Validating Orientation Transformation Functions in OpenPilot
This test suite validates orientation transformation functions in the OpenPilot system, focusing on conversions between Euler angles, quaternions, and rotation matrices. It ensures accurate coordinate transformations for vehicle positioning and navigation.
Test Coverage Overview
Implementation Analysis
Technical Details
Best Practices Demonstrated
commaai/openpilot
common/transformations/tests/test_orientation.py
import numpy as np
from openpilot.common.transformations.orientation import euler2quat, quat2euler, euler2rot, rot2euler, \
rot2quat, quat2rot, \
ned_euler_from_ecef
eulers = np.array([[ 1.46520501, 2.78688383, 2.92780854],
[ 4.86909526, 3.60618161, 4.30648981],
[ 3.72175965, 2.68763705, 5.43895988],
[ 5.92306687, 5.69573614, 0.81100357],
[ 0.67838374, 5.02402037, 2.47106426]])
quats = np.array([[ 0.66855182, -0.71500939, 0.19539353, 0.06017818],
[ 0.43163717, 0.70013301, 0.28209145, 0.49389021],
[ 0.44121991, -0.08252646, 0.34257534, 0.82532207],
[ 0.88578382, -0.04515356, -0.32936046, 0.32383617],
[ 0.06578165, 0.61282835, 0.07126891, 0.78424163]])
ecef_positions = np.array([[-2711076.55270557, -4259167.14692758, 3884579.87669935],
[ 2068042.69652729, -5273435.40316622, 2927004.89190746],
[-2160412.60461669, -4932588.89873832, 3406542.29652851],
[-1458247.92550567, 5983060.87496612, 1654984.6099885 ],
[ 4167239.10867871, 4064301.90363223, 2602234.6065749 ]])
ned_eulers = np.array([[ 0.46806039, -0.4881889 , 1.65697808],
[-2.14525969, -0.36533066, 0.73813479],
[-1.39523364, -0.58540761, -1.77376356],
[-1.84220435, 0.61828016, -1.03310421],
[ 2.50450101, 0.36304151, 0.33136365]])
class TestOrientation:
def test_quat_euler(self):
for i, eul in enumerate(eulers):
np.testing.assert_allclose(quats[i], euler2quat(eul), rtol=1e-7)
np.testing.assert_allclose(quats[i], euler2quat(quat2euler(quats[i])), rtol=1e-6)
for i, eul in enumerate(eulers):
np.testing.assert_allclose(quats[i], euler2quat(list(eul)), rtol=1e-7)
np.testing.assert_allclose(quats[i], euler2quat(quat2euler(list(quats[i]))), rtol=1e-6)
np.testing.assert_allclose(quats, euler2quat(eulers), rtol=1e-7)
np.testing.assert_allclose(quats, euler2quat(quat2euler(quats)), rtol=1e-6)
def test_rot_euler(self):
for eul in eulers:
np.testing.assert_allclose(euler2quat(eul), euler2quat(rot2euler(euler2rot(eul))), rtol=1e-7)
for eul in eulers:
np.testing.assert_allclose(euler2quat(eul), euler2quat(rot2euler(euler2rot(list(eul)))), rtol=1e-7)
np.testing.assert_allclose(euler2quat(eulers), euler2quat(rot2euler(euler2rot(eulers))), rtol=1e-7)
def test_rot_quat(self):
for quat in quats:
np.testing.assert_allclose(quat, rot2quat(quat2rot(quat)), rtol=1e-7)
for quat in quats:
np.testing.assert_allclose(quat, rot2quat(quat2rot(list(quat))), rtol=1e-7)
np.testing.assert_allclose(quats, rot2quat(quat2rot(quats)), rtol=1e-7)
def test_euler_ned(self):
for i in range(len(eulers)):
np.testing.assert_allclose(ned_eulers[i], ned_euler_from_ecef(ecef_positions[i], eulers[i]), rtol=1e-7)
#np.testing.assert_allclose(eulers[i], ecef_euler_from_ned(ecef_positions[i], ned_eulers[i]), rtol=1e-7)
# np.testing.assert_allclose(ned_eulers, ned_euler_from_ecef(ecef_positions, eulers), rtol=1e-7)