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from astropy.time import Time | ||
from ...orbits import Orbits | ||
from ... import coordinates | ||
from ...utils.helpers.orbits import make_real_orbits | ||
from .. import Propagator | ||
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import quivr | ||
import pyarrow as pa | ||
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class MockPropagator(Propagator): | ||
# MockPropagator propagates orbits by just setting the time of the orbits. | ||
def _propagate_orbits(self, orbits: Orbits, times: Time) -> Orbits: | ||
all_times = [] | ||
for t in times: | ||
repeated_time = Time([t] * len(orbits)) | ||
orbits.coordinates.time = coordinates.Times.from_astropy( | ||
repeated_time | ||
).to_structarray() | ||
all_times.append(orbits) | ||
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return quivr.concatenate(all_times) | ||
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def _generate_ephemeris(self, orbits: Orbits, observers): | ||
raise NotImplementedError("not impleemented") | ||
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def test_propagator_single_worker(): | ||
orbits = make_real_orbits(10) | ||
times = Time(["2020-01-01T00:00:00", "2020-01-01T00:00:01"]) | ||
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prop = MockPropagator() | ||
have = prop.propagate_orbits(orbits, times, num_jobs=1) | ||
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assert len(have) == len(orbits) * len(times) | ||
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def test_propagator_multiple_workers(): | ||
orbits = make_real_orbits(10) | ||
times = Time(["2020-01-01T00:00:00", "2020-01-01T00:00:01"]) | ||
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prop = MockPropagator() | ||
have = prop.propagate_orbits(orbits, times, num_jobs=4) | ||
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assert len(have) == len(orbits) * len(times) |