def test_eci_aer(useastropy):
t = '2013-01-15T12:00:05'
aer1 = pm.eci2aer(*eci0, 42, -100, 0, t, useastropy=useastropy)
assert aer1 == approx([83.73050, -6.614478, 1.473510e6], rel=0.001)
assert pm.aer2eci(*aer1, 42, -100, 0, t, useastropy=useastropy) == approx(eci0, rel=0.001)
with pytest.raises(ValueError):
pm.aer2eci(aer1[0], aer1[1], -1, 42, -100, 0, t, useastropy=useastropy)
def test_eci_aer(useastropy):
pytest.importorskip("numpy")
t = "2013-01-15T12:00:05"
aer1 = pm.eci2aer(*eci0, 42, -100, 0, t, useastropy=useastropy)
assert aer1 == approx([83.73050, -6.614478, 1.473510e6], rel=0.001)
assert pm.aer2eci(*aer1, 42, -100, 0, t, useastropy=useastropy) == approx(eci0, rel=0.001)
with pytest.raises(ValueError):
pm.aer2eci(aer1[0], aer1[1], -1, 42, -100, 0, t, useastropy=useastropy)
def test_aer2eci(use_astropy):
# test coords from Matlab aer2eci
pytest.importorskip("numpy")
if use_astropy:
pytest.importorskip("astropy")
aer = [162.55, 55.12, 384013940.9]
lla = [28.4, -80.5, 2.7]
t = datetime(1969, 7, 20, 21, 17, 40)
eci = pm.aer2eci(*aer, *lla, t, use_astropy=use_astropy)
rel = 0.001 if use_astropy else 0.06
assert eci == approx([-3.8454e8, -0.5099e8, -0.3255e8], rel=rel)
with pytest.raises(ValueError):
pm.aer2eci(aer[0], aer[1], -1, *lla, t)
def test_eci_vallado():
t = '2013-01-15T12:00:05'
lla = pm.eci2geodetic(eci0, t, useastropy=False)
assert lla == approx(lla0, rel=0.2)
eci1 = pm.eci2ecef(eci0, t, useastropy=False)
assert eci1 == approx(
[649012.04640917, -4697980.55129606, 4250818.82815207], rel=0.001)
assert pm.ecef2eci(eci1, t, useastropy=False) == approx(eci0, rel=0.001)
aer1 = pm.eci2aer(eci0, 42, -100, 0, t, useastropy=False)
assert aer1 == approx([83.73050, -6.614478, 1.473510e6], rel=0.001)
assert pm.aer2eci(*aer1, 42, -100, 0, t,
useastropy=False) == approx(eci0, rel=0.001)
with pytest.raises(ValueError):
pm.aer2eci(aer1[0], aer1[1], -1, 42, -100, 0, t, useastropy=False)
def eci_position_from_pulse(pulse, lat, long, alt):
time, az, el, r = pulse.split("\t")
t = datetime.strptime(time, "%Y-%m-%d-%H:%M:%S.%f-%Z")
# az: azimuth (degrees)
# el: elevation (degrees)
# r: range (km -> m)
x, y, z = pm.aer2eci(float(az), float(el), float(r) * 1000, lat, long, alt, t, deg=True)
return [x, y, z], t
def test_eci_astropy():
pytest.importorskip('astropy')
t = '2013-01-15T12:00:05'
lla = pm.eci2geodetic(eci0, t)
assert lla == approx(lla0, rel=0.2)
eci1 = pm.eci2ecef(eci0, t)
assert eci1 == approx(
[649012.04640917, -4697980.55129606, 4250818.82815207])
assert pm.ecef2eci(eci1, t) == approx(eci0)
aer1 = pm.eci2aer(eci0, 42, -100, 0, t)
assert aer1 == approx([83.73050, -6.614478, 1.473510e6])
assert pm.aer2eci(*aer1, 42, -100, 0, t) == approx(eci0)
with pytest.raises(ValueError):
pm.aer2eci(aer1[0], aer1[1], -1, 42, -100, 0, t)
