mirror of
https://github.com/sunnypilot/sunnypilot.git
synced 2026-02-19 06:33:57 +08:00
76a465e0ec
* locationd at 20hz
* update ref
* bump cereal
* dont modify global state
* add scons files
* ecef2geodetic and geodetic2ecef
* Finish local coords class
* Add header file
* Add orientation.cc
* cleanup
* Add functions to header file
* Add cython wrapper
* y u no work?
* This passes the tests
* test rot2quat and quat2rot
* Teste euler2rot and rot2euler
* rot_matrix
* test ecef_euler_from_ned and ned_euler_from_ecef
* add benchmark
* Add test
* Consistent newlines
* no more radians supported in geodetic
* test localcoord single
* test localcoord single
* all tests pass
* Unused import
* Add alternate namings
* Add source for formulas
* no explicit tests needed
* remove benchmark
* Add release files
* Typo
* Remove print statement
* no access to raw transform matrix
* temporarily add tolerance
* handcode quat2euler
* update ref
old-commit-hash: c18e7da3c2
69 lines
3.3 KiB
Python
Executable File
69 lines
3.3 KiB
Python
Executable File
#!/usr/bin/env python3
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import numpy as np
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import unittest
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from common.transformations.orientation import euler2quat, quat2euler, euler2rot, rot2euler, \
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rot2quat, quat2rot, \
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ned_euler_from_ecef
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eulers = np.array([[ 1.46520501, 2.78688383, 2.92780854],
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[ 4.86909526, 3.60618161, 4.30648981],
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[ 3.72175965, 2.68763705, 5.43895988],
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[ 5.92306687, 5.69573614, 0.81100357],
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[ 0.67838374, 5.02402037, 2.47106426]])
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quats = np.array([[ 0.66855182, -0.71500939, 0.19539353, 0.06017818],
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[ 0.43163717, 0.70013301, 0.28209145, 0.49389021],
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[ 0.44121991, -0.08252646, 0.34257534, 0.82532207],
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[ 0.88578382, -0.04515356, -0.32936046, 0.32383617],
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[ 0.06578165, 0.61282835, 0.07126891, 0.78424163]])
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ecef_positions = np.array([[-2711076.55270557, -4259167.14692758, 3884579.87669935],
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[ 2068042.69652729, -5273435.40316622, 2927004.89190746],
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[-2160412.60461669, -4932588.89873832, 3406542.29652851],
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[-1458247.92550567, 5983060.87496612, 1654984.6099885 ],
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[ 4167239.10867871, 4064301.90363223, 2602234.6065749 ]])
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ned_eulers = np.array([[ 0.46806039, -0.4881889 , 1.65697808],
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[-2.14525969, -0.36533066, 0.73813479],
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[-1.39523364, -0.58540761, -1.77376356],
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[-1.84220435, 0.61828016, -1.03310421],
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[ 2.50450101, 0.36304151, 0.33136365]])
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class TestOrientation(unittest.TestCase):
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def test_quat_euler(self):
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for i, eul in enumerate(eulers):
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np.testing.assert_allclose(quats[i], euler2quat(eul), rtol=1e-7)
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np.testing.assert_allclose(quats[i], euler2quat(quat2euler(quats[i])), rtol=1e-6)
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for i, eul in enumerate(eulers):
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np.testing.assert_allclose(quats[i], euler2quat(list(eul)), rtol=1e-7)
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np.testing.assert_allclose(quats[i], euler2quat(quat2euler(list(quats[i]))), rtol=1e-6)
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np.testing.assert_allclose(quats, euler2quat(eulers), rtol=1e-7)
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np.testing.assert_allclose(quats, euler2quat(quat2euler(quats)), rtol=1e-6)
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def test_rot_euler(self):
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for eul in eulers:
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np.testing.assert_allclose(euler2quat(eul), euler2quat(rot2euler(euler2rot(eul))), rtol=1e-7)
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for eul in eulers:
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np.testing.assert_allclose(euler2quat(eul), euler2quat(rot2euler(euler2rot(list(eul)))), rtol=1e-7)
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np.testing.assert_allclose(euler2quat(eulers), euler2quat(rot2euler(euler2rot(eulers))), rtol=1e-7)
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def test_rot_quat(self):
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for quat in quats:
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np.testing.assert_allclose(quat, rot2quat(quat2rot(quat)), rtol=1e-7)
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for quat in quats:
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np.testing.assert_allclose(quat, rot2quat(quat2rot(list(quat))), rtol=1e-7)
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np.testing.assert_allclose(quats, rot2quat(quat2rot(quats)), rtol=1e-7)
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def test_euler_ned(self):
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for i in range(len(eulers)):
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np.testing.assert_allclose(ned_eulers[i], ned_euler_from_ecef(ecef_positions[i], eulers[i]), rtol=1e-7)
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#np.testing.assert_allclose(eulers[i], ecef_euler_from_ned(ecef_positions[i], ned_eulers[i]), rtol=1e-7)
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# np.testing.assert_allclose(ned_eulers, ned_euler_from_ecef(ecef_positions, eulers), rtol=1e-7)
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if __name__ == "__main__":
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unittest.main()
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