bury scipy for now

pull/1086/head
Harald Schafer 5 years ago
parent 9e6e1cba56
commit a8261c8017
  1. 2
      selfdrive/locationd/kalman/helpers/lst_sq_computer.py
  2. 6
      selfdrive/locationd/kalman/models/loc_kf.py

@ -3,8 +3,8 @@
import os import os
import numpy as np import numpy as np
import scipy.optimize as opt
import sympy as sp import sympy as sp
#import scipy.optimize as opt
import common.transformations.orientation as orient import common.transformations.orientation as orient
from selfdrive.locationd.kalman.helpers import (TEMPLATE_DIR, load_code, from selfdrive.locationd.kalman.helpers import (TEMPLATE_DIR, load_code,

@ -5,17 +5,18 @@ import os
import numpy as np import numpy as np
import sympy as sp import sympy as sp
from laika.constants import EARTH_GM
from laika.raw_gnss import GNSSMeasurement
from selfdrive.locationd.kalman.helpers import ObservationKind from selfdrive.locationd.kalman.helpers import ObservationKind
from selfdrive.locationd.kalman.helpers.ekf_sym import EKF_sym, gen_code from selfdrive.locationd.kalman.helpers.ekf_sym import EKF_sym, gen_code
from selfdrive.locationd.kalman.helpers.lst_sq_computer import LstSqComputer from selfdrive.locationd.kalman.helpers.lst_sq_computer import LstSqComputer
from selfdrive.locationd.kalman.helpers.sympy_helpers import (euler_rotate, from selfdrive.locationd.kalman.helpers.sympy_helpers import (euler_rotate,
quat_matrix_r, quat_matrix_r,
quat_rotate) quat_rotate)
#from laika.constants import EARTH_GM
EARTH_GM = 3.986005e14 # m^3/s^2 (gravitational constant * mass of earth)
def parse_prr(m): def parse_prr(m):
from laika.raw_gnss import GNSSMeasurement
sat_pos_vel_i = np.concatenate((m[GNSSMeasurement.SAT_POS], sat_pos_vel_i = np.concatenate((m[GNSSMeasurement.SAT_POS],
m[GNSSMeasurement.SAT_VEL])) m[GNSSMeasurement.SAT_VEL]))
R_i = np.atleast_2d(m[GNSSMeasurement.PRR_STD]**2) R_i = np.atleast_2d(m[GNSSMeasurement.PRR_STD]**2)
@ -24,6 +25,7 @@ def parse_prr(m):
def parse_pr(m): def parse_pr(m):
from laika.raw_gnss import GNSSMeasurement
pseudorange = m[GNSSMeasurement.PR] pseudorange = m[GNSSMeasurement.PR]
pseudorange_stdev = m[GNSSMeasurement.PR_STD] pseudorange_stdev = m[GNSSMeasurement.PR_STD]
sat_pos_freq_i = np.concatenate((m[GNSSMeasurement.SAT_POS], sat_pos_freq_i = np.concatenate((m[GNSSMeasurement.SAT_POS],

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