def __init__(self, y, m, d, h, minutes, seconds):
if y < 1980:
raise Exception("Year #{y} must >= 1980")
in_time = utc.utc_datetime(year=y,
month=m,
day=d,
hour=h,
minute=minutes,
second=0)
gps_t = utc.utc_datetime(year=1980,
month=1,
day=6,
hour=0,
minute=0,
second=0)
self.m_day_of_year = in_time.timetuple().tm_yday
gps_sec = (in_time -
gps_t).total_seconds() + seconds + self.utc_offset(in_time)
gps_days = int(math.floor(gps_sec / GpsTime.SEC_PER_DAY))
gps_weeks = gps_days / 7.0
self.m_week = int(math.floor(gps_weeks))
self.sec_of_week = gps_sec - self.m_week * 7.0 * GpsTime.SEC_PER_DAY
def __init__(self, y, m, d, h, minutes, seconds):
if (y < 1980):
raise Exception("Year #{y} must >= 1980")
in_time = utc.utc_datetime(year=y, month=m, day=d, hour=h, minute=minutes, second=0)
gps_t = utc.utc_datetime(year=1980, month=1, day=6, hour=0, minute=0, second=0)
self.m_day_of_year = in_time.timetuple().tm_yday
gps_sec = ( in_time - gps_t ).total_seconds() + seconds + self.utc_offset(in_time)
gps_days = int(math.floor(gps_sec / GpsTime.SEC_PER_DAY))
gps_weeks = gps_days / 7.0
self.m_week = int(math.floor(gps_weeks))
self.sec_of_week = gps_sec - self.m_week*7.0*GpsTime.SEC_PER_DAY
def test_gps(self):
import ephem
dnd = ephem.Observer()
dnd.lon = str(location.Dunedin.lon.to_degrees())
dnd.lat = str(location.Dunedin.lat.to_degrees())
dnd.elevation = location.Dunedin.alt
dnd.pressure = 0.0
t = utc.utc_datetime(2013,9,20,0,0,3)
dnd.date = t
for svnum in range(31,32):
l1 = 'GPS BIIRM-2 (PRN 31) '
l2 = '1 29486U 06042A 13264.26023969 -.00000084 00000-0 00000+0 0 2292'
l3 = '2 29486 56.1466 336.5502 0081195 316.5190 69.5394 2.00563866 51246'
j = ephem.readtle(l1,l2,l3)
# http://blog.thetelegraphic.com/2012/gps-sattelite-tracking-in-python-using-pyephem/
#j = ephem.Gps(svnum)
j.compute(dnd)
ra_e = angle.from_rad(j.ra.real)
dec_e= angle.from_rad(j.dec.real)
sv = GpsSatellite(svnum, location.Dunedin)
ra, dec = sv.radec(t)
print angle.wrap_360(ra.to_degrees())
self.assertAlmostEqual(ra.to_degrees(), ra_e.to_degrees(), 0)
self.assertAlmostEqual(dec.to_degrees(), dec_e.to_degrees(), 0)
def setUp(self):
self.utc_date = utc.utc_datetime(year=2009,
month=7,
day=22,
hour=5,
minute=9,
second=50.3)
def test_gps(self):
import ephem
dnd = ephem.Observer()
dnd.lon = str(location.Dunedin.lon.to_degrees())
dnd.lat = str(location.Dunedin.lat.to_degrees())
dnd.elevation = location.Dunedin.alt
dnd.pressure = 0.0
t = utc.utc_datetime(2013, 9, 20, 0, 0, 3)
dnd.date = t
for svnum in range(31, 32):
l1 = "GPS BIIRM-2 (PRN 31) "
l2 = "1 29486U 06042A 13264.26023969 -.00000084 00000-0 00000+0 0 2292"
l3 = "2 29486 56.1466 336.5502 0081195 316.5190 69.5394 2.00563866 51246"
j = ephem.readtle(l1, l2, l3)
# http://blog.thetelegraphic.com/2012/gps-sattelite-tracking-in-python-using-pyephem/
# j = ephem.Gps(svnum)
j.compute(dnd)
ra_e = angle.from_rad(j.ra.real)
dec_e = angle.from_rad(j.dec.real)
sv = GpsSatellite(svnum, location.Dunedin)
ra, dec = sv.radec(t)
print(angle.wrap_360(ra.to_degrees()))
self.assertAlmostEqual(ra.to_degrees(), ra_e.to_degrees(), 0)
self.assertAlmostEqual(dec.to_degrees(), dec_e.to_degrees(), 0)
def test_basic(self):
utcd = utc_datetime(year=2009,
month=7,
day=22,
hour=5,
minute=9,
second=50.3)
apyt = time.Time('2009-07-22 05:09:50.3', format='iso', scale='utc')
apyt2 = time.Time(utcd, scale='utc')
utcd2 = apyt.to_datetime(UTC())
obstime = apyt2.to_datetime(UTC())
self.assertEqual(utcd2.year, utcd.year)
self.assertEqual(utcd2.month, utcd.month)
self.assertEqual(utcd2.day, utcd.day)
self.assertEqual(utcd2.hour, utcd.hour)
self.assertEqual(utcd2.minute, utcd.minute)
self.assertEqual(utcd2.second, utcd.second)
self.assertEqual((utcd - obstime).total_seconds(), 0.0)
def utc_offset(self, t):
if t >= utc.utc_datetime(2017, 1, 1):
return 18
if t >= utc.utc_datetime(2015, 7, 1):
return 17
if t >= utc.utc_datetime(2012, 7, 1):
return 16
if t >= utc.utc_datetime(2009, 1, 1):
return 15
if t >= utc.utc_datetime(2006, 1, 1):
return 14
if t >= utc.utc_datetime(1999, 1, 1):
return 13
if t >= utc.utc_datetime(1997, 7, 1):
return 12
if t >= utc.utc_datetime(1996, 1, 1):
return 11
if t >= utc.utc_datetime(1994, 7, 1):
return 10
if t >= utc.utc_datetime(1993, 7, 1):
return 9
if t >= utc.utc_datetime(1992, 7, 1):
return 8
if t >= utc.utc_datetime(1991, 1, 1):
return 7
if t >= utc.utc_datetime(1990, 1, 1):
return 6
if t >= utc.utc_datetime(1988, 1, 1):
return 5
if t >= utc.utc_datetime(1985, 7, 1):
return 4
if t >= utc.utc_datetime(1983, 7, 1):
return 3
if t >= utc.utc_datetime(1982, 7, 1):
return 2
if t >= utc.utc_datetime(1981, 7, 1):
return 1
if t >= utc.utc_datetime(1980, 1, 1):
return 0
return False
def setUp(self):
self.ep = EphemeridesProxy.Instance()
self.s = self.ep.server
self.t = utc.utc_datetime(2002, 10, 31, 0, 2, 2)
self.eph_hash = self.s.get_ephemeris(self.t.isoformat(), 1)
def utc_offset(self, t):
if (t >= utc.utc_datetime(2012, 7, 1)):
return 16
if (t >= utc.utc_datetime(2009, 1, 1)):
return 15
if (t >= utc.utc_datetime(2006, 1, 1)):
return 14
if (t >= utc.utc_datetime(1999, 1, 1)):
return 13
if (t >= utc.utc_datetime(1997, 7, 1)):
return 12
if (t >= utc.utc_datetime(1996, 1, 1)):
return 11
if (t >= utc.utc_datetime(1994, 7, 1)):
return 10
if (t >= utc.utc_datetime(1993, 7, 1)):
return 9
if (t >= utc.utc_datetime(1992, 7, 1)):
return 8
if (t >= utc.utc_datetime(1991, 1, 1)):
return 7
if (t >= utc.utc_datetime(1990, 1, 1)):
return 6
if (t >= utc.utc_datetime(1988, 1, 1)):
return 5
if (t >= utc.utc_datetime(1985, 7, 1)):
return 4
if (t >= utc.utc_datetime(1983, 7, 1)):
return 3
if (t >= utc.utc_datetime(1982, 7, 1)):
return 2
if (t >= utc.utc_datetime(1981, 7, 1)):
return 1
if (t >= utc.utc_datetime(1980, 1, 1)):
return 0
return False
def test_radec(self): sv = GpsSatellite(31, location.Dunedin) t = utc.utc_datetime(2013,9,20,0,0,3) ra, dec = sv.radec(t) self.assertLess(ra.to_degrees(), 360.0) self.assertLess(abs(dec.to_degrees()), 90.0)
def setUp(self):
self.t = utc.utc_datetime(2002, 10, 31, 0, 2, 2)
self.s = Sun()
def test_power(self): sv = GpsSatellite(31, location.Dunedin) t = utc.utc_datetime(2013,9,20,0,0,3) self.assertLess(sv.jansky(t), 5.0e6) self.assertGreater(sv.jansky(t), 3.0e6)
def test_power(self):
sv = GpsSatellite(31, location.Dunedin)
t = utc.utc_datetime(2013, 9, 20, 0, 0, 3)
self.assertLess(sv.jansky(t), 5.0e6)
self.assertGreater(sv.jansky(t), 3.0e6)
def setUp(self): self.t = utc.utc_datetime(2002, 10, 31, 0, 2, 2) self.s = Sun()
print(r.url)
print(r.text)
t = datetime.datetime.utcnow() # utc.utc_datetime(2002, 10, 31, 2, 2, 2)
#for i in range(0,100):
#t = t - datetime.timedelta(seconds=100.0)
#payload = {'date': t, 'sv':1}
#r = requests.get('{}/position'.format(server), params=payload)
#print r.text
#payload = {'date': t.isoformat(), 'sv':1, 'lat':-45.86, 'lon':170.54}
#r = requests.get('{}/catalog'.format(server), params=payload)
#print r.url
#print r.text
ep = EphemeridesProxy.Instance()
t = utc.utc_datetime(2013, 9, 21, 0, 59, 3)
sv = 21
for i in range(0,100):
t = t + datetime.timedelta(seconds=1.0)
pos = ep.get_sv_position(t, sv)
pos_remote = ep.get_remote_position(t, sv)
diff = np.array(pos) - np.array(pos_remote)
dr = np.sqrt(diff.dot(diff))
print(t, dr)
def setUp(self):
self.ep = EphemeridesProxy.Instance()
self.s = self.ep.server
self.t = utc.utc_datetime(2002, 10, 31, 0, 2, 2)
self.eph_hash = self.s.get_ephemeris(self.t.isoformat(), 1)
def setUp(self):
self.utc_date = utc.utc_datetime(year=2009, month=7, day=22, hour=5, minute=9, second=50.3)
def setUp(self):
self.s = jsonrpclib.Server('http://astro.elec.ac.nz:8876/rpc/gps')
self.t = utc.utc_datetime(2002, 10, 31, 0, 2, 2)
self.eph_hash = self.s.get_ephemeris(self.t.isoformat(), 1)
def test_radec(self):
sv = GpsSatellite(31, location.Dunedin)
t = utc.utc_datetime(2013, 9, 20, 0, 0, 3)
ra, dec = sv.radec(t)
self.assertLess(ra.to_degrees(), 360.0)
self.assertLess(abs(dec.to_degrees()), 90.0)