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TST: attempt at tests re-run.
1 parent d20159d commit 8e734c6

2 files changed

Lines changed: 25 additions & 12 deletions

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rocketpy/mathutils/_calc/polation_1d.py

Lines changed: 1 addition & 1 deletion
Original file line numberDiff line numberDiff line change
@@ -81,7 +81,7 @@ def _cubic_eval_vec(
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float or np.ndarray
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The evaluated cubic polynomial value(s).
8383
"""
84-
return a + t * (b + t * (c + t * d))
84+
return a + b * t + c * (t**2) + d * (t**3)
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8787
class Linear1DPolation(PolationBase):

tests/integration/simulation/test_flight.py

Lines changed: 24 additions & 11 deletions
Original file line numberDiff line numberDiff line change
@@ -2,6 +2,7 @@
22

33
import matplotlib as plt
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import numpy as np
5+
import numpy.testing as npt
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import pytest
67

78
from rocketpy import Flight, HemisphericalParachute
@@ -447,7 +448,8 @@ def test_freestream_speed_at_apogee(example_plain_env, calisto):
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"""
448449
# NOTE: this rocket doesn't move in x or z direction. There's no wind.
449450
hard_atol = 1e-12
450-
soft_atol = 1e-6
451+
soft_atol = 1e-5
452+
soft_rtol = 1e-4
451453
test_flight = Flight(
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environment=example_plain_env,
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rocket=calisto,
@@ -458,25 +460,36 @@ def test_freestream_speed_at_apogee(example_plain_env, calisto):
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atol=13 * [hard_atol],
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)
460462

461-
assert np.isclose(
463+
npt.assert_allclose(
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test_flight.stream_velocity_x(test_flight.apogee_time),
463-
0.46415477243050873,
465+
0.4641507314747016,
464466
atol=hard_atol,
467+
rtol=soft_rtol,
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)
466-
assert np.isclose(
467-
test_flight.stream_velocity_y(test_flight.apogee_time), 0.0, atol=hard_atol
469+
npt.assert_allclose(
470+
test_flight.stream_velocity_y(test_flight.apogee_time),
471+
0.0,
472+
atol=hard_atol,
473+
rtol=soft_rtol,
468474
)
469475
# NOTE: stream_velocity_z has a higher error due to apogee detection estimation
470-
assert np.isclose(
471-
test_flight.stream_velocity_z(test_flight.apogee_time), 0.0, atol=soft_atol
476+
npt.assert_allclose(
477+
test_flight.stream_velocity_z(test_flight.apogee_time),
478+
0.0,
479+
atol=soft_atol,
480+
rtol=soft_rtol,
472481
)
473-
assert np.isclose(
482+
npt.assert_allclose(
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test_flight.free_stream_speed(test_flight.apogee_time),
475-
0.46415477243050873,
484+
0.46415073147558955,
476485
atol=hard_atol,
486+
rtol=soft_rtol,
477487
)
478-
assert np.isclose(
479-
test_flight.apogee_freestream_speed, 0.46415477243050873, atol=hard_atol
488+
npt.assert_allclose(
489+
test_flight.apogee_freestream_speed,
490+
0.46415073147558955,
491+
atol=hard_atol,
492+
rtol=soft_rtol,
480493
)
481494

482495

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