openpilot is an open source driver assistance system. openpilot performs the functions of Automated Lane Centering and Adaptive Cruise Control for over 200 supported car makes and models.
You can not select more than 25 topics Topics must start with a letter or number, can include dashes ('-') and can be up to 35 characters long.
 
 
 
 
 
 

174 lines
5.4 KiB

# distutils: language = c++
# cython: language_level = 3
from common.transformations.transformations cimport Matrix3, Vector3, Quaternion
from common.transformations.transformations cimport ECEF, NED, Geodetic
from common.transformations.transformations cimport euler2quat as euler2quat_c
from common.transformations.transformations cimport quat2euler as quat2euler_c
from common.transformations.transformations cimport quat2rot as quat2rot_c
from common.transformations.transformations cimport rot2quat as rot2quat_c
from common.transformations.transformations cimport euler2rot as euler2rot_c
from common.transformations.transformations cimport rot2euler as rot2euler_c
from common.transformations.transformations cimport rot_matrix as rot_matrix_c
from common.transformations.transformations cimport ecef_euler_from_ned as ecef_euler_from_ned_c
from common.transformations.transformations cimport ned_euler_from_ecef as ned_euler_from_ecef_c
from common.transformations.transformations cimport geodetic2ecef as geodetic2ecef_c
from common.transformations.transformations cimport ecef2geodetic as ecef2geodetic_c
from common.transformations.transformations cimport LocalCoord_c
import cython
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