Exemplo n.º 1
0
 def test_era(self):
     """Comare ERA relative to erfa.era00 test case."""
     t = Time(2400000.5, 54388.0, format='jd', location=(0, 0), scale='ut1')
     era = t.earth_rotation_angle()
     expected = 0.4022837240028158102 * u.radian
     # Without the TIO locator/polar motion, this should be close already.
     assert np.abs(era - expected) < 1e-10 * u.radian
     # And with it, one should reach full precision.
     sp = erfa.sp00(t.tt.jd1, t.tt.jd2)
     iers_table = iers.earth_orientation_table.get()
     xp, yp = [c.to_value(u.rad) for c in iers_table.pm_xy(t)]
     r = erfa.rx(-yp, erfa.ry(-xp, erfa.rz(sp, np.eye(3))))
     expected1 = expected + (np.arctan2(r[0, 1], r[0, 0]) << u.radian)
     assert np.abs(era - expected1) < 1e-12 * u.radian
     # Now try at a longitude different from 0.
     t2 = Time(2400000.5,
               54388.0,
               format='jd',
               location=(45, 0),
               scale='ut1')
     era2 = t2.earth_rotation_angle()
     r2 = erfa.rz(np.deg2rad(45), r)
     expected2 = expected + (np.arctan2(r2[0, 1], r2[0, 0]) << u.radian)
     assert np.abs(era2 - expected2) < 1e-12 * u.radian
Exemplo n.º 2
0
GST = erfa.anp(erfa.gmst82(DJMJD0 + DATE, TUT) + EE)
print("GST = %.17f radians" % GST)
print("    = %.17f degrees" % math.degrees(GST))
print("    = %s%dd%dm%d.%ds" % erfa.a2af(6, GST))
print("    = %s%dh%dm%d.%ds" % erfa.a2tf(6, GST))

# Form celestial-terrestrial matrix (no polar motion yet).
##RC2TI = erfa.cr(RNPB)
##RC2TI = erfa.rz(GST, RC2TI)
RC2TI = erfa.rz(GST, RNPB)
print("celestial to terrestrial matrix (no polar motion)")
pprint(RC2TI)

# Polar motion matrix (TIRS->ITRS, IERS 1996).
RPOM = erfa.ir()
RPOM = erfa.rx(-YP, RPOM)
RPOM = erfa.ry(-XP, RPOM)

# Form celestial-terrestrial matrix (including polar motion).
RC2IT = erfa.rxr(RPOM, RC2TI)
print("celestial to terrestrial matrix (including polar motion)")
pprint(RC2IT)

##A = scipy.matrix(RC2IT)

print('''
============================================
IAU 2000A, CIO based, using classical angles
============================================
''')
# CIP and CIO, IAU 2000A.
Exemplo n.º 3
0
GST = erfa.anp(erfa.gmst82(DJMJD0+DATE, TUT) + EE)
print("GST = %.17f radians"%GST)
print("    = %.17f degrees"%math.degrees(GST))
print("    = %s%dd%dm%d.%ds"%erfa.a2af(6, GST))
print("    = %s%dh%dm%d.%ds"%erfa.a2tf(6, GST))

# Form celestial-terrestrial matrix (no polar motion yet).
##RC2TI = erfa.cr(RNPB)
##RC2TI = erfa.rz(GST, RC2TI)
RC2TI = erfa.rz(GST, RNPB)
print("celestial to terrestrial matrix (no polar motion)")
pprint(RC2TI)

# Polar motion matrix (TIRS->ITRS, IERS 1996).
RPOM = erfa.ir()
RPOM = erfa.rx(-YP, RPOM)
RPOM = erfa.ry(-XP, RPOM)

# Form celestial-terrestrial matrix (including polar motion).
RC2IT = erfa.rxr(RPOM, RC2TI)
print("celestial to terrestrial matrix (including polar motion)")
pprint(RC2IT)

##A = scipy.matrix(RC2IT)

print('''
============================================
IAU 2000A, CIO based, using classical angles
============================================
''')
# CIP and CIO, IAU 2000A.
Exemplo n.º 4
0
    print("    = %s"%c, end='')
    print("%dd%dm%d.%ds"%tuple(a))
for c,a in erfa.a2tf(6, GST):
    print("    = %s"%c, end='')
    print("%dh%dm%d.%ds"%tuple(a))

# Form celestial-terrestrial matrix (no polar motion yet).
##RC2TI = erfa.cr(RNPB)
##RC2TI = erfa.rz(GST, RC2TI)
RC2TI = erfa.rz(GST, RNPB)
print("celestial to terrestrial matrix (no polar motion)")
pprint(RC2TI)

# Polar motion matrix (TIRS->ITRS, IERS 1996).
RPOM = np.array([np.identity(3)]) ##erfa.ir()
RPOM = erfa.rx(np.array([-YP]), RPOM)
RPOM = erfa.ry(np.array([-XP]), RPOM)

# Form celestial-terrestrial matrix (including polar motion).
RC2IT = erfa.rxr(RPOM, RC2TI)
print("celestial to terrestrial matrix (including polar motion)")
pprint(RC2IT)

##A = scipy.matrix(RC2IT)

print('''
============================================
IAU 2000A, CIO based, using classical angles
============================================
''')
# CIP and CIO, IAU 2000A.