def ahrs():
#print('')
imu = IMU(verbose=False)
header = 47
#print('-'*header)
#print("| {:20} | {:20} |".format("Accels [g's]", "Orient(r,p,h) [deg]"))
#print('-'*header)
fall = False
#for _ in range(10):
a, m, g = imu.get() # get data from nxp-9dof fxos8700 + fxas21002
r, p, h = imu.getOrientation(
a, m) # convert sensor data to angle in roll,pitch,yaw axis
#print the angle data
#print('| {:>6.1f} {:>6.1f} {:>6.1f} | {:>6.1f} {:>6.1f} {:>6.1f} |'.format(a[0], a[1], a[2], r, p, h))
time.sleep(1)
r = abs(r)
p = abs(p)
#h =abs(h)
if r > 50 or p > 50:
fall = True
else:
fall = False
return fall
def ahrs():
print('')
imu = IMU(verbose=True)
header = 47
print('-'*header)
print("| {:20} | {:20} |".format("Accels [g's]", "Orient(r,p,h) [deg]"))
print('-'*header)
for _ in range(10):
a, m, g = imu.get()
r, p, h = imu.getOrientation(a, m)
print('| {:>6.1f} {:>6.1f} {:>6.1f} | {:>6.1f} {:>6.1f} {:>6.1f} |'.format(a[0], a[1], a[2], r, p, h))
time.sleep(0.50)
print('-'*header)
print(' r: roll')
print(' p: pitch')
print(' h: heading')
print(' g: gravity')
print('deg: degree')
print('')
class NXP9DoF:
'''
Reads from an Adafruit NXP 9-DoF FXOS8700 + FXAS21002 sensor.
Note that this has been calibrated based on the orientation of the
NXP9DoF board as installed on the KR01 robot, with the Adafruit
logo on the chip (mounted horizontally) as follows:
Fore
_---------------
| * |
| |
| |
Port | | Starboard
| |
----------------
Aft
If you mount the chip in a different orientation you will likely
need to multiply one or more of the axis by -1.0.
Depending on where you are on the Earth, true North changes because
the Earth is not a perfect sphere. You can get the declination angle
for your location from:
http://www.magnetic-declination.com/
E.g., for Pukerua Bay, New Zealand:
Latitude: 41° 1' 57.7" S
Longitude: 174° 53' 11.8" E
PUKERUA BAY
Magnetic Declination: +22° 37'
Declination is POSITIVE (EAST)
Inclination: 66° 14'
Magnetic field strength: 55716.5 nT
E.g., for Wellington, New Zealand:
Latitude: 41° 17' 11.9" S
Longitude: 174° 46' 32.1" E
KELBURN
Magnetic Declination: +22° 47'
Declination is POSITIVE (EAST)
Inclination: 66° 28'
Magnetic field strength: 55863.3 nT
'''
# permitted error between Euler and Quaternion (in degrees) to allow setting value
ERROR_RANGE = 5.0 # was 3.0
# ..........................................................................
def __init__(self, config, queue, level):
self._log = Logger("nxp9dof", level)
if config is None:
raise ValueError("no configuration provided.")
self._config = config
self._queue = queue
_config = self._config['ros'].get('nxp9dof')
self._quaternion_accept = _config.get(
'quaternion_accept') # permit Quaternion once calibrated
self._loop_delay_sec = _config.get('loop_delay_sec')
# verbose will print some start-up info on the IMU sensors
self._imu = IMU(gs=4, dps=2000, verbose=True)
# setting a bias correction for the accel only; the mags/gyros are not getting a bias correction
self._imu.setBias((0.0, 0.0, 0.0), None, None)
# self._imu.setBias((0.1,-0.02,.25), None, None)
_i2c = busio.I2C(board.SCL, board.SDA)
self._fxos = adafruit_fxos8700.FXOS8700(_i2c)
self._log.info('accelerometer and magnetometer ready.')
self._fxas = adafruit_fxas21002c.FXAS21002C(_i2c)
self._log.info('gyroscope ready.')
self._thread = None
self._enabled = False
self._closed = False
self._heading = None
self._pitch = None
self._roll = None
self._is_calibrated = False
self._log.info('ready.')
# ..........................................................................
def get_imu(self):
return self._imu
# ..........................................................................
def get_fxos(self):
return self._fxos
# ..........................................................................
def get_fxas(self):
return self._fxas
# ..........................................................................
def enable(self):
if not self._closed:
self._enabled = True
# if we haven't started the thread yet, do so now...
if self._thread is None:
self._thread = threading.Thread(target=NXP9DoF._read,
args=[self])
self._thread.start()
self._log.info('enabled.')
else:
self._log.warning('cannot enable: already closed.')
# ..........................................................................
def get_heading(self):
return self._heading
# ..........................................................................
def get_pitch(self):
return self._pitch
# ..........................................................................
def get_roll(self):
return self._roll
# ..........................................................................
def is_calibrated(self):
return self._is_calibrated
# ..........................................................................
@staticmethod
def _in_range(p, q):
return p >= (q - NXP9DoF.ERROR_RANGE) and p <= (q +
NXP9DoF.ERROR_RANGE)
# ..........................................................................
def imu_enable(self):
'''
Enables the handbuilt IMU on a 20Hz loop.
'''
if not self._closed:
self._enabled = True
# if we haven't started the thread yet, do so now...
if self._thread is None:
self._thread = threading.Thread(target=NXP9DoF._handbuilt_imu,
args=[self])
self._thread.start()
self._log.info('enabled.')
else:
self._log.warning('cannot enable: already closed.')
# ..........................................................................
def _handbuilt_imu(self):
'''
The function that reads sensor values in a loop. This checks to see
if the 'sys' calibration is at least 3 (True), and if the Euler and
Quaternion values are within an error range of each other, this sets
the class variable for heading, pitch and roll. If they aren't within
range for more than n polls, the values revert to None.
'''
self._log.info('starting sensor read...')
_heading = None
_pitch = None
_roll = None
_quat_w = None
_quat_x = None
_quat_y = None
_quat_z = None
count = 0
# 2. Absolute Orientation (Quaterion, 100Hz) Four point quaternion output for more accurate data manipulation ................
# grab data at 20Hz
_rate = Rate(1)
header = 90
print('-' * header)
# print("| {:17} | {:20} |".format("Accels [g's]", " IMU Accels"))
print("| {:17} |".format("Mag [xyz]"))
while not self._closed:
if self._enabled:
accel_x, accel_y, accel_z = self._fxos.accelerometer # m/s^2
gyro_x, gyro_y, gyro_z = self._fxas.gyroscope # radians/s
a, m, g = self._imu.get()
mag_x, mag_y, mag_z = self._fxos.magnetometer # uTesla
mag_x_g = m[0] * 100.0
mag_y_g = m[1] * 100.0
mag_z_g = m[2] * 100.0
# rate_gyro_x_dps = Convert.rps_to_dps(gyro_x)
# rate_gyro_y_dps = Convert.rps_to_dps(gyro_y)
# rate_gyro_z_dps = Convert.rps_to_dps(gyro_z)
# mag_x_g = mag_x * 100.0
# mag_y_g = mag_y * 100.0
# mag_z_g = mag_z * 100.0
heading = 180.0 * math.atan2(mag_y_g, mag_x_g) / math.pi
print(Fore.CYAN + '| x{:>6.3f} y{:>6.3f} z{:>6.3f} |'.format( mag_x_g, mag_y_g, mag_z_g) \
+ Style.BRIGHT + '\t{:>5.2f}'.format(heading) + Style.RESET_ALL)
# a, m, g = self._imu.get()
# print(Fore.CYAN + '| {:>6.3f} {:>6.3f} {:>6.3f} | {:>6.3f} {:>6.3f} {:>6.3f} |'.format( accel_x, accel_y, accel_z, a[0], a[1], a[2]) + Style.RESET_ALL)
_rate.wait()
# + Style.BRIGHT + ' {:>6.1f} {:>6.1f} {:>6.1f}° |'.format(r, p, deg) + Style.RESET_ALL)
# time.sleep(0.50)
# mag_x, mag_y, mag_z = self._fxos.magnetometer # uTesla
# gyro_x, gyro_y, gyro_z = self._fxas.gyroscope # radians/s
# header = 90
# print('-'*header)
# print("| {:17} | {:20} | {:20} | {:20} |".format("Accels [g's]", " Magnet [uT]", "Gyros [dps]", "Roll, Pitch, Heading"))
# print('-'*header)
# for _ in range(10):
# a, m, g = self._imu.get()
# r, p, h = self._imu.getOrientation(a, m)
# deg = Convert.to_degrees(h)
# print(Fore.CYAN + '| {:>5.2f} {:>5.2f} {:>5.2f} | {:>6.1f} {:>6.1f} {:>6.1f} | {:>6.1f} {:>6.1f} {:>6.1f} |'.format(
# a[0], a[1], a[2],
# m[0], m[1], m[2],
# g[0], g[1], g[2])
# + Style.BRIGHT + ' {:>6.1f} {:>6.1f} {:>6.1f}° |'.format(r, p, deg) + Style.RESET_ALL)
# time.sleep(0.50)
# print('-'*header)
# print(' uT: micro Tesla')
# print(' g: gravity')
# print('dps: degrees per second')
# print('')
#
# print(Fore.MAGENTA + 'acc: ({0:0.3f}, {1:0.3f}, {2:0.3f})'.format(accel_x, accel_y, accel_z)\
# + Fore.YELLOW + ' \tmag: ({0:0.3f}, {1:0.3f}, {2:0.3f})'.format(mag_x, mag_y, mag_z)\
# + Fore.CYAN + ' \tgyr: ({0:0.3f}, {1:0.3f}, {2:0.3f})'.format(gyro_x, gyro_y, gyro_z) + Style.RESET_ALL)
else:
self._log.info('disabled loop.')
time.sleep(10)
count += 1
self._log.debug('read loop ended.')
# ..........................................................................
def _read(self):
'''
The function that reads sensor values in a loop. This checks to see
if the 'sys' calibration is at least 3 (True), and if the Euler and
Quaternion values are within an error range of each other, this sets
the class variable for heading, pitch and roll. If they aren't within
range for more than n polls, the values revert to None.
'''
self._log.info('starting sensor read...')
_heading = None
_pitch = None
_roll = None
_quat_w = None
_quat_x = None
_quat_y = None
_quat_z = None
count = 0
# 2. Absolute Orientation (Quaterion, 100Hz) Four point quaternion output for more accurate data manipulation ................
# grab data at 10Hz
rate = Rate(10)
while not self._closed:
if self._enabled:
header = 91
print(Fore.CYAN + ('-' * header) + Style.RESET_ALL)
print(Fore.CYAN + "| {:17} | {:20} | {:20} | {:21} |".format(
"Accels [g's]", " Magnet [uT]", "Gyros [dps]",
"Roll, Pitch, Heading") + Style.RESET_ALL)
print(Fore.CYAN + ('-' * header) + Style.RESET_ALL)
for _ in range(10):
a, m, g = self._imu.get()
r, p, h = self._imu.getOrientation(a, m)
deg = Convert.to_degrees(h)
# self._log.info(Fore.GREEN + '| {:>6.1f} {:>6.1f} {:>6.1f} | {:>6.1f} {:>6.1f} {:>6.1f} |'.format(a[0], a[1], a[2], r, p, h) + Style.RESET_ALL)
print(Fore.CYAN + '| {:>5.2f} {:>5.2f} {:>5.2f} '.format(
a[0], a[1], a[2]) + Fore.YELLOW +
'| {:>6.1f} {:>6.1f} {:>6.1f} '.format(
m[0], m[1], m[2]) + Fore.MAGENTA +
'| {:>6.1f} {:>6.1f} {:>6.1f} '.format(
g[0], g[1], g[2]) + Fore.GREEN +
'| {:>6.1f} {:>6.1f} {:>6.1f}° |'.format(r, p, deg) +
Style.RESET_ALL)
time.sleep(0.50)
print('-' * header)
print(' uT: micro Tesla')
print(' g: gravity')
print('dps: degrees per second')
print('')
# accel_x, accel_y, accel_z = self._fxos.accelerometer # m/s^2
# mag_x, mag_y, mag_z = self._fxos.magnetometer # uTesla
# gyro_x, gyro_y, gyro_z = self._fxas.gyroscope # radians/s
#
# print(Fore.MAGENTA + 'acc: ({0:0.3f}, {1:0.3f}, {2:0.3f})'.format(accel_x, accel_y, accel_z)\
# + Fore.YELLOW + ' \tmag: ({0:0.3f}, {1:0.3f}, {2:0.3f})'.format(mag_x, mag_y, mag_z)\
# + Fore.CYAN + ' \tgyr: ({0:0.3f}, {1:0.3f}, {2:0.3f})'.format(gyro_x, gyro_y, gyro_z) + Style.RESET_ALL)
rate.wait()
else:
self._log.info('disabled loop.')
time.sleep(10)
count += 1
self._log.debug('read loop ended.')
# ..........................................................................
def disable(self):
self._enabled = False
self._log.info('disabled.')
# ..........................................................................
def close(self):
self._closed = True
self._log.info('closed.')
def read9():
#--------9dof init----------
imu = IMU(gs=2, dps=2000, verbose=False)
i2c = I2C(0x1F)
#--------Set calibration values for magnetometer---------
'''Splits avarages to MSB and LSB'''
XMSB = (Xavg / 256) & 0xFF
XLSB = Xavg & 0xFF
YMSB = (Yavg / 256) & 0xFF
YLSB = Yavg & 0xFF
ZMSB = (Zavg / 256) & 0xFF
ZLSB = Zavg & 0xFF
'''Writes splitted avarages to offset registers'''
i2c.write8(0x3F, int(XMSB))
i2c.write8(0x40, int(XLSB))
i2c.write8(0x41, int(YMSB))
i2c.write8(0x42, int(YLSB))
i2c.write8(0x43, int(ZMSB))
i2c.write8(0x44, int(ZLSB))
#--------Talker node init------------
#pub = rospy.Publisher('chatter', String, queue_size=10)
pub = rospy.Publisher('imu', Imu)
rospy.init_node('talker', anonymous=True)
rate = rospy.Rate(10) # 25hz
#---------Readloop---------
while not rospy.is_shutdown():
Havg = 0
#Collects samples and returns avaraged value.
for x in range(0, 20):
try:
a, m, g = imu.get() #Gets data from sensors
r, p, h = imu.getOrientation(
a, m) #calculates orientation from data
ac, ma = imu.rawOrientation() #raw data for magnetometer
'''
#Prevents error in Havg when heading fluctuates between 359 and 0.
if(x > 1):
if(Havg > 260):
if(h < 100):
h += 360
if(Havg < 100):
if(h > 260):
h -= 360
Havg = (Havg + h)/2
'''
except IOError:
pass
'''
#Corrects the heading so that 0 < Havg < 359.
if(Havg < 0):
Havg += 360
if(Havg >= 360):
Havg -= 360
heading = str(Havg)
'''
roll = r * (3.141592 / 180.0) #converts degrees to radians
pitch = p * (3.141592 / 180.0)
yaw = h * (3.141592 / 180.0)
'''
a[0] = a[0] * 9.806 #converts g's to m/s^2
a[1] = a[1] * 9.806
a[2] = a[2] * 9.806
g[0] = g[0] * (3.141592/180.0) #converts degrees to radians
g[1] = g[1] * (3.141592/180.0)
g[2] = g[2] * (3.141592/180.0)
'''
print("Heading: " + str(h))
#q = toQuaternion(r, p, h)
q = tf.transformations.quaternion_from_euler(roll, pitch, yaw)
imuMsg.orientation.x = q[0] #magnetometer
imuMsg.orientation.y = q[1]
imuMsg.orientation.z = q[2]
imuMsg.orientation.w = q[3]
imuMsg.angular_velocity.x = g[0] * (3.141592 / 180.0) #gyro
imuMsg.angular_velocity.y = g[1] * (3.141592 / 180.0)
imuMsg.angular_velocity.z = g[2] * (3.141592 / 180.0)
imuMsg.linear_acceleration.x = a[0] * 9.806 #accelerometer
imuMsg.linear_acceleration.y = a[1] * 9.806
imuMsg.linear_acceleration.z = a[2] * 9.806
rospy.loginfo(imuMsg)
pub.publish(imuMsg)
rate.sleep()
#!/usr/bin/env python
from __future__ import division, print_function
from nxp_imu import IMU
import time
imu = IMU(gs=4, dps=2000, verbose=True)
header = 67
print('-' * header)
print("| {:17} | {:20} | {:20} |".format("Accels [g's]", " Magnet [uT]",
"Gyros [dps]"))
print('-' * header)
for _ in range(10000):
a, m, g = imu.get()
print(
'| {:>5.2f} {:>5.2f} {:>5.2f} | {:>6.1f} {:>6.1f} {:>6.1f} | {:>6.1f} {:>6.1f} {:>6.1f} |'
.format(a[0], a[1], a[2], m[0], m[1], m[2], g[0], g[1], g[2]))
r, p, y = imu.getOrientation(accel=a, mag=m)
# print('| {:>5.2f} {:>5.2f} {:>5.2f} {:>5.2f}|'.format(y, p, r, y))
time.sleep(0.10)
print('-' * header)
print(' uT: micro Tesla')
print(' g: gravity')
print('dps: degrees per second')
print('')
msg = Imu()
while not geckopy.is_shutdown():
a, m, g = imu.get()
msg.linear_acceleration.x = a[0]
msg.linear_acceleration.y = a[1]
msg.linear_acceleration.z = a[2]
msg.angular_velocity.x = g[0]
msg.angular_velocity.y = g[1]
msg.angular_velocity.z = g[2]
msg.magnetic_field.x = m[0]
msg.magnetic_field.y = m[1]
msg.magnetic_field.z = m[2]
r, p, h = imu.getOrientation(a, m)
q = euler2quat(r, p, h, degrees=True)
msg.orientation.w = q.w
msg.orientation.x = q.x
msg.orientation.y = q.y
msg.orientation.z = q.z
print(msg)
pub.publish(protobufPack(msg))
rate.sleep()
'gyroX_dps', 'gyroY_dps', 'gyroZ_dps', 'gyroX_deg', 'gyroY_deg',
'gyroZ_deg', 'temp_C', 'humidity', 'pres_Pa', 'alt_m'
])
createCsv(headers)
imu = IMU(gs=8, dps=2000, verbose=True)
incrementalData = empty((0, len(headers)))
saveIdx = 50
idx = 0
while True:
imuError = False
bmeError = False
try:
a, m, g = imu.get()
q = imu.getOrientation(a, m)
a, m, g, q = [around(a, 3), around(m, 3), around(g, 3), around(q, 3)]
except:
a, m, g, q = [["Err"] * 3] * 4
try:
bmeError = True
bmeSensor = BME280(t_mode=BME280_OSAMPLE_8,
p_mode=BME280_OSAMPLE_8,
h_mode=BME280_OSAMPLE_8)
temp = bmeSensor.read_temperature()
humidity = bmeSensor.read_humidity()
pressure = bmeSensor.read_pressure()
alt = (((101325.0 / pressure)**(1 / 5.257) - 1) *
(temp + 273.15)) / 0.0065
temp, humidity, pressure, alt = [
around(temp, 3),