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Comma Device
2026-01-11 18:23:29 +08:00
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Reference Frames
------
Many reference frames are used throughout. This
folder contains all helper functions needed to
transform between them. Generally this is done
by generating a rotation matrix and multiplying.
| Name | [x, y, z] | Units | Notes |
| :-------------: |:-------------:| :-----:| :----: |
| Geodetic | [Latitude, Longitude, Altitude] | geodetic coordinates | Sometimes used as [lon, lat, alt], avoid this frame. |
| ECEF | [x, y, z] | meters | We use **ITRF14 (IGS14)**, NOT NAD83. <br> This is the global Mesh3D frame. |
| NED | [North, East, Down] | meters | Relative to earth's surface, useful for visualizing. |
| Device | [Forward, Right, Down] | meters | This is the Mesh3D local frame. <br> Relative to camera, **not imu.** <br> ![img](http://upload.wikimedia.org/wikipedia/commons/thumb/2/2f/RPY_angles_of_airplanes.png/440px-RPY_angles_of_airplanes.png)|
| Calibrated | [Forward, Right, Down] | meters | This is the frame the model outputs are in. <br> More details below. <br>|
| Car | [Forward, Right, Down] | meters | This is useful for estimating position of points on the road. <br> More details below. <br>|
| View | [Right, Down, Forward] | meters | Like device frame, but according to camera conventions. |
| Camera | [u, v, focal] | pixels | Like view frame, but 2d on the camera image.|
| Normalized Camera | [u / focal, v / focal, 1] | / | |
| Model | [u, v, focal] | pixels | The sampled rectangle of the full camera frame the model uses. |
| Normalized Model | [u / focal, v / focal, 1] | / | |
Orientation Conventions
------
Quaternions, rotation matrices and euler angles are three
equivalent representations of orientation and all three are
used throughout the code base.
For euler angles the preferred convention is [roll, pitch, yaw]
which corresponds to rotations around the [x, y, z] axes. All
euler angles should always be in radians or radians/s unless
for plotting or display purposes. For quaternions the hamilton
notations is preferred which is [q<sub>w</sub>, q<sub>x</sub>, q<sub>y</sub>, q<sub>z</sub>]. All quaternions
should always be normalized with a strictly positive q<sub>w</sub>. **These
quaternions are a unique representation of orientation whereas euler angles
or rotation matrices are not.**
To rotate from one frame into another with euler angles the
convention is to rotate around roll, then pitch and then yaw,
while rotating around the rotated axes, not the original axes.
Car frame
------
Device frame is aligned with the road-facing camera used by openpilot. However, when controlling the vehicle it is helpful to think in a reference frame aligned with the vehicle. These two reference frames can be different.
The orientation of car frame is defined to be aligned with the car's direction of travel and the road plane when the vehicle is driving on a flat road and not turning. The origin of car frame is defined to be directly below device frame (in car frame), such that it is on the road plane. The position and orientation of this frame is not necessarily always aligned with the direction of travel or the road plane due to suspension movements and other effects.
Calibrated frame
------
It is helpful for openpilot's driving model to take in images that look similar when mounted differently in different cars. To achieve this we "calibrate" the images by transforming it into calibrated frame. Calibrated frame is defined to be aligned with car frame in pitch and yaw, and aligned with device frame in roll. It also has the same origin as device frame.
Example
------
To transform global Mesh3D positions and orientations (positions_ecef, quats_ecef) into the local frame described by the
first position and orientation from Mesh3D one would do:
```
ecef_from_local = rot_from_quat(quats_ecef[0])
local_from_ecef = ecef_from_local.T
positions_local = np.einsum('ij,kj->ki', local_from_ecef, postions_ecef - positions_ecef[0])
rotations_global = rot_from_quat(quats_ecef)
rotations_local = np.einsum('ij,kjl->kil', local_from_ecef, rotations_global)
eulers_local = euler_from_rot(rotations_local)
```

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import itertools
import numpy as np
from dataclasses import dataclass
import openpilot.common.transformations.orientation as orient
## -- hardcoded hardware params --
@dataclass(frozen=True)
class CameraConfig:
width: int
height: int
focal_length: float
@property
def size(self):
return (self.width, self.height)
@property
def intrinsics(self):
# aka 'K' aka camera_frame_from_view_frame
return np.array([
[self.focal_length, 0.0, float(self.width)/2],
[0.0, self.focal_length, float(self.height)/2],
[0.0, 0.0, 1.0]
])
@property
def intrinsics_inv(self):
# aka 'K_inv' aka view_frame_from_camera_frame
return np.linalg.inv(self.intrinsics)
@dataclass(frozen=True)
class _NoneCameraConfig(CameraConfig):
width: int = 0
height: int = 0
focal_length: float = 0
@dataclass(frozen=True)
class DeviceCameraConfig:
fcam: CameraConfig
dcam: CameraConfig
ecam: CameraConfig
def all_cams(self):
for cam in ['fcam', 'dcam', 'ecam']:
if not isinstance(getattr(self, cam), _NoneCameraConfig):
yield cam, getattr(self, cam)
_ar_ox_fisheye = CameraConfig(1928, 1208, 567.0) # focal length probably wrong? magnification is not consistent across frame
_os_fisheye = CameraConfig(2688 // 2, 1520 // 2, 567.0 / 4 * 3)
_ar_ox_config = DeviceCameraConfig(CameraConfig(1928, 1208, 2648.0), _ar_ox_fisheye, _ar_ox_fisheye)
_os_config = DeviceCameraConfig(CameraConfig(2688 // 2, 1520 // 2, 1522.0 * 3 / 4), _os_fisheye, _os_fisheye)
_neo_config = DeviceCameraConfig(CameraConfig(1164, 874, 910.0), CameraConfig(816, 612, 650.0), _NoneCameraConfig())
DEVICE_CAMERAS = {
# A "device camera" is defined by a device type and sensor
# sensor type was never set on eon/neo/two
("neo", "unknown"): _neo_config,
# unknown here is AR0231, field was added with OX03C10 support
("tici", "unknown"): _ar_ox_config,
# before deviceState.deviceType was set, assume tici AR config
("unknown", "ar0231"): _ar_ox_config,
("unknown", "ox03c10"): _ar_ox_config,
# simulator (emulates a tici)
("pc", "unknown"): _ar_ox_config,
}
prods = itertools.product(('tici', 'tizi', 'mici'), (('ar0231', _ar_ox_config), ('ox03c10', _ar_ox_config), ('os04c10', _os_config)))
DEVICE_CAMERAS.update({(d, c[0]): c[1] for d, c in prods})
# device/mesh : x->forward, y-> right, z->down
# view : x->right, y->down, z->forward
device_frame_from_view_frame = np.array([
[ 0., 0., 1.],
[ 1., 0., 0.],
[ 0., 1., 0.]
])
view_frame_from_device_frame = device_frame_from_view_frame.T
# aka 'extrinsic_matrix'
# road : x->forward, y -> left, z->up
def get_view_frame_from_road_frame(roll, pitch, yaw, height):
device_from_road = orient.rot_from_euler([roll, pitch, yaw]).dot(np.diag([1, -1, -1]))
view_from_road = view_frame_from_device_frame.dot(device_from_road)
return np.hstack((view_from_road, [[0], [height], [0]]))
# aka 'extrinsic_matrix'
def get_view_frame_from_calib_frame(roll, pitch, yaw, height):
device_from_calib= orient.rot_from_euler([roll, pitch, yaw])
view_from_calib = view_frame_from_device_frame.dot(device_from_calib)
return np.hstack((view_from_calib, [[0], [height], [0]]))
def vp_from_ke(m):
"""
Computes the vanishing point from the product of the intrinsic and extrinsic
matrices C = KE.
The vanishing point is defined as lim x->infinity C (x, 0, 0, 1).T
"""
return (m[0, 0]/m[2, 0], m[1, 0]/m[2, 0])
def roll_from_ke(m):
# note: different from calibration.h/RollAnglefromKE: i think that one's just wrong
return np.arctan2(-(m[1, 0] - m[1, 1] * m[2, 0] / m[2, 1]),
-(m[0, 0] - m[0, 1] * m[2, 0] / m[2, 1]))
def normalize(img_pts, intrinsics):
# normalizes image coordinates
# accepts single pt or array of pts
intrinsics_inv = np.linalg.inv(intrinsics)
img_pts = np.array(img_pts)
input_shape = img_pts.shape
img_pts = np.atleast_2d(img_pts)
img_pts = np.hstack((img_pts, np.ones((img_pts.shape[0], 1))))
img_pts_normalized = img_pts.dot(intrinsics_inv.T)
img_pts_normalized[(img_pts < 0).any(axis=1)] = np.nan
return img_pts_normalized[:, :2].reshape(input_shape)
def denormalize(img_pts, intrinsics, width=np.inf, height=np.inf):
# denormalizes image coordinates
# accepts single pt or array of pts
img_pts = np.array(img_pts)
input_shape = img_pts.shape
img_pts = np.atleast_2d(img_pts)
img_pts = np.hstack((img_pts, np.ones((img_pts.shape[0], 1), dtype=img_pts.dtype)))
img_pts_denormalized = img_pts.dot(intrinsics.T)
if np.isfinite(width):
img_pts_denormalized[img_pts_denormalized[:, 0] > width] = np.nan
img_pts_denormalized[img_pts_denormalized[:, 0] < 0] = np.nan
if np.isfinite(height):
img_pts_denormalized[img_pts_denormalized[:, 1] > height] = np.nan
img_pts_denormalized[img_pts_denormalized[:, 1] < 0] = np.nan
return img_pts_denormalized[:, :2].reshape(input_shape)
def get_calib_from_vp(vp, intrinsics):
vp_norm = normalize(vp, intrinsics)
yaw_calib = np.arctan(vp_norm[0])
pitch_calib = -np.arctan(vp_norm[1]*np.cos(yaw_calib))
roll_calib = 0
return roll_calib, pitch_calib, yaw_calib
def device_from_ecef(pos_ecef, orientation_ecef, pt_ecef):
# device from ecef frame
# device frame is x -> forward, y-> right, z -> down
# accepts single pt or array of pts
input_shape = pt_ecef.shape
pt_ecef = np.atleast_2d(pt_ecef)
ecef_from_device_rot = orient.rotations_from_quats(orientation_ecef)
device_from_ecef_rot = ecef_from_device_rot.T
pt_ecef_rel = pt_ecef - pos_ecef
pt_device = np.einsum('jk,ik->ij', device_from_ecef_rot, pt_ecef_rel)
return pt_device.reshape(input_shape)
def img_from_device(pt_device):
# img coordinates from pts in device frame
# first transforms to view frame, then to img coords
# accepts single pt or array of pts
input_shape = pt_device.shape
pt_device = np.atleast_2d(pt_device)
pt_view = np.einsum('jk,ik->ij', view_frame_from_device_frame, pt_device)
# This function should never return negative depths
pt_view[pt_view[:, 2] < 0] = np.nan
pt_img = pt_view/pt_view[:, 2:3]
return pt_img.reshape(input_shape)[:, :2]

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#pragma once
#include <eigen3/Eigen/Dense>
#define DEG2RAD(x) ((x) * M_PI / 180.0)
#define RAD2DEG(x) ((x) * 180.0 / M_PI)
struct ECEF {
double x, y, z;
Eigen::Vector3d to_vector() const {
return Eigen::Vector3d(x, y, z);
}
};
struct NED {
double n, e, d;
Eigen::Vector3d to_vector() const {
return Eigen::Vector3d(n, e, d);
}
};
struct Geodetic {
double lat, lon, alt;
bool radians=false;
};
ECEF geodetic2ecef(const Geodetic &g);
Geodetic ecef2geodetic(const ECEF &e);
class LocalCoord {
public:
Eigen::Matrix3d ned2ecef_matrix;
Eigen::Matrix3d ecef2ned_matrix;
Eigen::Vector3d init_ecef;
LocalCoord(const Geodetic &g, const ECEF &e);
LocalCoord(const Geodetic &g) : LocalCoord(g, ::geodetic2ecef(g)) {}
LocalCoord(const ECEF &e) : LocalCoord(::ecef2geodetic(e), e) {}
NED ecef2ned(const ECEF &e);
ECEF ned2ecef(const NED &n);
NED geodetic2ned(const Geodetic &g);
Geodetic ned2geodetic(const NED &n);
};

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from openpilot.common.transformations.orientation import numpy_wrap
from openpilot.common.transformations.transformations import (ecef2geodetic_single,
geodetic2ecef_single)
from openpilot.common.transformations.transformations import LocalCoord as LocalCoord_single
class LocalCoord(LocalCoord_single):
ecef2ned = numpy_wrap(LocalCoord_single.ecef2ned_single, (3,), (3,))
ned2ecef = numpy_wrap(LocalCoord_single.ned2ecef_single, (3,), (3,))
geodetic2ned = numpy_wrap(LocalCoord_single.geodetic2ned_single, (3,), (3,))
ned2geodetic = numpy_wrap(LocalCoord_single.ned2geodetic_single, (3,), (3,))
geodetic2ecef = numpy_wrap(geodetic2ecef_single, (3,), (3,))
ecef2geodetic = numpy_wrap(ecef2geodetic_single, (3,), (3,))
geodetic_from_ecef = ecef2geodetic
ecef_from_geodetic = geodetic2ecef

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import numpy as np
from openpilot.common.transformations.orientation import rot_from_euler
from openpilot.common.transformations.camera import get_view_frame_from_calib_frame, view_frame_from_device_frame, _ar_ox_fisheye
# segnet
SEGNET_SIZE = (512, 384)
# MED model
MEDMODEL_INPUT_SIZE = (512, 256)
MEDMODEL_YUV_SIZE = (MEDMODEL_INPUT_SIZE[0], MEDMODEL_INPUT_SIZE[1] * 3 // 2)
MEDMODEL_CY = 47.6
medmodel_fl = 910.0
medmodel_intrinsics = np.array([
[medmodel_fl, 0.0, 0.5 * MEDMODEL_INPUT_SIZE[0]],
[0.0, medmodel_fl, MEDMODEL_CY],
[0.0, 0.0, 1.0]])
# BIG model
BIGMODEL_INPUT_SIZE = (1024, 512)
BIGMODEL_YUV_SIZE = (BIGMODEL_INPUT_SIZE[0], BIGMODEL_INPUT_SIZE[1] * 3 // 2)
bigmodel_fl = 910.0
bigmodel_intrinsics = np.array([
[bigmodel_fl, 0.0, 0.5 * BIGMODEL_INPUT_SIZE[0]],
[0.0, bigmodel_fl, 256 + MEDMODEL_CY],
[0.0, 0.0, 1.0]])
# SBIG model (big model with the size of small model)
SBIGMODEL_INPUT_SIZE = (512, 256)
SBIGMODEL_YUV_SIZE = (SBIGMODEL_INPUT_SIZE[0], SBIGMODEL_INPUT_SIZE[1] * 3 // 2)
sbigmodel_fl = 455.0
sbigmodel_intrinsics = np.array([
[sbigmodel_fl, 0.0, 0.5 * SBIGMODEL_INPUT_SIZE[0]],
[0.0, sbigmodel_fl, 0.5 * (256 + MEDMODEL_CY)],
[0.0, 0.0, 1.0]])
DM_INPUT_SIZE = (1440, 960)
dmonitoringmodel_fl = _ar_ox_fisheye.focal_length
dmonitoringmodel_intrinsics = np.array([
[dmonitoringmodel_fl, 0.0, DM_INPUT_SIZE[0]/2],
[0.0, dmonitoringmodel_fl, DM_INPUT_SIZE[1]/2 - (_ar_ox_fisheye.height - DM_INPUT_SIZE[1])/2],
[0.0, 0.0, 1.0]])
bigmodel_frame_from_calib_frame = np.dot(bigmodel_intrinsics,
get_view_frame_from_calib_frame(0, 0, 0, 0))
sbigmodel_frame_from_calib_frame = np.dot(sbigmodel_intrinsics,
get_view_frame_from_calib_frame(0, 0, 0, 0))
medmodel_frame_from_calib_frame = np.dot(medmodel_intrinsics,
get_view_frame_from_calib_frame(0, 0, 0, 0))
medmodel_frame_from_bigmodel_frame = np.dot(medmodel_intrinsics, np.linalg.inv(bigmodel_intrinsics))
calib_from_medmodel = np.linalg.inv(medmodel_frame_from_calib_frame[:, :3])
calib_from_sbigmodel = np.linalg.inv(sbigmodel_frame_from_calib_frame[:, :3])
# This function is verified to give similar results to xx.uncommon.utils.transform_img
def get_warp_matrix(device_from_calib_euler: np.ndarray, intrinsics: np.ndarray, bigmodel_frame: bool = False) -> np.ndarray:
calib_from_model = calib_from_sbigmodel if bigmodel_frame else calib_from_medmodel
device_from_calib = rot_from_euler(device_from_calib_euler)
camera_from_calib = intrinsics @ view_frame_from_device_frame @ device_from_calib
warp_matrix: np.ndarray = camera_from_calib @ calib_from_model
return warp_matrix

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#pragma once
#include <eigen3/Eigen/Dense>
#include "common/transformations/coordinates.hpp"
Eigen::Quaterniond ensure_unique(const Eigen::Quaterniond &quat);
Eigen::Quaterniond euler2quat(const Eigen::Vector3d &euler);
Eigen::Vector3d quat2euler(const Eigen::Quaterniond &quat);
Eigen::Matrix3d quat2rot(const Eigen::Quaterniond &quat);
Eigen::Quaterniond rot2quat(const Eigen::Matrix3d &rot);
Eigen::Matrix3d euler2rot(const Eigen::Vector3d &euler);
Eigen::Vector3d rot2euler(const Eigen::Matrix3d &rot);
Eigen::Matrix3d rot_matrix(double roll, double pitch, double yaw);
Eigen::Matrix3d rot(const Eigen::Vector3d &axis, double angle);
Eigen::Vector3d ecef_euler_from_ned(const ECEF &ecef_init, const Eigen::Vector3d &ned_pose);
Eigen::Vector3d ned_euler_from_ecef(const ECEF &ecef_init, const Eigen::Vector3d &ecef_pose);

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import numpy as np
from collections.abc import Callable
from openpilot.common.transformations.transformations import (ecef_euler_from_ned_single,
euler2quat_single,
euler2rot_single,
ned_euler_from_ecef_single,
quat2euler_single,
quat2rot_single,
rot2euler_single,
rot2quat_single)
def numpy_wrap(function, input_shape, output_shape) -> Callable[..., np.ndarray]:
"""Wrap a function to take either an input or list of inputs and return the correct shape"""
def f(*inps):
*args, inp = inps
inp = np.array(inp)
shape = inp.shape
if len(shape) == len(input_shape):
out_shape = output_shape
else:
out_shape = (shape[0],) + output_shape
# Add empty dimension if inputs is not a list
if len(shape) == len(input_shape):
inp.shape = (1, ) + inp.shape
result = np.asarray([function(*args, i) for i in inp])
result.shape = out_shape
return result
return f
euler2quat = numpy_wrap(euler2quat_single, (3,), (4,))
quat2euler = numpy_wrap(quat2euler_single, (4,), (3,))
quat2rot = numpy_wrap(quat2rot_single, (4,), (3, 3))
rot2quat = numpy_wrap(rot2quat_single, (3, 3), (4,))
euler2rot = numpy_wrap(euler2rot_single, (3,), (3, 3))
rot2euler = numpy_wrap(rot2euler_single, (3, 3), (3,))
ecef_euler_from_ned = numpy_wrap(ecef_euler_from_ned_single, (3,), (3,))
ned_euler_from_ecef = numpy_wrap(ned_euler_from_ecef_single, (3,), (3,))
quats_from_rotations = rot2quat
quat_from_rot = rot2quat
rotations_from_quats = quat2rot
rot_from_quat = quat2rot
euler_from_rot = rot2euler
euler_from_quat = quat2euler
rot_from_euler = euler2rot
quat_from_euler = euler2quat

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import numpy as np
import openpilot.common.transformations.coordinates as coord
geodetic_positions = np.array([[37.7610403, -122.4778699, 115],
[27.4840915, -68.5867592, 2380],
[32.4916858, -113.652821, -6],
[15.1392514, 103.6976037, 24],
[24.2302229, 44.2835412, 1650]])
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 ]])
ecef_positions_offset = np.array([[-2711004.46961115, -4259099.33540613, 3884605.16002147],
[ 2068074.30639499, -5273413.78835412, 2927012.48741131],
[-2160344.53748176, -4932586.20092211, 3406636.2962545 ],
[-1458211.98517094, 5983151.11161276, 1655077.02698447],
[ 4167271.20055269, 4064398.22619263, 2602238.95265847]])
ned_offsets = np.array([[78.722153649976391, 24.396208657446344, 60.343017506838436],
[10.699003365155221, 37.319278617604269, 4.1084100025050407],
[95.282646251726959, 61.266689955574428, -25.376506058505054],
[68.535769283630003, -56.285970011848889, -100.54840137956515],
[-33.066609321880179, 46.549821994306861, -84.062540548335591]])
ecef_init_batch = np.array([2068042.69652729, -5273435.40316622, 2927004.89190746])
ecef_positions_offset_batch = np.array([[ 2068089.41454771, -5273434.46829148, 2927074.04783672],
[ 2068103.31628647, -5273393.92275431, 2927102.08725987],
[ 2068108.49939636, -5273359.27047121, 2927045.07091581],
[ 2068075.12395611, -5273381.69432566, 2927041.08207992],
[ 2068060.72033399, -5273430.6061505, 2927094.54928305]])
ned_offsets_batch = np.array([[ 53.88103168, 43.83445935, -46.27488057],
[ 93.83378995, 71.57943024, -30.23113187],
[ 57.26725796, 89.05602684, 23.02265814],
[ 49.71775195, 49.79767572, 17.15351015],
[ 78.56272609, 18.53100158, -43.25290759]])
class TestNED:
def test_small_distances(self):
start_geodetic = np.array([33.8042184, -117.888593, 0.0])
local_coord = coord.LocalCoord.from_geodetic(start_geodetic)
start_ned = local_coord.geodetic2ned(start_geodetic)
np.testing.assert_array_equal(start_ned, np.zeros(3,))
west_geodetic = start_geodetic + [0, -0.0005, 0]
west_ned = local_coord.geodetic2ned(west_geodetic)
assert np.abs(west_ned[0]) < 1e-3
assert west_ned[1] < 0
southwest_geodetic = start_geodetic + [-0.0005, -0.002, 0]
southwest_ned = local_coord.geodetic2ned(southwest_geodetic)
assert southwest_ned[0] < 0
assert southwest_ned[1] < 0
def test_ecef_geodetic(self):
# testing single
np.testing.assert_allclose(ecef_positions[0], coord.geodetic2ecef(geodetic_positions[0]), rtol=1e-9)
np.testing.assert_allclose(geodetic_positions[0, :2], coord.ecef2geodetic(ecef_positions[0])[:2], rtol=1e-9)
np.testing.assert_allclose(geodetic_positions[0, 2], coord.ecef2geodetic(ecef_positions[0])[2], rtol=1e-9, atol=1e-4)
np.testing.assert_allclose(geodetic_positions[:, :2], coord.ecef2geodetic(ecef_positions)[:, :2], rtol=1e-9)
np.testing.assert_allclose(geodetic_positions[:, 2], coord.ecef2geodetic(ecef_positions)[:, 2], rtol=1e-9, atol=1e-4)
np.testing.assert_allclose(ecef_positions, coord.geodetic2ecef(geodetic_positions), rtol=1e-9)
def test_ned(self):
for ecef_pos in ecef_positions:
converter = coord.LocalCoord.from_ecef(ecef_pos)
ecef_pos_moved = ecef_pos + [25, -25, 25]
ecef_pos_moved_double_converted = converter.ned2ecef(converter.ecef2ned(ecef_pos_moved))
np.testing.assert_allclose(ecef_pos_moved, ecef_pos_moved_double_converted, rtol=1e-9)
for geo_pos in geodetic_positions:
converter = coord.LocalCoord.from_geodetic(geo_pos)
geo_pos_moved = geo_pos + np.array([0, 0, 10])
geo_pos_double_converted_moved = converter.ned2geodetic(converter.geodetic2ned(geo_pos) + np.array([0, 0, -10]))
np.testing.assert_allclose(geo_pos_moved[:2], geo_pos_double_converted_moved[:2], rtol=1e-9, atol=1e-6)
np.testing.assert_allclose(geo_pos_moved[2], geo_pos_double_converted_moved[2], rtol=1e-9, atol=1e-4)
def test_ned_saved_results(self):
for i, ecef_pos in enumerate(ecef_positions):
converter = coord.LocalCoord.from_ecef(ecef_pos)
np.testing.assert_allclose(converter.ned2ecef(ned_offsets[i]),
ecef_positions_offset[i],
rtol=1e-9, atol=1e-4)
np.testing.assert_allclose(converter.ecef2ned(ecef_positions_offset[i]),
ned_offsets[i],
rtol=1e-9, atol=1e-4)
def test_ned_batch(self):
converter = coord.LocalCoord.from_ecef(ecef_init_batch)
np.testing.assert_allclose(converter.ecef2ned(ecef_positions_offset_batch),
ned_offsets_batch,
rtol=1e-9, atol=1e-7)
np.testing.assert_allclose(converter.ned2ecef(ned_offsets_batch),
ecef_positions_offset_batch,
rtol=1e-9, atol=1e-7)

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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)

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# cython: language_level=3
from libcpp cimport bool
cdef extern from "orientation.cc":
pass
cdef extern from "orientation.hpp":
cdef cppclass Quaternion "Eigen::Quaterniond":
Quaternion()
Quaternion(double, double, double, double)
double w()
double x()
double y()
double z()
cdef cppclass Vector3 "Eigen::Vector3d":
Vector3()
Vector3(double, double, double)
double operator()(int)
cdef cppclass Matrix3 "Eigen::Matrix3d":
Matrix3()
Matrix3(double*)
double operator()(int, int)
Quaternion euler2quat(const Vector3 &)
Vector3 quat2euler(const Quaternion &)
Matrix3 quat2rot(const Quaternion &)
Quaternion rot2quat(const Matrix3 &)
Vector3 rot2euler(const Matrix3 &)
Matrix3 euler2rot(const Vector3 &)
Matrix3 rot_matrix(double, double, double)
Vector3 ecef_euler_from_ned(const ECEF &, const Vector3 &)
Vector3 ned_euler_from_ecef(const ECEF &, const Vector3 &)
cdef extern from "coordinates.cc":
cdef struct ECEF:
double x
double y
double z
cdef struct NED:
double n
double e
double d
cdef struct Geodetic:
double lat
double lon
double alt
bool radians
ECEF geodetic2ecef(const Geodetic &)
Geodetic ecef2geodetic(const ECEF &)
cdef cppclass LocalCoord_c "LocalCoord":
Matrix3 ned2ecef_matrix
Matrix3 ecef2ned_matrix
LocalCoord_c(const Geodetic &, const ECEF &)
LocalCoord_c(const Geodetic &)
LocalCoord_c(const ECEF &)
NED ecef2ned(const ECEF &)
ECEF ned2ecef(const NED &)
NED geodetic2ned(const Geodetic &)
Geodetic ned2geodetic(const NED &)
cdef extern from "coordinates.hpp":
pass

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# distutils: language = c++
# cython: language_level = 3
from openpilot.common.transformations.transformations cimport Matrix3, Vector3, Quaternion
from openpilot.common.transformations.transformations cimport ECEF, NED, Geodetic
from openpilot.common.transformations.transformations cimport euler2quat as euler2quat_c
from openpilot.common.transformations.transformations cimport quat2euler as quat2euler_c
from openpilot.common.transformations.transformations cimport quat2rot as quat2rot_c
from openpilot.common.transformations.transformations cimport rot2quat as rot2quat_c
from openpilot.common.transformations.transformations cimport euler2rot as euler2rot_c
from openpilot.common.transformations.transformations cimport rot2euler as rot2euler_c
from openpilot.common.transformations.transformations cimport rot_matrix as rot_matrix_c
from openpilot.common.transformations.transformations cimport ecef_euler_from_ned as ecef_euler_from_ned_c
from openpilot.common.transformations.transformations cimport ned_euler_from_ecef as ned_euler_from_ecef_c
from openpilot.common.transformations.transformations cimport geodetic2ecef as geodetic2ecef_c
from openpilot.common.transformations.transformations cimport ecef2geodetic as ecef2geodetic_c
from openpilot.common.transformations.transformations cimport LocalCoord_c
import numpy as np
cimport numpy as np
cdef np.ndarray[double, ndim=2] matrix2numpy(Matrix3 m):
return np.array([
[m(0, 0), m(0, 1), m(0, 2)],
[m(1, 0), m(1, 1), m(1, 2)],
[m(2, 0), m(2, 1), m(2, 2)],
])
cdef Matrix3 numpy2matrix(np.ndarray[double, ndim=2, mode="fortran"] m):
assert m.shape[0] == 3
assert m.shape[1] == 3
return Matrix3(<double*>m.data)
cdef ECEF list2ecef(ecef):
cdef ECEF e
e.x = ecef[0]
e.y = ecef[1]
e.z = ecef[2]
return e
cdef NED list2ned(ned):
cdef NED n
n.n = ned[0]
n.e = ned[1]
n.d = ned[2]
return n
cdef Geodetic list2geodetic(geodetic):
cdef Geodetic g
g.lat = geodetic[0]
g.lon = geodetic[1]
g.alt = geodetic[2]
return g
def euler2quat_single(euler):
cdef Vector3 e = Vector3(euler[0], euler[1], euler[2])
cdef Quaternion q = euler2quat_c(e)
return [q.w(), q.x(), q.y(), q.z()]
def quat2euler_single(quat):
cdef Quaternion q = Quaternion(quat[0], quat[1], quat[2], quat[3])
cdef Vector3 e = quat2euler_c(q)
return [e(0), e(1), e(2)]
def quat2rot_single(quat):
cdef Quaternion q = Quaternion(quat[0], quat[1], quat[2], quat[3])
cdef Matrix3 r = quat2rot_c(q)
return matrix2numpy(r)
def rot2quat_single(rot):
cdef Matrix3 r = numpy2matrix(np.asfortranarray(rot, dtype=np.double))
cdef Quaternion q = rot2quat_c(r)
return [q.w(), q.x(), q.y(), q.z()]
def euler2rot_single(euler):
cdef Vector3 e = Vector3(euler[0], euler[1], euler[2])
cdef Matrix3 r = euler2rot_c(e)
return matrix2numpy(r)
def rot2euler_single(rot):
cdef Matrix3 r = numpy2matrix(np.asfortranarray(rot, dtype=np.double))
cdef Vector3 e = rot2euler_c(r)
return [e(0), e(1), e(2)]
def rot_matrix(roll, pitch, yaw):
return matrix2numpy(rot_matrix_c(roll, pitch, yaw))
def ecef_euler_from_ned_single(ecef_init, ned_pose):
cdef ECEF init = list2ecef(ecef_init)
cdef Vector3 pose = Vector3(ned_pose[0], ned_pose[1], ned_pose[2])
cdef Vector3 e = ecef_euler_from_ned_c(init, pose)
return [e(0), e(1), e(2)]
def ned_euler_from_ecef_single(ecef_init, ecef_pose):
cdef ECEF init = list2ecef(ecef_init)
cdef Vector3 pose = Vector3(ecef_pose[0], ecef_pose[1], ecef_pose[2])
cdef Vector3 e = ned_euler_from_ecef_c(init, pose)
return [e(0), e(1), e(2)]
def geodetic2ecef_single(geodetic):
cdef Geodetic g = list2geodetic(geodetic)
cdef ECEF e = geodetic2ecef_c(g)
return [e.x, e.y, e.z]
def ecef2geodetic_single(ecef):
cdef ECEF e = list2ecef(ecef)
cdef Geodetic g = ecef2geodetic_c(e)
return [g.lat, g.lon, g.alt]
cdef class LocalCoord:
cdef LocalCoord_c * lc
def __init__(self, geodetic=None, ecef=None):
assert (geodetic is not None) or (ecef is not None)
if geodetic is not None:
self.lc = new LocalCoord_c(list2geodetic(geodetic))
elif ecef is not None:
self.lc = new LocalCoord_c(list2ecef(ecef))
@property
def ned2ecef_matrix(self):
return matrix2numpy(self.lc.ned2ecef_matrix)
@property
def ecef2ned_matrix(self):
return matrix2numpy(self.lc.ecef2ned_matrix)
@property
def ned_from_ecef_matrix(self):
return self.ecef2ned_matrix
@property
def ecef_from_ned_matrix(self):
return self.ned2ecef_matrix
@classmethod
def from_geodetic(cls, geodetic):
return cls(geodetic=geodetic)
@classmethod
def from_ecef(cls, ecef):
return cls(ecef=ecef)
def ecef2ned_single(self, ecef):
assert self.lc
cdef ECEF e = list2ecef(ecef)
cdef NED n = self.lc.ecef2ned(e)
return [n.n, n.e, n.d]
def ned2ecef_single(self, ned):
assert self.lc
cdef NED n = list2ned(ned)
cdef ECEF e = self.lc.ned2ecef(n)
return [e.x, e.y, e.z]
def geodetic2ned_single(self, geodetic):
assert self.lc
cdef Geodetic g = list2geodetic(geodetic)
cdef NED n = self.lc.geodetic2ned(g)
return [n.n, n.e, n.d]
def ned2geodetic_single(self, ned):
assert self.lc
cdef NED n = list2ned(ned)
cdef Geodetic g = self.lc.ned2geodetic(n)
return [g.lat, g.lon, g.alt]
def __dealloc__(self):
del self.lc

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