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.
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import numpy as np
"""
Coordinate transformation module. All methods accept arrays as input
with each row as a position.
"""
a = 6378137
b = 6356752.3142
esq = 6.69437999014 * 0.001
e1sq = 6.73949674228 * 0.001
def geodetic2ecef(geodetic):
geodetic = np.array(geodetic)
input_shape = geodetic.shape
geodetic = np.atleast_2d(geodetic)
lat = (np.pi/180)*geodetic[:,0]
lon = (np.pi/180)*geodetic[:,1]
alt = geodetic[:,2]
xi = np.sqrt(1 - esq * np.sin(lat)**2)
x = (a / xi + alt) * np.cos(lat) * np.cos(lon)
y = (a / xi + alt) * np.cos(lat) * np.sin(lon)
z = (a / xi * (1 - esq) + alt) * np.sin(lat)
ecef = np.array([x, y, z]).T
return ecef.reshape(input_shape)
def ecef2geodetic(ecef):
"""
Convert ECEF coordinates to geodetic using ferrari's method
"""
def ferrari(x, y, z):
# ferrari's method
r = np.sqrt(x * x + y * y)
Esq = a * a - b * b
F = 54 * b * b * z * z
G = r * r + (1 - esq) * z * z - esq * Esq
C = (esq * esq * F * r * r) / (pow(G, 3))
S = np.cbrt(1 + C + np.sqrt(C * C + 2 * C))
P = F / (3 * pow((S + 1 / S + 1), 2) * G * G)
Q = np.sqrt(1 + 2 * esq * esq * P)
r_0 = -(P * esq * r) / (1 + Q) + np.sqrt(0.5 * a * a*(1 + 1.0 / Q) - \
P * (1 - esq) * z * z / (Q * (1 + Q)) - 0.5 * P * r * r)
U = np.sqrt(pow((r - esq * r_0), 2) + z * z)
V = np.sqrt(pow((r - esq * r_0), 2) + (1 - esq) * z * z)
Z_0 = b * b * z / (a * V)
h = U * (1 - b * b / (a * V))
lat = (180/np.pi)*np.arctan((z + e1sq * Z_0) / r)
lon = (180/np.pi)*np.arctan2(y, x)
return lat, lon, h
geodetic = []
ecef = np.array(ecef)
input_shape = ecef.shape
ecef = np.atleast_2d(ecef)
for p in ecef:
geodetic.append(ferrari(*p))
geodetic = np.array(geodetic)
return geodetic.reshape(input_shape)
class LocalCoord(object):
"""
Allows conversions to local frames. In this case NED.
That is: North East Down from the start position in
meters.
"""
def __init__(self, init_geodetic, init_ecef):
self.init_ecef = init_ecef
lat, lon, _ = (np.pi/180)*init_geodetic
self.ned2ecef_matrix = np.array([[-np.sin(lat)*np.cos(lon), -np.sin(lon), -np.cos(lat)*np.cos(lon)],
[-np.sin(lat)*np.sin(lon), np.cos(lon), -np.cos(lat)*np.sin(lon)],
[np.cos(lat), 0, -np.sin(lat)]])
self.ecef2ned_matrix = self.ned2ecef_matrix.T
@classmethod
def from_geodetic(self, init_geodetic):
init_ecef = geodetic2ecef(init_geodetic)
return LocalCoord(init_geodetic, init_ecef)
@classmethod
def from_ecef(self, init_ecef):
init_geodetic = ecef2geodetic(init_ecef)
return LocalCoord(init_geodetic, init_ecef)
def ecef2ned(self, ecef):
return np.dot(self.ecef2ned_matrix, (ecef - self.init_ecef).T).T
def ned2ecef(self, ned):
# Transpose so that init_ecef will broadcast correctly for 1d or 2d ned.
return (np.dot(self.ned2ecef_matrix, ned.T).T + self.init_ecef)
def geodetic2ned(self, geodetic):
ecef = geodetic2ecef(geodetic)
return self.ecef2ned(ecef)
def ned2geodetic(self, ned):
ecef = self.ned2ecef(ned)
return ecef2geodetic(ecef)