def get_moon(times):
t = Table()
earth = get_body(times, 'earth')
moon = get_body(times, 'moon')
em_x = moon['x']-earth['x']
em_y = moon['y']-earth['y']
em_z = moon['z']-earth['z']
em_d = np.sqrt(em_x**2 + em_y**2 + em_z**2)
em_vx = moon['vx']-earth['vx']
em_vy = moon['vy']-earth['vy']
em_vz = moon['vz']-earth['vz']
em_v = np.sqrt(em_vx**2 + em_vy**2 + em_vz**2)
t.add_column(moon['utc'])
t.add_column(moon['jd'])
t.add_column(em_x)
t.add_column(em_y)
t.add_column(em_z)
t.add_column(em_d, name='d')
t.add_column(em_vx)
t.add_column(em_vy)
t.add_column(em_vz)
t.add_column(em_v, name='v')
t.add_column(np.arcsin(em_z/em_d), name='dec')
t.add_column(np.arctan2(em_y, em_x), name='RA')
return t
def termtime(daytime,daytime2,code,unit='hour'):
if unit=='hour':
times=daytime+np.linspace(0.,1.,25)*(daytime2-daytime)
elif unit=='minute':
times=daytime+np.linspace(0.,1.,61)*(daytime2-daytime)
else:
times=daytime+np.linspace(0.,1.,61)*(daytime2-daytime)
gmttimes=times-eighthours
if type=='jieqi':
diflongitudes=get_body('sun', gmttimes, ephemeris='jpl').\
transform_to(GeocentricTrueEcliptic(equinox=gmttimes)).lon.deg
else:
sunlongitudes=get_body('sun', gmttimes, ephemeris='jpl').\
transform_to(GeocentricTrueEcliptic(equinox=gmttimes)).lon.deg
moonlongitudes=get_body('moon', gmttimes, ephemeris='jpl').\
transform_to(GeocentricTrueEcliptic(equinox=gmttimes)).lon.deg
diflongitudes=(moonlongitudes-sunlongitudes)%360
difcode=diflongitudes // sec
difcode=[int(difcode[i]) for i in range(len(difcode))]
for i in range(len(difcode)-1):
if difcode[i+1]!=code:
if unit=='hour':
return termtime(times[i],times[i+1],code,"minute")
else:
if unit=='minute':
return termtime(times[i],times[i+1],code,"second")
else:
return ((code+1) % (360//sec),(times[i]+0.5*(times[i+1]-times[i])).value)
return (-1,"")
def gcrs_to_geosolarecliptic(gcrs_coo, to_frame):
if not to_frame.obstime.isscalar:
raise ValueError(
"To perform this transformation the obstime Attribute must be a scalar."
)
_earth_orbit_perpen_point_gcrs = UnitSphericalRepresentation(
lon=0 * u.deg,
lat=(90 * u.deg - _obliquity_rotation_value(to_frame.obstime)))
_earth_detilt_matrix = _make_rotation_matrix_from_reprs(
_earth_orbit_perpen_point_gcrs, CartesianRepresentation(0, 0, 1))
sun_pos_gcrs = get_body("sun", to_frame.obstime).cartesian
earth_pos_gcrs = get_body("earth", to_frame.obstime).cartesian
sun_earth = sun_pos_gcrs - earth_pos_gcrs
sun_earth_detilt = sun_earth.transform(_earth_detilt_matrix)
# Earth-Sun Line in Geocentric Solar Ecliptic Frame
x_axis = CartesianRepresentation(1, 0, 0)
rot_matrix = _make_rotation_matrix_from_reprs(sun_earth_detilt, x_axis)
return matrix_product(rot_matrix, _earth_detilt_matrix)
def __init__(self, observer, body_name, t):
"""Calculate properties of the geometry of the observer, the body and
the Sun."""
self.observer = observer
self.body_name = body_name
self.t = t
# Position of the Sun
self.sun = get_body('sun', self.t)
# Position of the body
self.body = get_body(body_name, self.t)
# The location of the observer in HPC co-ordinates.
self.observer_hpc = coordinates.Helioprojective(
observer=observer, obstime=observer.obstime)
# The location of the body as seen by the observer, following the
# SunPy example
self.body_hpc = self.body.transform_to(
frames.Helioprojective).transform_to(self.observer_hpc)
# The body and the observer in HCC for ease of distance calculation.
self.body_hcc = self.body.transform_to(frames.Heliocentric)
self.observer_hcc = self.observer.transform_to(frames.Heliocentric)
def gcrs_to_geosolarecliptic(gcrs_coo, to_frame):
if not to_frame.obstime.isscalar:
raise ValueError(
"To perform this transformation the obstime Attribute must be a scalar."
)
_earth_orbit_perpen_point_gcrs = UnitSphericalRepresentation(
lon=0 * u.deg, lat=(90 * u.deg - _obliquity_rotation_value(to_frame.obstime))
)
_earth_detilt_matrix = _make_rotation_matrix_from_reprs(
_earth_orbit_perpen_point_gcrs, CartesianRepresentation(0, 0, 1)
)
sun_pos_gcrs = get_body("sun", to_frame.obstime).cartesian
earth_pos_gcrs = get_body("earth", to_frame.obstime).cartesian
sun_earth = sun_pos_gcrs - earth_pos_gcrs
sun_earth_detilt = sun_earth.transform(_earth_detilt_matrix)
# Earth-Sun Line in Geocentric Solar Ecliptic Frame
x_axis = CartesianRepresentation(1, 0, 0)
rot_matrix = _make_rotation_matrix_from_reprs(sun_earth_detilt, x_axis)
return matrix_product(rot_matrix, _earth_detilt_matrix)
def galactic(tstart=None, tend=None, tstep=None, time=None):
if time is not None and (tstart is not None or tend is not None
or tstep is not None):
raise AssertionError(
'Must enter one time, or a start time, end time, and time step')
elif time is not None:
with solar_system_ephemeris.set('jpl'):
jup_ephem = get_body('sun', time).galactic
elif time is None and (tstart is None or tend is None or tstep is None):
raise AssertionError('Must enter start time, end time, and time step')
elif time is None and (tstart is not None and tend is not None
and tstep is not None):
# tstart = tstart.mjd + (tstep/2) #use this line if you want times in the center of timeranges, dont use if you want coordinates at the time intervals themselves
tstart = tstart.mjd # use if you want coordinates at time intervals not at center of intervals
tend = tend.mjd
times = np.arange(tstart, tend, tstep, dtype=float)
times_list = Time(times, format='mjd').fits
times_list = Time(times_list, format='fits')
jup_ephem = list()
for date in times_list:
with solar_system_ephemeris.set('jpl'):
jup = get_body('sun', date).galactic
jup_ephem.append(jup)
return jup_ephem
def CCTerm(start,end,type):
eighthours=TimeDelta(8*3600,format='sec')
def termtime(daytime,daytime2,code,unit='hour'):
if unit=='hour':
times=daytime+np.linspace(0.,1.,25)*(daytime2-daytime)
elif unit=='minute':
times=daytime+np.linspace(0.,1.,61)*(daytime2-daytime)
else:
times=daytime+np.linspace(0.,1.,61)*(daytime2-daytime)
gmttimes=times-eighthours
if type=='jieqi':
diflongitudes=get_body('sun', gmttimes, ephemeris='jpl').\
transform_to(GeocentricTrueEcliptic(equinox=gmttimes)).lon.deg
else:
sunlongitudes=get_body('sun', gmttimes, ephemeris='jpl').\
transform_to(GeocentricTrueEcliptic(equinox=gmttimes)).lon.deg
moonlongitudes=get_body('moon', gmttimes, ephemeris='jpl').\
transform_to(GeocentricTrueEcliptic(equinox=gmttimes)).lon.deg
diflongitudes=(moonlongitudes-sunlongitudes)%360
difcode=diflongitudes // sec
difcode=[int(difcode[i]) for i in range(len(difcode))]
for i in range(len(difcode)-1):
if difcode[i+1]!=code:
if unit=='hour':
return termtime(times[i],times[i+1],code,"minute")
else:
if unit=='minute':
return termtime(times[i],times[i+1],code,"second")
else:
return ((code+1) % (360//sec),(times[i]+0.5*(times[i+1]-times[i])).value)
return (-1,"")
start=Time(Time(start,out_subfmt='date').iso)
end=Time(Time(end,out_subfmt='date').iso)
daycount=int(round((Time(end)-Time(start)).value))
# print(start,end,daycount)
# print(daycount)
times=Time(start)+np.linspace(0.,1.,daycount+1)*(end-start+TimeDelta(3,format='sec')) # 考量潤秒，故加上3秒
times=Time(Time(times,out_subfmt='date').iso)
gmttimes=times-TimeDelta(8*3600,format='sec')
if type=='jieqi':
diflongitudes= get_body('sun', gmttimes, ephemeris='jpl').\
transform_to(GeocentricTrueEcliptic(equinox=gmttimes)).lon.deg
sec=15
else:
sunlongitudes=get_body('sun', gmttimes, ephemeris='jpl').\
transform_to(GeocentricTrueEcliptic(equinox=gmttimes)).lon.deg
moonlongitudes=get_body('moon', gmttimes, ephemeris='jpl').\
transform_to(GeocentricTrueEcliptic(equinox=gmttimes)).lon.deg
diflongitudes=(moonlongitudes-sunlongitudes)%360
sec=90
res=[]
difcode=diflongitudes // sec
difcode=[int(difcode[i]) for i in range(len(difcode))]
for i in range(len(difcode)-1):
if difcode[i]!=difcode[i+1]:
res.append(termtime(times[i],times[i+1],difcode[i],'hour'))
return res
def get_position(body_name, time, observer=None):
"""
Get the position of one of the supported bodies. If an observer is given then light travel time from the body
to the observer is taken in to account.
Parameters
----------
body_name : `str`
The body whose position will be calculated
time : `~astropy.time.Time`
The time at which the body position is calculated. If the observer is not None, then the time is the
time at the observer.
observer : None, `~astropy.coordinate.SkyCoord`
If None, the position of the body is returned. If not none, the position of the body as seen from the
observer takes into account the light travel time from the body to the observer.
Returns
-------
`~astropy.coordinate.SkyCoord`
The position of the body. If the observer is not none, the position of the body as seen from the
observer takes into account the light travel time from the body to the observer.
"""
_body_name = body_name.lower()
if observer is None:
if _body_name in spice_spacecraft:
spice_target = get_spice_target(_body_name)
if _body_name == 'soho':
# Use the SPICE kernels if available, otherwise estimate the position of SOHO.
try:
coordinate = spice_target.coordinate(time)
except: # SpiceyError:
earth = get_body('earth', time).transform_to(frames.HeliographicStonyhurst)
coordinate = SkyCoord(lat=earth.lat, lon=earth.lon, radius=0.99 * earth.radius, obstime=time, frame=frames.HeliographicStonyhurst)
else:
coordinate = spice_target.coordinate(time)
elif _body_name in solar_system_objects:
coordinate = get_body(_body_name, time)
else:
raise ValueError('The body name is not recognized.')
else:
if _body_name in spice_spacecraft:
#log.warning('Light travel time corrected locations of spacecraft are not yet supported ({:s} seen from observer).'.format(body_name))
spice_target = get_spice_target(_body_name)
coordinate = spice_target.coordinate(time)
elif _body_name in solar_system_objects:
body_frame = get_body_heliographic_stonyhurst(_body_name, observer=observer, time=time)
# Explicitly convert the returned body frame in to a SkyCoord.
coordinate = SkyCoord(lat=body_frame.lat, lon=body_frame.lon, radius=body_frame.radius, obstime=time, frame=frames.HeliographicStonyhurst)
else:
raise ValueError('The body name is not recognized.')
return coordinate.transform_to(frames.HeliographicStonyhurst)
def get_observer(observer_name, t):
""" Get the location of the observer given the name of the observer."""
# TODO understand LASCO and helioviewer image processing steps
if observer_name.lower() == 'soho':
earth = get_body('earth', t).transform_to(frames.Heliocentric)
return SkyCoord(earth.x,
earth.y,
0.99 * earth.z,
frame=frames.Heliocentric,
obstime=t)
else:
return get_body(observer_name, t)
def find_parallax(self, date):
'''Find the maximum parallax of self.planet on the given date
from self.observer's location -- in other words, the difference
in Mars' position between the observer's position and an
observer at the same latitude but opposite longitude:
this tells you you how much difference you would see from
your position if Mars didn't move between your sunrise and sunset.
'''
# To calculate from a point on the equator, set lat to 0.
observer_loc = EarthLocation.from_geodetic(self.location.lon,
self.location.lat,
self.location.height)
# Specify the anti-point.
# This isn't really an antipode unless lat == 0.
antipode_loc = EarthLocation.from_geodetic(-observer.lon,
observer.lat,
observer.height)
# XXX Oops, astropy doesn't offer next_rising etc.
# so we'll need a function to find that before this
# function can be implemented since it only works
# when the planet is on the horizon so both the observer
# and the anti-observer can see it.
risetime = find_next_rising(planetname, date)
obs_planet = get_body(planetname, risetime, observer_loc)
ant_planet = get_body(planetname, risetime, antipode_loc)
# First, calculate it the straightforward way using the arctan:
print()
mars_dist_miles = mars.distance.km / 1.609344
print("Miles to Mars:", mars_dist_miles)
earth_mean_radius = 3958.8 # in miles
half_dist = earth_mean_radius * math.cos(observer_loc.lat)
print("Distance between observers:", 2. * half_dist)
par = 2. * math.atan(half_dist / mars_dist_miles) \
* 180. / math.pi * 3600.
print("Calculated parallax (arcsec):", par)
# See what astropy calculates as the difference between observations:
print()
print("parallax on %s: RA %f, dec %f" % (antipode.date,
obs_planet.ra - ant_planet.ra,
obs_planet.dec - ant_planet.dec))
total_par = (math.sqrt((obs_planet.ra.radians
- ant_planet.ra.radians)**2
+ (obs_planet.dec.radians
- ant_planet.dec.radians)**2)
* 180. * 3600. / math.pi)
print("Total parallax (sum of squares): %f arcseconds" % total_par)
print()
def test_regression_10291():
"""
According to https://eclipse.gsfc.nasa.gov/OH/transit12.html,
the minimum separation between Venus and the Sun during the 2012
transit is 554 arcseconds for an observer at the Geocenter.
If light deflection from the Sun is incorrectly applied, this increases
to 557 arcseconds.
"""
t = Time('2012-06-06 01:29:36')
sun = get_body('sun', t)
venus = get_body('venus', t)
assert_quantity_allclose(venus.separation(sun),
554.427*u.arcsecond, atol=0.001*u.arcsecond)
def find_parallax(self, date):
'''Find the maximum parallax of self.planet on the given date
from self.observer's location -- in other words, the difference
in Mars' position between the observer's position and an
observer at the same latitude but opposite longitude:
this tells you you how much difference you would see from
your position if Mars didn't move between your sunrise and sunset.
'''
# To calculate from a point on the equator, set lat to 0.
observer_loc = EarthLocation.from_geodetic(self.location.lon,
self.location.lat,
self.location.height)
# Specify the anti-point.
# This isn't really an antipode unless lat == 0.
antipode_loc = EarthLocation.from_geodetic(-observer.lon, observer.lat,
observer.height)
# XXX Oops, astropy doesn't offer next_rising etc.
# so we'll need a function to find that before this
# function can be implemented since it only works
# when the planet is on the horizon so both the observer
# and the anti-observer can see it.
risetime = find_next_rising(planetname, date)
obs_planet = get_body(planetname, risetime, observer_loc)
ant_planet = get_body(planetname, risetime, antipode_loc)
# First, calculate it the straightforward way using the arctan:
print()
mars_dist_miles = mars.distance.km / 1.609344
print("Miles to Mars:", mars_dist_miles)
earth_mean_radius = 3958.8 # in miles
half_dist = earth_mean_radius * math.cos(observer_loc.lat)
print("Distance between observers:", 2. * half_dist)
par = 2. * math.atan(half_dist / mars_dist_miles) \
* 180. / math.pi * 3600.
print("Calculated parallax (arcsec):", par)
# See what astropy calculates as the difference between observations:
print()
print("parallax on %s: RA %f, dec %f" %
(antipode.date, obs_planet.ra - ant_planet.ra,
obs_planet.dec - ant_planet.dec))
total_par = (
math.sqrt((obs_planet.ra.radians - ant_planet.ra.radians)**2 +
(obs_planet.dec.radians - ant_planet.dec.radians)**2) *
180. * 3600. / math.pi)
print("Total parallax (sum of squares): %f arcseconds" % total_par)
print()
def main():
# MeerKAT
obs_lat = -30.71323598930457
obs_lon = 21.443001467965008
loc = EarthLocation.from_geodetic(obs_lat,
obs_lon) #,obs_height,ellipsoid)
myms = sys.argv[1].rstrip('/')
maintab = table(myms, ack=False)
scans = list(numpy.unique(maintab.getcol('SCAN_NUMBER')))
ids, names, dirs = get_fields(myms)
print(myms + ' | ' + str(len(ids)) + ' fields | ' + str(len(scans)) +
' scans')
#header = 'Scan Field ID t[iso] t[s] t0[s] t1[s] int0 int1 Duration[m] N_int'
header = 't[iso] Scan Field Name SunRA[deg] SunDec[deg] SunRA[hms] SunDec[dms] SunSep[deg] MoonRA[deg] MoonDec[deg] MoonRA[hms] MoonDec[dms] MoonSep[deg]'
print('-' * len(header))
print(header)
print('-' * len(header))
for scan in scans:
subtab = maintab.query(query='SCAN_NUMBER==' + str(scan))
field = numpy.unique(subtab.getcol('FIELD_ID'))[0]
name, field_ra, field_dec = match_field(ids, names, dirs, field)
field_hms, field_dms = format_coords(field_ra, field_dec)
t_scan = numpy.mean(subtab.getcol('TIME'))
t = Time(t_scan / 86400.0, format='mjd')
with solar_system_ephemeris.set('builtin'):
sun = get_body('Sun', t, loc)
moon = get_body('Moon', t, loc)
sun_ra = sun.ra.value
sun_dec = sun.dec.value
moon_ra = moon.ra.value
moon_dec = moon.dec.value
sun_hms, sun_dms = format_coords(sun_ra, sun_dec)
moon_hms, moon_dms = format_coords(moon_ra, moon_dec)
delta_ra_sun = field_ra - sun_ra
delta_dec_sun = field_dec - sun_dec
delta_ra_moon = field_ra - moon_ra
delta_dec_moon = field_dec - moon_dec
sun_sep = calcsep(field_ra, field_dec, sun_ra, sun_dec)
moon_sep = calcsep(field_ra, field_dec, moon_ra, moon_dec)
# print field,name,sun_sep
print(
'%-28s %-5i %-5i %-12s %-12f %-12f %-16s %-16s %-12f %-12f %-12f %-16s %-16s %-12f'
% (t.iso, scan, field, name, sun_ra, sun_dec, sun_hms, sun_dms,
sun_sep, moon_ra, moon_dec, moon_hms, moon_dms, moon_sep))
print('-' * len(header))
def EarthRegion(times):
gmttimes=times-eighthours
sun=get_body('sun', gmttimes, ephemeris='jpl')
moon=get_body('moon', gmttimes, ephemeris='jpl')
earth=get_body('earth', gmttimes, ephemeris='jpl')
rs=const.R_sun.to('km').value
re=const.R_earth.to('km').value
ro=1737.1
sunpos=np.transpose(np.array([sun.cartesian.x.value,
sun.cartesian.y.value,sun.cartesian.z.value]))
moonpos=np.transpose(np.array([moon.cartesian.x.value,
moon.cartesian.y.value,moon.cartesian.z.value]))
earthpos=np.zeros((len(sunpos),3))
Ucenter,Pcenter,uarc,parc,SOdir=ShadowCone(sunpos,rs,moonpos,ro)
return(Region(sunpos,moonpos,earthpos,re,Ucenter,Pcenter,uarc,parc,SOdir))
def _select_solar_system(self, body: str) -> None:
"""Set RA/Dec for selected solar system body."""
from astropy.coordinates import solar_system_ephemeris, get_body
# nothing?
if body == "":
return
# clear simbad and JPL
self.textSimbadName.clear()
self.textJplHorizonsName.clear()
QtWidgets.QApplication.setOverrideCursor(QtCore.Qt.WaitCursor)
with solar_system_ephemeris.set("builtin"):
# get coordinates
body = get_body(body, Time.now(), self.observer.location)
QtWidgets.QApplication.restoreOverrideCursor()
# set them
self.textMoveRA.setText(
body.ra.to_string(unit=u.hour, sep=" ", precision=2))
self.textMoveDec.setText(body.dec.to_string(sep=" ", precision=2))
# update destination
self._calc_dest_equatorial(clear=False)
def solarbody_to_radec(
body,
location,
timestamp,
# default output in degrees
as_radians=False,
as_string=False):
"""Calculate equatorial (ra, dec) for solar body ephemerides
Parameters
----------
body: Name of solar body, Astropy convention
location: Telescope geocentric position, `Astropy.EarthLocaton`
timestamp: Unix timestamp
Returns
-------
tuple: (ra, dec) equatorial coordinates in degrees
"""
obs_time = timestamp2datetime(timestamp)
obs_time = obs_time.strftime("%Y-%m-%d %H:%M:%S")
obs_time = Time(obs_time)
with solar_system_ephemeris.set('builtin'):
solar_gcrs = get_body(body, obs_time, location)
return radec_from_pointing_object(solar_gcrs,
as_radians=as_radians,
as_string=as_string)
def planet(body, obs_loc, t=None):
if t is None:
t = datetime.utcnow()
body = body.lower()
if not body in solar_system_ephemeris.bodies:
raise Exception("Body not available!")
if type(obs_loc) == str and obs_loc in cities.keys():
lon, lat = cities[obs_loc][:-1]
elif isinstance(obs_loc, tuple):
if len(obs_loc) == 2:
lon, lat = obs_loc
else:
raise Exception("obs_loc should be in the format: (lon, lat)")
else:
raise Exception(
"obs_loc should be a city name or geographic coordiantes.")
loc = EarthLocation(lon=lon, lat=lat)
with solar_system_ephemeris.set('jpl'):
crd = get_body(body, Time(t), loc)
ra = crd.ra.value
dec = crd.dec.value
r = crd.distance.value
x, y, z = radec_to_cartesian(ra, dec, r)
alt, az = radec_to_altaz(lon=lon, lat=lat, ra=ra, dec=dec, t=t)
return (x, y, z), (ra, dec, r), (az, alt)
def get_planet_info():
planet_info = []
with solar_system_ephemeris.set('de432s'):
for planet_name in planets:
planet = get_body(planet_name, current_time, location)
planet_info.append({
"name":
planet_name,
"lightMinutes":
to_light_minutes(planet.distance),
"xyz":
get_xyz(planet)
})
sun = get_sun(current_time)
planet_info.append({
"name": "The Sun",
"lightMinutes": to_light_minutes(sun.distance),
"xyz": get_xyz(sun)
})
moon = get_moon(current_time)
planet_info.append({
"name": "The Moon",
"lightMinutes": to_light_minutes(moon.distance),
"xyz": get_xyz(moon)
})
return json.dumps(planet_info)
def plot_solarsystem(self, obs_time):
"""
Put planets of Solar System on a given Axes instance. Designation of the
each planet is its roman symbol
"""
# for Uranus must be another symbol, but at Unicode U+2645, which renders as ♅ (Wiki)
planets = OrderedDict([('Mercury', '☿'), ('Venus', '♀'), ('Mars', '♂'),
('Jupiter', '♃'), ('Saturn', '♄'),
('Uranus', '♅'), ('Neptune', '♆')])
planets_coords = [
get_body(planet, obs_time, location=self.obs_loc)
for planet in planets.keys()
]
for coords, (name, symbol) in zip(planets_coords, planets.items()):
planet = SkyCoord(coords.ra, coords.dec,
frame='gcrs').transform_to('icrs')
self.ax.plot([planet.ra.radian], [-planet.dec.value + 45],
label=name,
linestyle='',
color='violet',
marker='$' + symbol + '$',
markersize=markers['planet'])
print("planets are plotted")
def sun_position(obs_time):
location = EarthLocation(lon=115.2505 * u.deg,
lat=42.211833333 * u.deg,
height=1365.0 * u.m)
solar_system_ephemeris.set('de432s')
# GCRS
phasecentre = get_body('sun', obs_time, location, ephemeris='jpl')
print('SUN: RA:{} Dec:{}'.format(phasecentre.ra.value,
phasecentre.dec.value))
# convert phasecentre into ITRS coordinate
# ITRF - Alta
cAltAz = phasecentre.transform_to(
AltAz(obstime=obs_time, location=location))
newAltAzcoordiantes = SkyCoord(alt=cAltAz.alt,
az=cAltAz.az,
obstime=obs_time,
frame='altaz')
new_ra_dec = newAltAzcoordiantes.transform_to('icrs')
print(new_ra_dec)
c_ITRS = phasecentre.transform_to(ITRS(obstime=obs_time,
location=location))
local_ha = location.lon - c_ITRS.spherical.lon
local_ha.wrap_at(24 * u.hourangle, inplace=True)
print("UTC: {} Local Hour Angle: {}".format(obs_time,
local_ha.to('deg').value))
obs_time1 = Time(obs_time, scale='utc', location=location)
lst = obs_time1.sidereal_time('mean')
local_ha1 = lst.to('deg').value - phasecentre.ra.value
print("UTC: {} Local Hour Angle: {}".format(obs_time, local_ha1 * u.deg))
def moon_coordinates(time, cam):
"""This function searches for the moon position at a given time.
Parameters
-----------
time: 'astropy.time.core.Time'
Time the image was taken.
cam: 'str'
Camera
Returns
-------
moon_altitude: 'float'
Altitude of the moon at the time the image was taken [radians]
"""
observer = cam.location
object = 'moon'
with solar_system_ephemeris.set('builtin'):
coordinates = get_body(object, time, observer)
ra = coordinates.ra
dec = coordinates.dec
moon_position = SkyCoord(ra=ra, dec=dec, frame='icrs', unit='deg')
moon_position_altaz = moon_position.transform_to(
AltAz(obstime=time, location=observer))
moon_altitude = moon_position_altaz.alt.radian
print('time', type(time))
return moon_altitude
def Get_Sun_Coordinates(self, cg, ctime):
#
# Get_Sun_Coordinates
#
# This method obtains the Sun Coordinates both in (Ra,Dec) and (Alt, Az)
# While astropy may use very accurate calculations and corrections from
# IERS, for some reason it cannot download the data. So, I decided to
# work off-line with a lesser precision, although enoug for us.
#
#
# @guiguesp - 2020-04-05
# - 2020-05-30 : Now using sunpy 1.1
#_____________________________________________________________________________
t = Time(ctime)
with solar_system_ephemeris.set('builtin'):
sun_radec = get_body('sun', t, cg)
aa = AltAz(location=cg, obstime=t)
sun_altaz = sun_radec.transform_to(aa)
L0 = Sun_Coordinates.sun.L0(ctime)
B0 = Sun_Coordinates.sun.B0(ctime)
P = Sun_Coordinates.sun.P(ctime)
R_Sun = Sun_Coordinates.sun.angular_radius(ctime)
Carrington = Sun_Coordinates.sun.carrington_rotation_number(ctime)
return sun_radec, sun_altaz, L0, B0, P, R_Sun, Carrington
def rm_celestial_bodies(
self,
radius=10.0,
bodies=['moon', 'venus', 'mars', 'mercury', 'jupiter', 'saturn']):
"""Removes stars in the vicinity of bright celestial bodies from the
image.
Parameters
----------
radius : float
Radius in pixels
bodies : list(str)
List of names of celestial bodies. For allowed values see
astropy.coordinates.get_body.
"""
altaz_cs = AltAz(obstime=self.time, location=self.camera.location)
objects = [
get_body(p, self.time, self.camera.location).transform_to(altaz_cs)
for p in bodies
]
px_pos = np.array([
np.array(self.camera.__project_stars__(p.az, p.alt))
for p in objects
])
D = distance_matrix(self.star_pos, px_pos)
choice = np.all(D > radius, axis=1)
self.star_pos = self.star_pos[choice, :]
self.star_mag = self.star_mag[choice]
def stentime(plot=False):
gravity = EarthLocation(lat=31.78135 * u.deg,
lon=76.99313 * u.deg,
height=1000 * u.m)
time = Time(datetime(2020, 6, 8, 20, 18, 37, 274634))
deluni = np.linspace(0, 12, 1440)
delta = deluni * u.hour
utcoffset = 5.5 * u.hour
time = time - utcoffset
saturn = get_body('Saturn', time=time, location=gravity)
frame = AltAz(obstime=time + delta, location=gravity)
range1 = saturn.transform_to(frame)
alts = range1.alt.value
list20 = []
for i in range(1440):
if (alts[i] >= 20):
list20.append(i)
first20delta = deluni[list20[0]]
last20delta = deluni[list20[len(list20) - 1]]
st = first20delta * u.hour
ls = last20delta * u.hour
if plot:
plt.plot(delta, range1.alt.value)
plt.xlim(0, 12)
plt.xlabel('Hours from 8 PM IST')
plt.ylabel('Saturn Alt at Gravity')
plt.show()
rise = time + st + utcoffset
set = time + ls + utcoffset
rised = rise.to_datetime()
setd = set.to_datetime()
print(rise.to_datetime())
print(set.to_datetime())
return rised, setd
def check_sun_position(self):
now = dt.utcnow()
sun = get_body("sun", Time(now))
sun.location = self.nanten2
azel = sun.altaz
sun_az = azel.az.deg
if sun_az > 240.:
sun_az -= 360.
sun_el = azel.alt.deg
stop_flag = False
az_list = self.az_list
el_list = self.el_list
for i in range(len(az_list)):
if sun_az + 15 > +240.:
if (sun_az - 360. + 15 >= az_list[i] / 3600. >=
-120.) or (sun_az - 15 <= az_list[i] / 3600. <= +240.):
stop_flag = True
else:
pass
elif sun_az - 15 < -240.:
if (sun_az + 360. - 15 <= az_list[i] / 3600. <=
+120.) or (sun_az + 15 >= az_list[i] / 3600. >= -240.):
stop_flag = True
else:
pass
elif sun_az - 15 <= az_list[i] / 3600. <= sun_az + 15:
stop_flag = True
else:
pass
if sun_el - 15 <= el_list[i] / 3600. <= sun_el + 15:
stop_flag = True
return stop_flag
def get_object(objectName: str, earthPos: (float, float), time: str) -> dict:
"""Get the altitude and azimuth of an object at a given time and location
:param objectName: Name of the target object
:param earthPos: Latitude and Longitude of the observation location
:param time: Time of observation
:type objectName: string
:type earthPos: (float, float)
:type time: string
:return: A dict containing the altitude and azimuth of the object
:rtype: { 'alt': float, 'az': float }
"""
(lat, long) = earthPos
astroTime = Time(time)
objectCoord = get_body(objectName, astroTime)
earthCoord = EarthLocation(lat=lat * u.deg, lon=long * u.deg)
observation_frame = AltAz(obstime=astroTime, location=earthCoord)
object_alt_az = objectCoord.transform_to(observation_frame)
return {
'alt': round(object_alt_az.alt.deg, 2),
'az': round(object_alt_az.az.deg, 2)
}
def run(self):
if self.target == "Home":
self.telescope.goto_home()
elif self.target == "Stop":
self.telescope.tracking = False
else:
body = get_body(self.target.lower(), Time.now())
self.telescope.goto(body.ra.hour, body.dec.degree)
def get_mars_ephemeris(timedate):
"""
Get the ephemeris of Mars given a particular julian date
"""
t = Time(timedate)
with solar_system_ephemeris.set('builtin'):
mars = get_body('mars', t)
return mars
def _get_bodies(self, time):
"""Get position of the solar system bodies from Astropy.
"""
return [
get_body(body, time, ephemeris=self.ephemeris).transform_to(ITRS)
for body in self.bodies
]
def set_beam_target(self,
target_or_ra,
dec=None,
load_time=None,
verbose=True):
"""
Given the name of an astronomical target, 'sun', or 'zenith', compute the
current topocentric position of the body and point the beam at it. If
the 'dec' keyword is not None, the target is intepreted to be a RA.
"""
# Force to string
target_or_ra = str(target_or_ra)
if dec is not None:
dec = str(dec)
# Figure out what to do with the name
if target_or_ra.lower() in ('z', 'zen', 'zenith'):
## Zenith is easy
az, alt = 0.0, 90.0
else:
## Load in where we are
obs = EarthLocation.from_geocentric(*self.station.ecef, unit=u.m)
## Resolve the name into coordinates
if dec is not None:
ra = Angle(target_or_ra, unit='hourangle')
dec = Angle(dec, unit='deg')
sc = SkyCoord(ra, dec, frame='fk5')
if verbose:
print(
f"Resolved '{target_or_ra}, {dec}' to RA {sc.ra}, Dec. {sc.dec}"
)
elif target_or_ra.lower() in solar_system_ephemeris.bodies:
if target_or_ra.lower().startswith('earth'):
raise ValueError(f"Invalid target: '{target_or_ra}'")
sc = get_body(target_or_ra.lower(), Time.now(), location=obs)
if verbose:
print(
f"Resolved '{target_or_ra}' to {target_or_ra.lower()}")
else:
sc = SkyCoord.from_name(target_or_ra)
if verbose:
print(
f"Resolved '{target_or_ra}' to RA {sc.ra}, Dec. {sc.dec}"
)
## Figure out where it is right now
aa = sc.transform_to(AltAz(obstime=Time.now(), location=obs))
az = aa.az.deg
alt = aa.alt.deg
if verbose:
print(f"Currently at azimuth {aa.az}, altitude {aa.alt}")
# Point the beam
self.set_beam_pointing(az, alt, degrees=True, load_time=load_time)
def check_sky_tonight(self, obj):
if obj in self.planet_list:
midnight = Time(self.date + ' 00:00:00')
sky_obj = get_body(obj, midnight)
else:
sky_obj = SkyCoord.from_name(obj)
sky_objaltazs_viewing_date = sky_obj.transform_to(self.viewing_frame)
last_hour = 999
for altaz in sky_objaltazs_viewing_date: # need to parallelize this at some point
altitude = altaz.alt
(sign, d, m, s) = altitude.signed_dms
(zsign, zd, zm, zs) = altaz.az.signed_dms
zstr = zsign + zd
ohour = str(altaz.obstime)[11:13]
omin = str(altaz.obstime)[14:16]
odate = str(altaz.obstime)[0:10]
oday = str(altaz.obstime)[8:10]
omon = str(altaz.obstime)[5:7]
object_type = 'Planet'
suggested_filters = ''
finder_link = ''
if obj not in self.planet_list:
my_messier = Messier.MessierData()
object_type = my_messier.object_type[obj]
finder_link = "<a href=\"https://freestarcharts.com/images/Articles/Messier" \
"/Single/{0}_Finder_Chart.pdf\" target=\"_blank\">Finder Chart</a>".format(obj.upper())
if obj in my_messier.messier_filters.keys():
suggested_filters = my_messier.messier_filters[obj]
skip_print = True
if 0 <= int(omin) < 5:
if ohour == last_hour:
skip_print = True
else:
skip_print = False
else:
skip_print = True
last_hour = ohour
if altitude.is_within_bounds(20 * u.deg,
90 * u.deg) and not skip_print:
obs_date, obs_hour = un_utc(odate, ohour)
if int(ohour) % 2 == 0:
tr_bgclr = "#d5f5e3"
else:
tr_bgclr = "#d6eaf8"
compass = return_sector(zstr)
direction = str(zstr) + " - {0}".format(compass)
table_row = "<tr bgcolor={6}><td>{0}</td><td>{5}</td><td>{1}</td><td>{2}</td><td>{3}˚</td>" \
"<td>{4}˚</td><td>{8}</td><td>{7}</td></tr>\n" \
.format(obj.upper(), obs_date, obs_hour, d, direction, object_type, tr_bgclr, suggested_filters,
finder_link)
key = int(omon) * 10000 + int(oday) * 100 + int(ohour)
self.viewing_index[self.v_i_ctr] = key
self.viewing_dictionary[self.v_i_ctr] = table_row
self.v_i_ctr += 1
def jupLoc(tt, dd, loc):
ds = str(dd[0]) + '-' + str(dd[1]) + '-' + str(dd[2])
ts = str(tt[0]) + ':' + str(tt[1]) + ':' + str(tt[2])
t = Time(ds + ' ' + ts)
# loc = EarthLocation.of_site('Kitt Peak')
with solar_system_ephemeris.set('builtin'):
jup_loc = get_body('jupiter', t, loc)
return jup_loc.ra, jup_loc.dec
def compute_constraint(self, times, observer, targets):
# use get_body rather than get sun here, since
# it returns the Sun's coordinates in an observer
# centred frame, so the separation is as-seen
# by the observer.
# 'get_sun' returns ICRS coords.
sun = get_body('sun', times, location=observer.location)
solar_separation = sun.separation(targets)
if self.min is None and self.max is not None:
mask = self.max >= solar_separation
elif self.max is None and self.min is not None:
mask = self.min <= solar_separation
elif self.min is not None and self.max is not None:
mask = ((self.min <= solar_separation) &
(solar_separation <= self.max))
else:
raise ValueError("No max and/or min specified in "
"SunSeparationConstraint.")
return mask
def __init__(self, parent = None, arg = None, name = "mount", port="", connect = True, var = {}):
self.arg = arg
self.Autoconnect = connect
self.port = port
self.parent = parent
self.name = name
self.sname = self.name
self.variables = var
self.rate = 1
self.mount = drive(profile = 'HEQ5', mode = "eq", connectMethod = 'pymlab',
obs_lat = 48.986976, obs_lon = 14.467532, obs_alt = 300, port = '/dev/ttyUSB0')
self.mount.run()
self.mount.UnPark()
#self.mount.Slew(SkyCoord(alt = 45, az = 10, obstime = Time.now(), frame = 'altaz', unit="deg", location = self.mount.getObs()).icrs)
rospy.Subscriber("/mount/controll", String, callback_btn)
rospy.Subscriber("/arom/UI/buttons", String, callback_btn)
self.pub_status = rospy.Publisher('/mount/status', String, queue_size=10)
self.pub_radec = rospy.Publisher('/mount/status/coordinates/RaDec', Float32MultiArray, queue_size=10)
#rospy.init_node('AROM_mount')
AromNode.__init__(self)
print "zinicializovano"
rate = rospy.Rate(self.rate)
ra = 0
dec = 90
while not rospy.is_shutdown():
try:
if len(btn_data) > 0:
print btn_data[0], len(btn_data)
lastBtn = btn_data[0]
btn_data.pop(0)
if "name" in lastBtn:
split = lastBtn.split(" ")
self.mount.Slew(SkyCoord.from_name(split[1]))
#self.mount.Slew(SkyCoord(alt = float(split[1]), az = float(split[2]), obstime = Time.now(), frame = 'altaz', unit="deg", location = self.mount.getObs()).icrs)
elif "solar" in lastBtn:
split = lastBtn.split(" ")
self.mount.Slew(get_body(split[1], obstime = Time.now(), location = self.mount.getObs()).icrs)
elif "sun" in lastBtn:
self.mount.Slew(get_sun(Time.now()).icrs)
elif "altaz" in lastBtn:
split = lastBtn.split(" ")
self.mount.Slew(SkyCoord(alt = float(split[1]), az = float(split[2]), obstime = Time.now(), frame = 'altaz', unit="deg", location = self.mount.getObs()).icrs)
elif "radec" in lastBtn:
split = lastBtn.split(" ")
self.mount.Slew(SkyCoord(alt = float(split[1]), az = float(split[2]), obstime = Time.now(), frame = 'altaz', unit="deg", location = self.mount.getObs()).icrs)
elif lastBtn == 'KEY_OK':
self.mount.Slew(SkyCoord(ra = float(split[1]), dec = float(split[2]), frame = 'icrs', unit="deg"))
#now = Time.now()
#altazframe = AltAz(obstime=now, location=self.mount.getObs())
#sunaltaz = get_sun(now).transform_to(altazframe)
#print sunaltaz, altazframe, now
#self.mount.Slew(SkyCoord(get_sun(Time.now()), location = self.mount.getObs()).icrs)
if lastBtn == 'KEY_UP':
dec += 10
self.mount.Slew(SkyCoord(ra = ra, dec=dec, unit="deg"))
#self.mount.Slew(SkyCoord(alt = 45, az = 181+90, obstime = Time.now(), frame = 'altaz', unit="deg", location = self.mount.getObs()).icrs)
# mode: -90 - 0
if lastBtn == 'KEY_DOWN':
dec -= 10
self.mount.Slew(SkyCoord(ra = ra, dec=dec, unit="deg"))
#self.mount.Slew(SkyCoord(alt = 45, az = 181+45, obstime = Time.now(), frame = 'altaz', unit="deg", location = self.mount.getObs()).icrs)
# mode: -180 - -90
if lastBtn == 'KEY_LEFT':
ra += 10
self.mount.Slew(SkyCoord(ra = ra, dec=dec, unit="deg"))
#self.mount.Slew(SkyCoord(alt = 45, az = 181, obstime = Time.now(), frame = 'altaz', unit="deg", location = self.mount.getObs()).icrs)
#mode: -90 - 0
if lastBtn == 'KEY_RIGHT':
ra -= 10
self.mount.Slew(SkyCoord(ra = ra, dec=dec, unit="deg"))
#self.mount.Slew(SkyCoord(alt = 1, az = 181+90, obstime = Time.now(), frame = 'altaz', unit="deg", location = self.mount.getObs()).icrs)
#mode: -180 - -90
if lastBtn == 'KEY_MENU':
self.mount.Slew(SkyCoord(alt = 1, az = 181+45, obstime = Time.now(), frame = 'altaz', unit="deg", location = self.mount.getObs()).icrs)
if lastBtn == 'KEY_TAB':
self.mount.Slew(SkyCoord(alt = 1, az = 181, obstime = Time.now(), frame = 'altaz', unit="deg", location = self.mount.getObs()).icrs)
elif lastBtn == 'KEY_STOP' or lastBtn == 'home':
self.mount.GoPark()
elif lastBtn == 'KEY_PLAY':
self.mount.UnPark()
else:
#(ra, dec) = self.mount.getCoordinates('RaDec')
#print ra, dec
#try:
# mat = Float32MultiArray(data=[ra, dec])
# self.pub_radec.publish(mat)
#except Exception, e:
# print e
#mat = Float32MultiArray(data=[ra, dec])
#mat.layout.dim.append(MultiArrayDimension())
#mat.layout.dim[0].label = "RaDec"
#mat.layout.dim[0].size = 2
#mat.data.
#print mat
#self.pub_radec.publish(mat)
pass
except Exception, e:
rospy.logerr(e)
rate.sleep()
def find_opp_and_retro(self, start_time):
cur_time = Time(start_time)
last_RA = 0.
last_dist = Distance(999, unit=units.au)
pre_closest = True
self.retrograding = False
retro_start = None
retro_end = None
opptime = None
# Earth location to use for calculating Mars' position.
# Setting it to None will (I think? docs aren't clear) calculate
# from the center of the Earth; this is much faster, skips
# calculations like parallax due to earth's rotation,
# and avoids seeing a lot of spurious retrograde/direct
# transitions due solely to the observer's position changing
# as the earth rotates.
location = None
# A place to store the data points
self.planettrack = []
# When a planet is approaching opposition, its elongation is negative.
# When it flips to positive (-180 to 180), it just passed opposition.
# Can't check for exactly 180 if we're only checking time coarsely.
last_elong = -1
# We'll look for the end of retrograde then go a few days
# past it; but first, put a limit on how far we can go.
end_time = cur_time + TimeDelta(300, format='jd')
# Initially, go one day at a time:
coarsemode = TimeDelta(1, format='jd')
# but in fine mode, we'll go one hour at a time:
finemode = TimeDelta(60*60, format='sec')
# and near opposition we'll go even finer for a few days:
superfinemode = TimeDelta(60 * 5, format='sec')
timeslice = coarsemode
while cur_time < end_time:
cur_time += timeslice
mars = get_body(planetname, cur_time)
flags = ''
# Are we starting or stopping retrograde?
if ( (mars.ra == last_RA) or
(mars.ra < last_RA and not self.retrograding) or
(mars.ra > last_RA and self.retrograding) ):
# Are we still in coarse mode? If so, jump back
# in time a few days and go to fine mode.
if timeslice == coarsemode:
print("Switching to fine mode on", cur_time)
print(" RA", mars.ra.hour, ", dec", mars.dec.degree)
timeslice = finemode
cur_time -= TimeDelta(EXTRA_DAYS, format='jd')
continue
# We're in fine mode. Record dates when the planet
# starts or ends retrograde, hits opposition or makes
# its closest approach.
if self.retrograding:
flags += END_RETROGRADE
# Don't consider this the actual end of retrograde
# unless we're already past opposition.
# There are potentially a lot of false retrogrades.
# We can get them from parallax if we calculate
# Mars' position from a specific earth location;
# but even if we don't, pyastro gives us a lot
# of false little retrogrades and I don't know why.
if opptime:
retro_end = cur_time
else:
flags += START_RETROGRADE
retro_start = cur_time
if mars.ra == last_RA:
flags += STATIONARY
self.retrograding = not self.retrograding
# Calculate elongation to find the opposition time:
sun = get_body('sun', cur_time)
elongation = (mars.ra - sun.ra).degree
# print(cur_time, "\n RA",
# mars.ra.hour, "dec", mars.dec.degree,
# "elongation", elongation)
if last_elong > 180. and elongation <= 180.:
if timeslice == superfinemode:
flags += OPPOSITION
opptime = cur_time
timeslice = finemode
print("Opposition on", cur_time, ", switching back to fine")
# XXX it would be nice not to go back to finemode
# until after we've found closest approach.
# But astropy randomly finds a closest approach
# date weeks before the actual closest approach,
# at the start of retrograde.
else:
# Looks like opposition. But let's go back a day and
# get a finer view of the time.
print("Switching to superfine mode on", cur_time)
timeslice = superfinemode
cur_time -= TimeDelta(1, format='jd')
if mars.distance >= last_dist and pre_closest:
flags += CLOSEST_APPROACH
# self.find_parallax(cur_time)
pre_closest = False
elif mars.distance < last_dist: # receding
pre_closest = True
if flags or self.save_all_points:
self.planettrack.append([cur_time.datetime,
mars.ra.radian, mars.dec.radian,
mars.distance.km, flags])
last_RA = mars.ra
last_dist = mars.distance
last_elong = elongation
# If we've seen the opposition as well as retro_start and retro_end
# then we're done. Switch back to coarse mode and record a
# few more days.
if timeslice == finemode and retro_start and retro_end and opptime:
timeslice = coarsemode
end_time = cur_time + TimeDelta(EXTRA_DAYS, format='jd')
# We're done calculating all the points.
# Now calculate the retrograde midpoint, if we have both start and end.
if retro_start and retro_end:
mid_retro_date = retro_start + (retro_end - retro_start) / 2
mars = get_body(planetname, mid_retro_date)
# Insert that into our planettrack list:
for i, point in enumerate(self.planettrack):
if point[IDATE] == mid_retro_date:
point[IFLAGS] += MIDPOINT_RETRO
break
elif point[IDATE] > mid_retro_date:
self.planettrack.insert(i, [mid_retro_date.datetime,
mars.ra.radian, mars.dec.radian,
mars.distance.km,
MIDPOINT_RETRO])
# We've just changed a list in the middle of looping
# over that list, but it's okay because we're breaking out.
break
else:
print("don't have both retro start and end")
# Now print what we found.
print("%20s %-19s %-11s %-10s %s" % ('', 'Date',
'RA', 'Dec', 'Dist (mi)'))
for point in self.planettrack:
if point[IFLAGS]:
# print("%20s %-19s %-11s %-10s %d" % \
# (self.flags_to_string(point[4]), str(point[0]),
# point[1], point[2],
# point[3] * 9.2956e7))
print("%20s %-19s %-11.7f %-10.7f %d" % \
(self.flags_to_string(point[IFLAGS]), str(point[IDATE]),
self.rads_to_hours(point[IRA]),
self.rads_to_degrees(point[IDEC]),
point[IDIST] / 1.609344))
