Exemplo n.º 1
0
 def distanceToSun(self):
     """
     Find the distance between the Sun and the target pointings
     """
     lofar = Observer()
     lofar.lon = '6.869882'
     lofar.lat = '52.915129'
     lofar.elevation = 15.*u.m
     lofar.date = self.startTime
     
     # Create Sun object
     sun = Sun()
     sun.compute(lofar)
     
     # Create the target object
     target = FixedBody()
     target._epoch = '2000'
     target._ra = self.coordPoint1.ra.radian
     target._dec = self.coordPoint1.dec.radian
     target.compute(lofar)
     print 'INFO: Sun is {:0.2f} degrees away from {}'.format(\
           float(separation(target, sun))*180./np.pi, self.namePoint1)
     target._ra = self.coordPoint2.ra.radian
     target._dec = self.coordPoint2.dec.radian
     target.compute(lofar)
     print 'INFO: Sun is {:0.2f} degrees away from {}'.format(\
           float(separation(target, sun))*180./np.pi, self.namePoint2)
Exemplo n.º 2
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def get_elevation_solar(obs_date, offender):
    """For a given observation date and bright solar system object, return its
       elevation over the course of that day.
       Input parameters:
       * obs_date: Observation date in datetime.datetime format
       * offender: Name of the solar system object. Allowed names are
                   Sun, Moon, and Jupiter.
       Returns:
       List of elevations in degrees. If offender is invalid, return None.
    """
    # Create the telescope object
    lofar = get_dutch_lofar_object()
    if offender == 'Sun':
        obj = Sun()
    elif offender == 'Moon':
        obj = Moon()
    elif offender == 'Jupiter':
        obj = Jupiter()
    else:
        return None

    yaxis = []
    for time in obs_date:
        lofar.date = time
        obj.compute(lofar)
        elevation = float(obj.alt)*180./np.pi
        if elevation < 0:
            elevation = np.nan
        yaxis.append(elevation)

    return yaxis
Exemplo n.º 3
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    def _findDistanceToSun(self, coord):
        """
        Print the distance between the specified pointing center and the Sun.
        """
        # Find the coordinates of the Sun at the start of the observing run
        sun = Sun()
        sun.compute(self.startTime)
        coordSun = SkyCoord('{} {}'.format(sun.ra, sun.dec),
                            unit=(u.hourangle, u.deg))
        coordTarget = SkyCoord('{} {}'.format(coord.split(';')[0], \
                              coord.split(';')[1]), \
                              unit=(u.hourangle, u.deg))

        # Find the separation between the Sun and the target
        return coordSun.separation(coordTarget).deg
Exemplo n.º 4
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    def from_observer(obs=None, date=None, yaw=0., theta_t=0., phi_t=0.):
        """
        Creates sky using an Ephem observer (Requires Ephem library)
        :param obs: the observer (location on Earth)
        :param date: the date of the observation
        :param yaw: the heading orientation of the observer
        :param theta_t: the heading tilt (pitch)
        :param phi_t: the heading tilt (roll)
        :return:
        """
        from ephem import Sun
        from datetime import datetime
        from utils import get_seville_observer

        sun = Sun()
        if obs is None:
            obs = get_seville_observer()
            obs.date = datetime(2017, 6, 21, 10, 0, 0) if date is None else date
        sun.compute(obs)
        theta_s, phi_s = np.pi/2 - sun.alt, (sun.az - yaw + np.pi) % (2 * np.pi) - np.pi

        return Sky(theta_s=theta_s, phi_s=phi_s, theta_t=theta_t, phi_t=phi_t)
Exemplo n.º 5
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def get_distance_solar(target, obs_date, offender):
    """Compute the angular distance in degrees between the specified target and
       the offending radio source in the solar system on the specified observing
       date.
       Input parameters:
       * target   - Coordinate of the target as an Astropy SkyCoord object
       * obs_date  - Observing date in datetime.datetime format
       * offender - Name of the offending bright source. Allowed values are
                    Sun, Moon, Jupiter.
       Returns:
       For Moon, the minimum and maximum separation are returned. For others,
       distance,None is returned."""
    # Get a list of values along the time axis
    d = obs_date.split('-')
    start_time = datetime(int(d[0]), int(d[1]), int(d[2]), 0, 0, 0)
    end_time = start_time + timedelta(hours=24)
    taxis = []
    temp_time = start_time
    while temp_time < end_time:
        taxis.append(temp_time)
        temp_time += timedelta(hours=1)
    angsep = []
    if offender == 'Sun':
        obj = Sun()
    elif offender == 'Moon':
        obj = Moon()
    elif offender == 'Jupiter':
        obj = Jupiter()
    else: pass
    # Estimate the angular distance over the entire time axis
    for time in taxis:
        obj.compute(time)
        coord = SkyCoord('{} {}'.format(obj.ra, obj.dec), unit=(u.hourangle, u.deg))
        angsep.append(coord.separation(target).deg)
    # Return appropriate result
    if offender == 'Moon':
        return np.min(angsep), np.max(angsep)
    else:
        return np.mean(angsep), None
Exemplo n.º 6
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def plot_ephemeris(obs, dt=10):
    sun = Sun()
    delta = timedelta(minutes=dt)

    azi, azi_diff, ele = [], [], []

    for month in xrange(12):
        obs.date = datetime(year=2018, month=month + 1, day=13)

        cur = obs.next_rising(sun).datetime() + delta
        end = obs.next_setting(sun).datetime()
        if cur > end:
            cur = obs.previous_rising(sun).datetime() + delta

        while cur <= end:
            obs.date = cur
            sun.compute(obs)
            a, e = sun.az, np.pi / 2 - sun.alt
            if len(azi) > 0:
                d = 60. / dt * np.absolute((a - azi[-1] + np.pi) % (2 * np.pi) - np.pi)
                if d > np.pi / 2:
                    azi_diff.append(0.)
                else:
                    azi_diff.append(d)
            else:
                azi_diff.append(0.)
            azi.append(a % (2 * np.pi))
            ele.append(e)
            # increase the current time
            cur = cur + delta

    ele = np.rad2deg(ele)
    azi = np.rad2deg(azi)
    azi_diff = np.rad2deg(azi_diff)
    azi = azi[ele < 90]
    azi_diff = azi_diff[ele < 90]
    ele = ele[ele < 90]

    ele_nonl = np.exp(.1 * (54 - ele))

    x = np.array([9 + np.exp(.1 * (54 - ele)), np.ones_like(azi_diff)]).T

    # w = np.linalg.pinv(x).dot(azi_diff)
    w = np.array([1., 0.])

    y = x.dot(w)
    error = np.absolute(y - azi_diff)
    print "Error: %.4f +/- %.4f" % (error.mean(), error.std() / np.sqrt(len(error))),
    print "| N = %d" % len(error)

    plt.figure(figsize=(10, 10))

    plt.subplot(221)
    plt.scatter(azi, ele, c=azi_diff, cmap='Reds', marker='.')
    plt.ylabel(r'$\theta_s (\circ)$')
    plt.xlim([0, 360])
    plt.ylim([85, 0])
    plt.xticks([0, 45, 90, 135, 180, 225, 270, 315, 360], [""] * 9)
    plt.yticks([0, 15, 30, 45, 60, 75])

    plt.subplot(222)
    plt.scatter(azi_diff, ele, c=azi, cmap='coolwarm', marker='.')
    xx = np.linspace(0, 90, 100, endpoint=True)
    yy = 9 + np.exp(.1 * (54 - xx))
    plt.plot(yy, xx, 'k-')
    plt.ylim([85, 0])
    plt.xlim([7, 60])
    plt.xticks([10, 20, 30, 40, 50, 60], [""] * 6)
    plt.yticks([0, 15, 30, 45, 60, 75], [""] * 6)

    plt.subplot(223)
    plt.scatter(azi, x[:, 0], c=azi_diff, cmap='Reds', marker='.')
    plt.xlabel(r'$\phi_s (\circ)$')
    plt.ylabel(r'$\Delta\phi_s (\circ/h)$ -- prediction')
    plt.xlim([0, 360])
    plt.ylim([7, 65])
    plt.xticks([0, 45, 90, 135, 180, 225, 270, 315, 360])
    plt.yticks([10, 20, 30, 40, 50, 60])

    plt.subplot(224)
    plt.scatter(azi_diff, x[:, 0], c=azi, cmap='coolwarm', marker='.')
    plt.plot([w[0] * 7 + w[1], w[0] * 65 + w[1]], [7, 65], 'k-')
    plt.xlabel(r'$\Delta\phi_s (\circ/h)$ -- true')
    plt.xlim([7, 60])
    plt.xticks([10, 20, 30, 40, 50, 60])
    plt.ylim([7, 65])
    plt.yticks([10, 20, 30, 40, 50, 60], [""] * 6)

    return plt
Exemplo n.º 7
0
#data.astype({'time':'int32'}).dtypes

# print data.dtypes
# print int(data['time'][0])
# print(data['time'])

# plt.figure(figsize=(14,10))
# #plt.scatter(data['t2'],data['mag'])
# n, bins, patches = plt.hist(data['t2'], bins=96)
# plt.xlim(-12,12)
# plt.show()

dt = '2016/5/27 00:00'
sun = Sun()
sun.compute(dt)

elginfield = Observer()
elginfield.lat = 43.19237
elginfield.lon = -81.31799
elginfield.date = dt
ra, dec = elginfield.radec_of('0', '-90')

print('RA_sun:',sun.ra)
print('Elgin nadir', ra)
print('Solar time:', hours((ra-sun.ra)%(2*pi)), 'hours')

fig, ax = plt.subplots(figsize=(14,10))
n, bins, patches = ax.hist(data['t2'], bins=192, rwidth=0.9, edgecolor='black')
ax.axvline(0, color='red')
Exemplo n.º 8
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        plt.show()

    elif mode is "res2azi":
        azi, azi_diff, ele, res = [], [], [], []

        for month in xrange(12):
            obs.date = datetime(year=2018, month=month + 1, day=13)

            cur = obs.next_rising(sun).datetime() + delta
            end = obs.next_setting(sun).datetime()
            if cur > end:
                cur = obs.previous_rising(sun).datetime() + delta

            while cur <= end:
                obs.date = cur
                sun.compute(obs)
                a, e = sun.az, np.pi / 2 - sun.alt
                if len(azi) > 0:
                    d = 60. / dt * np.absolute((a - azi[-1] + np.pi) %
                                               (2 * np.pi) - np.pi)
                    if d > np.pi / 2:
                        azi_diff.append(0.)
                    else:
                        azi_diff.append(d)
                else:
                    azi_diff.append(0.)

                d_err, d_eff, tau, _, _ = evaluate(sun_azi=a,
                                                   sun_ele=e,
                                                   tilting=False,
                                                   noise=0.)