コード例 #1
0
    def __init__(self):
        rospy.init_node('sensor_sim_gps')
        self.pub = rospy.Publisher("/gps_pose", PoseStamped)
        self.pubStat = rospy.Publisher("/gps_status", GPSStatus)

        # declare messages
        self.gps_msg = PoseStamped()
        self.gps_stat = GPSStatus()
        # Mimic GPS status message
        self.gps_stat.satellites_used = 7
        self.gps_stat.satellites_visible = 9
        self.gps_stat.position_source = 50

        #setup subscriber
        rospy.Subscriber("base_pose_ground_truth", Odometry, self.callback)

        #spin
        rospy.spin()
コード例 #2
0
ファイル: mtnode.py プロジェクト: rpng/xsens_mti_ros_node
    def spin_once(self):
        def baroPressureToHeight(value):
            c1 = 44330.0
            c2 = 9.869232667160128300024673081668e-6
            c3 = 0.1901975534856
            intermediate = 1 - math.pow(c2 * value, c3)
            height = c1 * intermediate
            return height

        # get data
        data = self.mt.read_measurement()
        # common header
        h = Header()
        h.stamp = rospy.Time.now()
        h.frame_id = self.frame_id

        # get data (None if not present)
        temp_data = data.get('Temperature')  # float
        orient_data = data.get('Orientation Data')
        velocity_data = data.get('Velocity')
        position_data = data.get('Latlon')
        altitude_data = data.get('Altitude')
        acc_data = data.get('Acceleration')
        gyr_data = data.get('Angular Velocity')
        mag_data = data.get('Magnetic')
        pressure_data = data.get('Pressure')
        time_data = data.get('Timestamp')
        gnss_data = data.get('GNSS')

        # debug the data from the sensor
        # print(data)
        # print("\n")

        # create messages and default values
        "Temp message"
        temp_msg = Temperature()
        pub_temp = False
        "Imu message supported with Modes 1 & 2"
        imuraw_msg = Imu()
        pub_imuraw = False
        imuins_msg = Imu()
        pub_imuins = False
        "SensorSample message supported with Mode 2"
        ss_msg = sensorSample()
        pub_ss = False
        "Mag message supported with Modes 1 & 2"
        mag_msg = Vector3Stamped()
        pub_mag = False
        "Baro in meters"
        baro_msg = FluidPressure()
        height_msg = baroSample()
        pub_baro = False
        "GNSS message supported only with MTi-G-7xx devices"
        "Valid only for modes 1 and 2"
        gnssPvt_msg = gnssSample()
        gps1_msg = NavSatFix()
        gps2_msg = GPSFix()
        pub_gnssPvt = False
        gnssSatinfo_msg = GPSStatus()
        pub_gnssSatinfo = False
        # All filter related outputs
        "Supported in mode 3"
        ori_msg = orientationEstimate()
        pub_ori = False
        "Supported in mode 3 for MTi-G-7xx devices"
        vel_msg = velocityEstimate()
        pub_vel = False
        "Supported in mode 3 for MTi-G-7xx devices"
        pos_msg = positionEstimate()
        pub_pos = False

        # first getting the sampleTimeFine
        # note if we are not using ros time, the we should replace the header
        # with the time supplied by the GNSS unit
        if time_data and not self.use_rostime:
            time = time_data['SampleTimeFine']
            h.stamp.secs = 100e-6 * time
            h.stamp.nsecs = 1e5 * time - 1e9 * math.floor(h.stamp.secs)

        # temp data
        if temp_data:
            temp_msg.temperature = temp_data['Temp']
            pub_temp = True

        # acceleration data
        if acc_data:
            if 'accX' in acc_data:  # found acceleration
                pub_imuraw = True
                imuraw_msg.linear_acceleration.x = acc_data['accX']
                imuraw_msg.linear_acceleration.y = acc_data['accY']
                imuraw_msg.linear_acceleration.z = acc_data['accZ']
            if 'freeAccX' in acc_data:  # found free acceleration
                pub_imuins = True
                imuins_msg.linear_acceleration.x = acc_data['freeAccX']
                imuins_msg.linear_acceleration.y = acc_data['freeAccY']
                imuins_msg.linear_acceleration.z = acc_data['freeAccZ']
            if 'Delta v.x' in acc_data:  # found delta-v's
                pub_ss = True
                ss_msg.internal.imu.dv.x = acc_data['Delta v.x']
                ss_msg.internal.imu.dv.y = acc_data['Delta v.y']
                ss_msg.internal.imu.dv.z = acc_data['Delta v.z']
            #else:
            #	raise MTException("Unsupported message in XDI_AccelerationGroup.")

        # gyro data
        if gyr_data:
            if 'gyrX' in gyr_data:  # found rate of turn
                pub_imuraw = True
                imuraw_msg.angular_velocity.x = gyr_data['gyrX']
                imuraw_msg.angular_velocity.y = gyr_data['gyrY']
                imuraw_msg.angular_velocity.z = gyr_data['gyrZ']
                # note we do not force publishing the INS if we do not use the free acceleration
                imuins_msg.angular_velocity.x = gyr_data['gyrX']
                imuins_msg.angular_velocity.y = gyr_data['gyrY']
                imuins_msg.angular_velocity.z = gyr_data['gyrZ']
            if 'Delta q0' in gyr_data:  # found delta-q's
                pub_ss = True
                ss_msg.internal.imu.dq.w = gyr_data['Delta q0']
                ss_msg.internal.imu.dq.x = gyr_data['Delta q1']
                ss_msg.internal.imu.dq.y = gyr_data['Delta q2']
                ss_msg.internal.imu.dq.z = gyr_data['Delta q3']
            #else:
            #	raise MTException("Unsupported message in XDI_AngularVelocityGroup.")

        # magfield
        if mag_data:
            ss_msg.internal.mag.x = mag_msg.vector.x = mag_data['magX']
            ss_msg.internal.mag.y = mag_msg.vector.y = mag_data['magY']
            ss_msg.internal.mag.z = mag_msg.vector.z = mag_data['magZ']
            pub_mag = True

        if pressure_data:
            pub_baro = True
            baro_msg.fluid_pressure = pressure_data['Pressure']
            height = baroPressureToHeight(pressure_data['Pressure'])
            height_msg.height = ss_msg.internal.baro.height = height

        # gps fix message
        if gnss_data and 'lat' in gnss_data:
            pub_gnssPvt = True
            # A "3" means that the MTi-G is using the GPS data.
            # A "1" means that the MTi-G was using GPS data and is now coasting/dead-reckoning the
            # 	position based on the inertial sensors (the MTi-G is not using GPS data in this mode).
            # 	This is done for 45 seconds, before the MTi-G Mode drops to "0".
            # A "0" means that the MTi-G doesn't use GPS data and also that it
            # 	doesn't output position based on the inertial sensors.
            if gnss_data['fix'] < 2:
                gnssSatinfo_msg.status = NavSatStatus.STATUS_NO_FIX  # no fix
                gps1_msg.status.status = NavSatStatus.STATUS_NO_FIX  # no fix
                gps1_msg.status.service = 0
            else:
                gnssSatinfo_msg.status = NavSatStatus.STATUS_FIX  # unaugmented
                gps1_msg.status.status = NavSatStatus.STATUS_FIX  # unaugmented
                gps1_msg.status.service = NavSatStatus.SERVICE_GPS
            # lat lon alt
            gps1_msg.latitude = gnss_data['lat']
            gps1_msg.longitude = gnss_data['lon']
            gps1_msg.altitude = gnss_data['hEll']
            # covariances
            gps1_msg.position_covariance[0] = math.pow(gnss_data['horzAcc'], 2)
            gps1_msg.position_covariance[4] = math.pow(gnss_data['horzAcc'], 2)
            gps1_msg.position_covariance[8] = math.pow(gnss_data['vertAcc'], 2)
            gps1_msg.position_covariance_type = NavSatFix.COVARIANCE_TYPE_DIAGONAL_KNOWN
            # custom message
            gnssPvt_msg.itow = gnss_data['iTOW']
            gnssPvt_msg.fix = gnss_data['fix']
            gnssPvt_msg.latitude = gnss_data['lat']
            gnssPvt_msg.longitude = gnss_data['lon']
            gnssPvt_msg.hEll = gnss_data['hEll']
            gnssPvt_msg.hMsl = gnss_data['hMsl']
            gnssPvt_msg.vel.x = gnss_data['velE']
            gnssPvt_msg.vel.y = gnss_data['velN']
            gnssPvt_msg.vel.z = gnss_data['velD']
            gnssPvt_msg.hAcc = gnss_data['horzAcc']
            gnssPvt_msg.vAcc = gnss_data['vertAcc']
            gnssPvt_msg.sAcc = gnss_data['speedAcc']
            gnssPvt_msg.pDop = gnss_data['PDOP']
            gnssPvt_msg.hDop = gnss_data['HDOP']
            gnssPvt_msg.vDop = gnss_data['VDOP']
            gnssPvt_msg.numSat = gnss_data['nSat']
            gnssPvt_msg.heading = gnss_data['heading']
            gnssPvt_msg.headingAcc = gnss_data['headingAcc']

        if orient_data:
            if 'Q0' in orient_data:
                pub_imuraw = True
                imuraw_msg.orientation.w = orient_data['Q0']
                imuraw_msg.orientation.x = orient_data['Q1']
                imuraw_msg.orientation.y = orient_data['Q2']
                imuraw_msg.orientation.z = orient_data['Q3']
                pub_imuins = True
                imuins_msg.orientation.w = orient_data['Q0']
                imuins_msg.orientation.x = orient_data['Q1']
                imuins_msg.orientation.y = orient_data['Q2']
                imuins_msg.orientation.z = orient_data['Q3']
            elif 'Roll' in orient_data:
                pub_ori = True
                ori_msg.roll = orient_data['Roll']
                ori_msg.pitch = orient_data['Pitch']
                ori_msg.yaw = orient_data['Yaw']
            else:
                raise MTException(
                    'Unsupported message in XDI_OrientationGroup')

        if velocity_data:
            pub_vel = True
            vel_msg.velE = velocity_data['velX']
            vel_msg.velN = velocity_data['velY']
            vel_msg.velU = velocity_data['velZ']

        if position_data:
            pub_pos = True
            pos_msg.latitude = position_data['lat']
            pos_msg.longitude = position_data['lon']

        if altitude_data:
            pub_pos = True
            tempData = altitude_data['ellipsoid']
            pos_msg.hEll = tempData[0]

        # publish available information
        if pub_imuraw:
            imuraw_msg.header = h
            self.imuraw_pub.publish(imuraw_msg)
        if pub_imuins:
            imuins_msg.header = h
            self.imuins_pub.publish(imuins_msg)
        if pub_mag:
            mag_msg.header = h
            self.mag_pub.publish(mag_msg)
        if pub_temp:
            temp_msg.header = h
            self.temp_pub.publish(temp_msg)
        if pub_ss:
            ss_msg.header = h
            self.ss_pub.publish(ss_msg)
        if pub_baro:
            baro_msg.header = h
            height_msg.header = h
            self.baro_pub.publish(baro_msg)
            self.height_pub.publish(height_msg)
        if pub_gnssPvt:
            gnssPvt_msg.header = h
            gps1_msg.header = h
            self.gnssPvt_pub.publish(gnssPvt_msg)
            self.gps1_pub.publish(gps1_msg)
        #if pub_gnssSatinfo:
        #	gnssSatinfo_msg.header = h
        #	self.gnssSatinfo_pub.publish(gnssSatinfo_msg)
        if pub_ori:
            ori_msg.header = h
            self.ori_pub.publish(ori_msg)
        if pub_vel:
            vel_msg.header = h
            self.vel_pub.publish(vel_msg)
        if pub_pos:
            pos_msg.header = h
            self.pos_pub.publish(pos_msg)
コード例 #3
0
    #ROS init
    rospy.loginfo("1")
    rospy.init_node('arduimu_driver')
    imuPub = rospy.Publisher('arduimu/imu', Imu)
    gpsPub = rospy.Publisher('arduimu/gps_fix', NavSatFix)
    velPub = rospy.Publisher('arduimu/gps_vel', TwistStamped)
    statPub = rospy.Publisher('arduimu/gps_status', GPSStatus)
    #Init Imu port
    arduPort = rospy.get_param('~port', '/dev/ttyUSB0')
    arduRate = rospy.get_param('~baud', 57600)

    rospy.loginfo("2")
    imuData = Imu()
    navData = NavSatFix()
    gpsVel = TwistStamped()
    gpsStat = GPSStatus()
    imuData.header.frame_id = "base_arduimu"
    navData.header.frame_id = "base_arduimu"
    gpsVel.header.frame_id = "base_arduimu"
    gpsStat.header.frame_id = "base_arduimu"

    rospy.loginfo("3")
    parser = ArduimuParser()

    try:
        rospy.loginfo("4")
        dataIn = serial.Serial(port=arduPort, baudrate=arduRate, timeout=.02)
        #Read in data
        sync0 = '\x00'
        sync1 = '\x00'
        while not rospy.is_shutdown():
コード例 #4
0
    gpsPub = rospy.Publisher('gps_fix', NavSatFix, queue_size=1)
    gpsStatPub = rospy.Publisher('gps_status', GPSStatus, queue_size=1)
    gpsVelPub = rospy.Publisher('gps_vel',TwistStamped, queue_size=1)
    #gpsTimePub = rospy.Publisher('time_reference', TimeReference)
    #Init gpsSerial port
    GPSport = rospy.get_param('~port','/dev/ttyUSB0')
    GPSrate = rospy.get_param('~baud',57600)
    frame_id = rospy.get_param('~frame_id','gps')
    if frame_id[0] != "/":
       frame_id = addTFPrefix(frame_id)

    time_ref_source = rospy.get_param('~time_ref_source', frame_id)
    navData = NavSatFix()
    gpsVel = TwistStamped()
    gpstime = TimeReference()
    gpsStatus = GPSStatus()
    gpstime.source = time_ref_source
    navData.header.frame_id = frame_id
    gpsVel.header.frame_id = frame_id
    GPSLock = False

    parser = NovatelParser()
    
    try:
        gpsSerial = serial.Serial(port=GPSport,baudrate=GPSrate,timeout=.01)
        #Read in gpsSerial data
        sync0 = '\x00'; sync1 = '\x00'; sync2 = '\x00';
        while not rospy.is_shutdown():
            # READ UNTIL SYNC
            data  = gpsSerial.read(1)
            sync2 = sync1; sync1 = sync0; sync0 = data;
コード例 #5
0
import serial
import time
import rospy
import numpy as np  # se emplea esta para operar matrices

from nav_msgs.msg import Odometry
from geometry_msgs.msg import Vector3Stamped
from gps_common.msg import GPSStatus, GPSFix

msg = Vector3Stamped()
gps = GPSFix()
gps2 = GPSStatus()

#gps = serial.Serial("/dev/tty_gps", baudrate = 9600)


class GPS(object):
    def __init__(self):
        self.gps = serial.Serial("/dev/tty_gps", baudrate=9600)
        self.line = 0
        self.data = 0

        #Geometria del elipsoide
        self.a = 6378137.0  # radius of the earth in metters
        self.b = 6356752.31414

        self.e1 = 6.6943800229e-3
        self.e2 = 6.73949677548e-3
        #radio polar de curvatura = c
        self.c = 6399593.626
        self.Long_rad = 0