def test_predicted_pass_no_eq(self):
aos = datetime.datetime.utcnow()
max_elevation_date = datetime.datetime.utcnow() + datetime.timedelta(
minutes=5)
los = datetime.datetime.utcnow() + datetime.timedelta(minutes=10)
max_elevation_position = Position(when_utc=max_elevation_date,
position_ecef=(1, 1, 1),
velocity_ecef=(1, 1, 1),
error_estimate=0)
p1 = PredictedPass(sate_id=1,
location=ARG,
aos=aos,
los=los,
duration_s=600,
max_elevation_date=max_elevation_date,
max_elevation_position=max_elevation_position,
max_elevation_deg=10)
p2 = PredictedPass(sate_id=1,
location=ARG,
aos=aos,
los=los,
duration_s=600,
max_elevation_date=max_elevation_date,
max_elevation_position=max_elevation_position,
max_elevation_deg=50)
self.assertNotEqual(p1, p2)
self.assertNotEqual(p2, p1)
def _build_predicted_pass(self, accuratepass):
"""Returns a classic predicted pass"""
tca_position = self.propagator.get_position(accuratepass.tca)
return PredictedPass(self.location, self.propagator.sate_id,
max_elevation_deg=accuratepass.max_elevation_deg,
aos=accuratepass.aos,
los=accuratepass.los,
duration_s=accuratepass.duration.total_seconds(),
max_elevation_position=tca_position,
max_elevation_date=accuratepass.tca,
)
def test_midpoint(self):
aos = dt.datetime.utcnow()
max_elevation_date = aos + dt.timedelta(minutes=5)
los = aos + dt.timedelta(minutes=10)
pass_ = PredictedPass(sate_id=1,
location=ARG,
aos=aos,
los=los,
duration_s=600,
max_elevation_date=max_elevation_date,
max_elevation_position=None,
max_elevation_deg=10)
self.assertEqual(pass_.midpoint, aos + dt.timedelta(minutes=5))
def test_off_nadir_satellite_passing_right_means_negative_sign(self):
position_ecef = llh_to_ecef(0, 10, 500 * 1000)
velocity_ecef = (0, 0, -1)
max_elevation_position = Position(None, position_ecef, velocity_ecef,
None)
pass_ = PredictedPass(sate_id=1,
location=self.location,
aos=None,
los=None,
duration_s=None,
max_elevation_position=max_elevation_position,
max_elevation_deg=None)
self.assertLessEqual(pass_.off_nadir_deg, 0)
def _get_next_pass(self, location, when_utc, aos_at_dg=0, limit_date=None):
if not isinstance(location, Location):
raise TypeError("location must be a Location instance")
pass_ = PredictedPass(location=location,
sate_id=self.sate_id,
aos=None,
los=None,
max_elevation_date=None,
max_elevation_position=None,
max_elevation_deg=0,
duration_s=0)
seconds = 0
self._iterations = 0
while True:
# to optimize the increment in seconds must be inverse proportional to
# the distance of 0 elevation
date = when_utc + datetime.timedelta(seconds=seconds)
if limit_date is not None and date > limit_date:
raise NotReachable('Propagation limit date exceded')
elev_pos = self.get_position(date)
_, elev = location.get_azimuth_elev(elev_pos)
elev_deg = degrees(elev)
if elev_deg > pass_.max_elevation_deg:
pass_.max_elevation_position = elev_pos
pass_.max_elevation_date = date
pass_.max_elevation_deg = elev_deg
if elev_deg > aos_at_dg and pass_.aos is None:
pass_.aos = date
if pass_.aos and elev_deg < aos_at_dg:
pass_.los = date
pass_.duration_s = (pass_.los - pass_.aos).total_seconds()
break
if elev_deg < -2:
delta_s = abs(elev_deg) * 15 + 10
else:
delta_s = 20
seconds += delta_s
self._iterations += 1
return pass_
def test_off_nadir_satellite_exactly_over(self):
position_ecef = llh_to_ecef(0, 0, 500 *
1000) # A satellite exactly over the point
velocity_ecef = (0, 0, 1)
max_elevation_position = Position(None, position_ecef, velocity_ecef,
None)
pass_ = PredictedPass(sate_id=1,
location=self.location,
aos=None,
los=None,
duration_s=None,
max_elevation_position=max_elevation_position,
max_elevation_deg=None)
self.assertAlmostEqual(pass_.off_nadir_deg, 0, delta=0.02)
def test_off_nadir_satellite_passing_left_means_positive_sign(self):
position_ecef = llh_to_ecef(0, -10, 500 *
1000) # A satellite exactyl over the point
velocity_ecef = (0, 0, -1)
max_elevation_position = Position(None, position_ecef, velocity_ecef,
None)
pass_ = PredictedPass(sate_id=1,
location=self.location,
aos=None,
los=None,
duration_s=None,
max_elevation_position=max_elevation_position,
max_elevation_deg=None)
self.assertGreaterEqual(pass_.off_nadir_deg, 0)
def get_pass(location, name, aos, los, max_elevation, when_max_elevation = 0.5):
duration_s = (los - aos).total_seconds()
max_elevation_date = aos + datetime.timedelta(seconds=duration_s * when_max_elevation)
return PredictedPass(location, name, max_elevation, aos, los, duration_s, max_elevation_date=max_elevation_date)