def test_interpolation_err_heo():
"""Tests the interpolation accuracy for Highly Elliptic Orbits."""
# Init TLE
line1 = "1 99999U 12345A 20162.50918981 .00000000 00000-0 00000-0 0 00005"
line2 = "2 99999 000.0000 124.6202 0000000 000.0000 000.0000 01.00273791000004"
# test init time
init_time = Time("2020:162:00:00:00", format="yday", scale="utc")
tle = TLE.from_tle(line1, line2)
tle.epoch = init_time
tle.mean_anomaly = 0
tle.eccentricity = 0.4
heo_line1, heo_line2 = tle.export_tle()
# print(tle)
duration = TimeDelta(3.0, format="jd")
steps = 4000 # number of steps within the propagation duration
dt, time_list = generate_timelist(init_time, duration, steps)
prop_output = propagation_engine(heo_line1, heo_line2, time_list)
max_err, max_nominal_err = check_errors(init_time, dt, prop_output["sat"],
prop_output["traj"], False)
assert max_err < 0.040 * u.mm
assert max_nominal_err < 0.00030 * u.mm
def test_tle_with_params(init_tle_leo, check_str_leo):
"""Test initialise from parameters."""
tle1 = init_tle_leo
tle2 = TLE(
tle1.epoch,
tle1.inclination,
tle1.raan,
tle1.eccentricity,
tle1.arg_perigee,
tle1.mean_anomaly,
tle1.mean_motion,
tle1.bstar,
tle1.n_dot,
n_dotdot=tle1.n_dotdot,
name=init_tle_leo.name,
intl_designator=tle1.intl_designator,
sat_num=tle1.sat_number,
classification=tle1.classification,
rev_nr=tle1.rev_nr,
el_nr=tle1.el_nr,
)
assert str(tle2) == check_str_leo == str(tle1)
def tle_geo():
"""Generates the TLE with near-circular LEO test setup."""
name = "TURKSAT 4B"
line1 = "1 40984U 15060A 18198.04228921 .00000095 00000-0 00000+0 0 9995"
line2 = "2 40984 0.0142 325.6420 0001708 151.3463 243.0113 1.00269765 10118"
return TLE.from_tle(line1, line2, name)
def tle_leo():
"""Generates the TLE with near-circular LEO test setup."""
name = "RASAT"
line1 = "1 37791U 11044D 18198.20691930 -.00000011 00000-0 70120-5 0 9992"
line2 = "2 37791 98.1275 290.4108 0021116 321.0704 38.8990 14.64672859369594"
return TLE.from_tle(line1, line2, name)
def tle_heo():
"""Generates the TLE with HEO test setup (e=0.70)."""
name = "ATLAS 2A CENTAUR R/B"
line1 = "1 23840U 96020B 18198.38669861 -.00000081 00000-0 00000+0 0 9997"
line2 = "2 23840 21.5075 284.9295 6975939 94.1963 356.6140 2.24211004182606"
return TLE.from_tle(line1, line2, name)
def init_tle_vgd():
"""Generates the TLE with LEO test setup."""
name = "VANGUARD 1"
line1 = "1 00005U 58002B 00179.78495062 .00000023 00000-0 28098-4 0 4753"
line2 = "2 00005 34.2682 348.7242 1859667 331.7664 19.3264 10.82419157413667"
return TLE.from_tle(line1, line2, name)
def init_tle_decay():
"""Generates the TLE with decay test setup."""
name = "MICROSAT-R DEB"
line1 = "1 44160U 19006AX 20178.55672017 .00609591 12600-3 17697-2 0 9996"
line2 = "2 44160 95.2356 283.8798 0142512 327.7074 31.5529 15.78083811 64981"
return TLE.from_tle(line1, line2, name)
def generate_geo_140w_trajectory(time_list):
"""Generates a GEO (140 deg West) trajectory."""
# Init TLE
tle = TLE.init_geo(Time("2015-10-04T00:00:00.000", scale="utc"), -140 * u.deg)
line1, line2 = tle.export_tle()
trajectory = propagation_engine(line1, line2, time_list)["traj"]
return trajectory
def test_init_geo(init_tle_geo):
"""Test init GEO satellite."""
tle_geo = init_tle_geo
epoch = Time("2020-06-10T12:13:14.000")
longitude = 42.0 * u.deg
tle = TLE.init_geo(
epoch,
longitude,
name=tle_geo.name,
sat_num=tle_geo.sat_number,
intl_designator=tle_geo.intl_designator,
rev_nr=tle_geo.rev_nr,
el_nr=tle_geo.el_nr,
)
assert str(tle_geo) == str(tle)
def _parse_tle_list(tle_source_str_list):
"""
Parses the TLE list.
Parameters
----------
tle_source_str_list : list[str]
TLE data as a list of strings.
Returns
-------
tle_list : list[TLE]
List of TLE data
"""
tle_list = []
name = line1 = line2 = None
for i, line in enumerate(tle_source_str_list):
# strip spaces and EOF around the line
line = line.strip()
# skip empty lines
if not line.strip():
continue
if __is_tle_line(line, 1):
line1 = line
if __is_tle_line(tle_source_str_list[i + 1], 2):
line2 = tle_source_str_list[i + 1]
if i > 0 and (
not __is_tle_line(tle_source_str_list[i - 1], 1)
and not __is_tle_line(tle_source_str_list[i - 1], 2)):
name = tle_source_str_list[i - 1].strip("\n ")
if name.startswith("0 "):
name = name[2:]
if line1 and line2:
tle = TLE.from_tle(line1, line2, name if name else "")
tle_list.append(tle)
# reset temp fields
name = line1 = line2 = None
return tle_list
def test_tle_init_incl_out_of_bounds(init_tle_leo):
"""Tests init with inclination input value out of bounds
- should raise `ValueError`."""
with pytest.raises(ValueError):
tle1 = init_tle_leo
TLE(
tle1.epoch,
2 * np.pi,
tle1.raan,
tle1.eccentricity,
tle1.arg_perigee,
tle1.mean_anomaly,
tle1.mean_motion,
tle1.bstar,
tle1.n_dot,
n_dotdot=tle1.n_dotdot,
name=init_tle_leo.name,
intl_designator=tle1.intl_designator,
sat_num=tle1.sat_number,
classification=tle1.classification,
rev_nr=tle1.rev_nr,
el_nr=tle1.el_nr,
)
def test_tle_init_with_lines(tle_leo, check_str_leo):
"""Test initialise from TLE."""
tle1 = TLE.from_tle(tle_leo.line1, tle_leo.line2, tle_leo.name)
assert str(tle1) == check_str_leo
def init_tle_geo(tle_geo):
"""Generates the GEO TLE test setup."""
return TLE.from_tle(tle_geo.line1, tle_geo.line2, tle_geo.name)
def init_tle_leo(tle_leo):
"""Generates the TLE with LEO test setup."""
return TLE.from_tle(tle_leo.line1, tle_leo.line2, tle_leo.name)
def init_tle_sso(tle_sso):
"""Generates the TLE with SSO repeat groundtrack test setup."""
return TLE.from_tle(tle_sso.line1, tle_sso.line2, tle_sso.name)