + 0.3), np.rint(x + 0.3))
    assert eq(da.fix(a - 2.5), np.fix(x - 2.5))

    assert eq(da.angle(a + 1j), np.angle(x + 1j))
    assert eq(da.real(a + 1j), np.real(x + 1j))
    assert eq((a + 1j).real, np.real(x + 1j))
    assert eq(da.imag(a + 1j), np.imag(x + 1j))
    assert eq((a + 1j).imag, np.imag(x + 1j))
    assert eq(da.conj(a + 1j * b), np.conj(x + 1j * y))
    assert eq((a + 1j * b).conj(), (x + 1j * y).conj())

    assert eq(da.clip(b, 1, 4), np.clip(y, 1, 4))
    assert eq(da.fabs(b), np.fabs(y))
    assert eq(da.sign(b - 2), np.sign(y - 2))

    l1, l2 = da.frexp(a)
    r1, r2 = np.frexp(x)
    assert eq(l1, r1)
    assert eq(l2, r2)

    l1, l2 = da.modf(a)
    r1, r2 = np.modf(x)
    assert eq(l1, r1)
    assert eq(l2, r2)

    assert eq(da.around(a, -1), np.around(x, -1))
Пример #4
0
def test_arithmetic():
    x = np.arange(5).astype('f4') + 2
    y = np.arange(5).astype('i8') + 2
    z = np.arange(5).astype('i4') + 2
    a = da.from_array(x, chunks=(2, ))
    b = da.from_array(y, chunks=(2, ))
    c = da.from_array(z, chunks=(2, ))
    assert eq(a + b, x + y)
    assert eq(a * b, x * y)
    assert eq(a - b, x - y)
    assert eq(a / b, x / y)
    assert eq(b & b, y & y)
    assert eq(b | b, y | y)
    assert eq(b ^ b, y ^ y)
    assert eq(a // b, x // y)
    assert eq(a**b, x**y)
    assert eq(a % b, x % y)
    assert eq(a > b, x > y)
    assert eq(a < b, x < y)
    assert eq(a >= b, x >= y)
    assert eq(a <= b, x <= y)
    assert eq(a == b, x == y)
    assert eq(a != b, x != y)

    assert eq(a + 2, x + 2)
    assert eq(a * 2, x * 2)
    assert eq(a - 2, x - 2)
    assert eq(a / 2, x / 2)
    assert eq(b & True, y & True)
    assert eq(b | True, y | True)
    assert eq(b ^ True, y ^ True)
    assert eq(a // 2, x // 2)
    assert eq(a**2, x**2)
    assert eq(a % 2, x % 2)
    assert eq(a > 2, x > 2)
    assert eq(a < 2, x < 2)
    assert eq(a >= 2, x >= 2)
    assert eq(a <= 2, x <= 2)
    assert eq(a == 2, x == 2)
    assert eq(a != 2, x != 2)

    assert eq(2 + b, 2 + y)
    assert eq(2 * b, 2 * y)
    assert eq(2 - b, 2 - y)
    assert eq(2 / b, 2 / y)
    assert eq(True & b, True & y)
    assert eq(True | b, True | y)
    assert eq(True ^ b, True ^ y)
    assert eq(2 // b, 2 // y)
    assert eq(2**b, 2**y)
    assert eq(2 % b, 2 % y)
    assert eq(2 > b, 2 > y)
    assert eq(2 < b, 2 < y)
    assert eq(2 >= b, 2 >= y)
    assert eq(2 <= b, 2 <= y)
    assert eq(2 == b, 2 == y)
    assert eq(2 != b, 2 != y)

    assert eq(-a, -x)
    assert eq(abs(a), abs(x))
    assert eq(~(a == b), ~(x == y))
    assert eq(~(a == b), ~(x == y))

    assert eq(da.logaddexp(a, b), np.logaddexp(x, y))
    assert eq(da.logaddexp2(a, b), np.logaddexp2(x, y))
    assert eq(da.exp(b), np.exp(y))
    assert eq(da.log(a), np.log(x))
    assert eq(da.log10(a), np.log10(x))
    assert eq(da.log1p(a), np.log1p(x))
    assert eq(da.expm1(b), np.expm1(y))
    assert eq(da.sqrt(a), np.sqrt(x))
    assert eq(da.square(a), np.square(x))

    assert eq(da.sin(a), np.sin(x))
    assert eq(da.cos(b), np.cos(y))
    assert eq(da.tan(a), np.tan(x))
    assert eq(da.arcsin(b / 10), np.arcsin(y / 10))
    assert eq(da.arccos(b / 10), np.arccos(y / 10))
    assert eq(da.arctan(b / 10), np.arctan(y / 10))
    assert eq(da.arctan2(b * 10, a), np.arctan2(y * 10, x))
    assert eq(da.hypot(b, a), np.hypot(y, x))
    assert eq(da.sinh(a), np.sinh(x))
    assert eq(da.cosh(b), np.cosh(y))
    assert eq(da.tanh(a), np.tanh(x))
    assert eq(da.arcsinh(b * 10), np.arcsinh(y * 10))
    assert eq(da.arccosh(b * 10), np.arccosh(y * 10))
    assert eq(da.arctanh(b / 10), np.arctanh(y / 10))
    assert eq(da.deg2rad(a), np.deg2rad(x))
    assert eq(da.rad2deg(a), np.rad2deg(x))

    assert eq(da.logical_and(a < 1, b < 4), np.logical_and(x < 1, y < 4))
    assert eq(da.logical_or(a < 1, b < 4), np.logical_or(x < 1, y < 4))
    assert eq(da.logical_xor(a < 1, b < 4), np.logical_xor(x < 1, y < 4))
    assert eq(da.logical_not(a < 1), np.logical_not(x < 1))
    assert eq(da.maximum(a, 5 - a), np.maximum(a, 5 - a))
    assert eq(da.minimum(a, 5 - a), np.minimum(a, 5 - a))
    assert eq(da.fmax(a, 5 - a), np.fmax(a, 5 - a))
    assert eq(da.fmin(a, 5 - a), np.fmin(a, 5 - a))

    assert eq(da.isreal(a + 1j * b), np.isreal(x + 1j * y))
    assert eq(da.iscomplex(a + 1j * b), np.iscomplex(x + 1j * y))
    assert eq(da.isfinite(a), np.isfinite(x))
    assert eq(da.isinf(a), np.isinf(x))
    assert eq(da.isnan(a), np.isnan(x))
    assert eq(da.signbit(a - 3), np.signbit(x - 3))
    assert eq(da.copysign(a - 3, b), np.copysign(x - 3, y))
    assert eq(da.nextafter(a - 3, b), np.nextafter(x - 3, y))
    assert eq(da.ldexp(c, c), np.ldexp(z, z))
    assert eq(da.fmod(a * 12, b), np.fmod(x * 12, y))
    assert eq(da.floor(a * 0.5), np.floor(x * 0.5))
    assert eq(da.ceil(a), np.ceil(x))
    assert eq(da.trunc(a / 2), np.trunc(x / 2))

    assert eq(da.degrees(b), np.degrees(y))
    assert eq(da.radians(a), np.radians(x))

    assert eq(da.rint(a + 0.3), np.rint(x + 0.3))
    assert eq(da.fix(a - 2.5), np.fix(x - 2.5))

    assert eq(da.angle(a + 1j), np.angle(x + 1j))
    assert eq(da.real(a + 1j), np.real(x + 1j))
    assert eq((a + 1j).real, np.real(x + 1j))
    assert eq(da.imag(a + 1j), np.imag(x + 1j))
    assert eq((a + 1j).imag, np.imag(x + 1j))
    assert eq(da.conj(a + 1j * b), np.conj(x + 1j * y))
    assert eq((a + 1j * b).conj(), (x + 1j * y).conj())

    assert eq(da.clip(b, 1, 4), np.clip(y, 1, 4))
    assert eq(da.fabs(b), np.fabs(y))
    assert eq(da.sign(b - 2), np.sign(y - 2))

    l1, l2 = da.frexp(a)
    r1, r2 = np.frexp(x)
    assert eq(l1, r1)
    assert eq(l2, r2)

    l1, l2 = da.modf(a)
    r1, r2 = np.modf(x)
    assert eq(l1, r1)
    assert eq(l2, r2)

    assert eq(da.around(a, -1), np.around(x, -1))
Пример #5
0
def CartesianToEquatorial(pos, observer=[0,0,0], frame='icrs'):
    """
    Convert Cartesian position coordinates to equatorial right ascension
    and declination, using the specified observer location.

    .. note::
        RA and DEC will be returned in degrees, with RA in the range [0,360]
        and DEC in the range [-90, 90].

    Parameters
    ----------
    pos : array_like
        a N x 3 array holding the Cartesian position coordinates
    observer : array_like
        a length 3 array holding the observer location
    frame : string
        A string, 'icrs' or 'galactic'. The frame of the input position.
        Use 'icrs' if the cartesian position is already in Equatorial.

    Returns
    -------
    ra, dec : array_like
        the right ascension and declination coordinates, in degrees. RA
        will be in the range [0,360] and DEC in the range [-90, 90]
    """

    # split x, y, z to signify that we do not need to have pos
    # as a full chunk in the last dimension.
    # this is useful when we use apply_gufunc.

    x, y, z = [pos[..., i] - observer[i] for i in range(3)]

    if frame == 'icrs':
        # FIXME: Convert these to a gufunc that uses astropy?
        # might be a step backward.

        # from equatorial to equatorial
        s = da.hypot(x, y)
        lon = da.arctan2(y, x)
        lat = da.arctan2(z, s)

        # convert to degrees
        lon = da.rad2deg(lon)
        lat = da.rad2deg(lat)
        # wrap lon to [0,360]
        lon = da.mod(lon-360., 360.)
        ra, dec = lon, lat
    else:
        from astropy.coordinates import SkyCoord

        def cart_to_eq(x, y, z):
            try:
                sc = SkyCoord(x, y, z, representation_type='cartesian', frame=frame)
                scg = sc.transform_to(frame='icrs')
                scg.representation_type = 'unitspherical'
            except:
                sc = SkyCoord(x, y, z, representation='cartesian', frame=frame)
                scg = sc.transform_to(frame='icrs')
                scg.representation = 'unitspherical'

            ra, dec = scg.ra.value, scg.dec.value

            return ra, dec

        dtype = pos.dtype
        ra, dec = da.apply_gufunc(cart_to_eq, '(),(),()->(),()', x, y, z, output_dtypes=[dtype, dtype])

    return da.stack((ra, dec), axis=0)
Пример #6
0
def CartesianToEquatorial(pos, observer=[0,0,0], frame='icrs'):
    """
    Convert Cartesian position coordinates to equatorial right ascension
    and declination, using the specified observer location.

    .. note::
        RA and DEC will be returned in degrees, with RA in the range [0,360]
        and DEC in the range [-90, 90].

    Parameters
    ----------
    pos : array_like
        a N x 3 array holding the Cartesian position coordinates
    observer : array_like
        a length 3 array holding the observer location
    frame : string
        A string, 'icrs' or 'galactic'. The frame of the input position.
        Use 'icrs' if the cartesian position is already in Equatorial.

    Returns
    -------
    ra, dec : array_like
        the right ascension and declination coordinates, in degrees. RA
        will be in the range [0,360] and DEC in the range [-90, 90]
    """

    # split x, y, z to signify that we do not need to have pos
    # as a full chunk in the last dimension.
    # this is useful when we use apply_gufunc.

    x, y, z = [pos[..., i] - observer[i] for i in range(3)]

    if frame == 'icrs':
        # FIXME: Convert these to a gufunc that uses astropy?
        # might be a step backward.

        # from equatorial to equatorial
        s = da.hypot(x, y)
        lon = da.arctan2(y, x)
        lat = da.arctan2(z, s)

        # convert to degrees
        lon = da.rad2deg(lon)
        lat = da.rad2deg(lat)
        # wrap lon to [0,360]
        lon = da.mod(lon-360., 360.)
        ra, dec = lon, lat
    else:
        from astropy.coordinates import SkyCoord

        def cart_to_eq(x, y, z):
            try:
                sc = SkyCoord(x, y, z, representation_type='cartesian', frame=frame)
                scg = sc.transform_to(frame='icrs')
                scg.representation_type = 'unitspherical'
            except:
                sc = SkyCoord(x, y, z, representation='cartesian', frame=frame)
                scg = sc.transform_to(frame='icrs')
                scg.representation = 'unitspherical'

            ra, dec = scg.ra.value, scg.dec.value

            return ra, dec

        dtype = pos.dtype
        ra, dec = da.apply_gufunc(cart_to_eq, '(),(),()->(),()', x, y, z, output_dtypes=[dtype, dtype])

    return da.stack((ra, dec), axis=0)