Lorenz Meier
12 years ago
1 changed files with 0 additions and 600 deletions
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/****************************************************************************
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* |
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* Copyright (C) 2012 PX4 Development Team. All rights reserved. |
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* Author: Lorenz Meier <lm@inf.ethz.ch> |
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* |
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* Redistribution and use in source and binary forms, with or without |
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* modification, are permitted provided that the following conditions |
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* are met: |
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* |
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* 1. Redistributions of source code must retain the above copyright |
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* notice, this list of conditions and the following disclaimer. |
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* 2. Redistributions in binary form must reproduce the above copyright |
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* notice, this list of conditions and the following disclaimer in |
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* the documentation and/or other materials provided with the |
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* distribution. |
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* 3. Neither the name PX4 nor the names of its contributors may be |
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* used to endorse or promote products derived from this software |
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* without specific prior written permission. |
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* |
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* THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS |
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* "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT |
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* LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS |
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* FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE |
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* COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT, |
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* INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING, |
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* BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS |
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* OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED |
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* AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT |
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* LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN |
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* ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE |
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* POSSIBILITY OF SUCH DAMAGE. |
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* |
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****************************************************************************/ |
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/**
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* @file mavlink_receiver.c |
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* MAVLink protocol message receive and dispatch |
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* |
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* @author Lorenz Meier <lm@inf.ethz.ch> |
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*/ |
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/* XXX trim includes */ |
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#include <nuttx/config.h> |
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#include <unistd.h> |
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#include <pthread.h> |
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#include <stdio.h> |
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#include <math.h> |
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#include <stdbool.h> |
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#include <fcntl.h> |
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#include <mqueue.h> |
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#include <string.h> |
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#include "mavlink_bridge_header.h" |
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#include <v1.0/common/mavlink.h> |
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#include <drivers/drv_hrt.h> |
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#include <time.h> |
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#include <float.h> |
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#include <unistd.h> |
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#include <nuttx/sched.h> |
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#include <sys/prctl.h> |
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#include <termios.h> |
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#include <errno.h> |
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#include <stdlib.h> |
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#include <poll.h> |
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#include <systemlib/param/param.h> |
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#include <systemlib/systemlib.h> |
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#include <mavlink/mavlink_log.h> |
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#include "waypoints.h" |
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#include "orb_topics.h" |
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#include "missionlib.h" |
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#include "mavlink_hil.h" |
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#include "mavlink_parameters.h" |
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#include "util.h" |
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/* XXX should be in a header somewhere */ |
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pthread_t receive_start(int uart); |
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static void handle_message(mavlink_message_t *msg); |
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static void *receive_thread(void *arg); |
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static mavlink_status_t status; |
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static struct vehicle_vicon_position_s vicon_position; |
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static struct vehicle_command_s vcmd; |
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static struct offboard_control_setpoint_s offboard_control_sp; |
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struct vehicle_global_position_s hil_global_pos; |
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struct vehicle_attitude_s hil_attitude; |
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struct vehicle_gps_position_s hil_gps; |
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struct sensor_combined_s hil_sensors; |
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orb_advert_t pub_hil_global_pos = -1; |
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orb_advert_t pub_hil_attitude = -1; |
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orb_advert_t pub_hil_gps = -1; |
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orb_advert_t pub_hil_sensors = -1; |
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static orb_advert_t cmd_pub = -1; |
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static orb_advert_t flow_pub = -1; |
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static orb_advert_t offboard_control_sp_pub = -1; |
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static orb_advert_t vicon_position_pub = -1; |
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extern bool gcs_link; |
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static void |
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handle_message(mavlink_message_t *msg) |
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{ |
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if (msg->msgid == MAVLINK_MSG_ID_COMMAND_LONG) { |
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mavlink_command_long_t cmd_mavlink; |
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mavlink_msg_command_long_decode(msg, &cmd_mavlink); |
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if (cmd_mavlink.target_system == mavlink_system.sysid && ((cmd_mavlink.target_component == mavlink_system.compid) |
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|| (cmd_mavlink.target_component == MAV_COMP_ID_ALL))) { |
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//check for MAVLINK terminate command
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if (cmd_mavlink.command == MAV_CMD_PREFLIGHT_REBOOT_SHUTDOWN && ((int)cmd_mavlink.param1) == 3) { |
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/* This is the link shutdown command, terminate mavlink */ |
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printf("[mavlink] Terminating .. \n"); |
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fflush(stdout); |
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usleep(50000); |
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/* terminate other threads and this thread */ |
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thread_should_exit = true; |
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} else { |
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/* Copy the content of mavlink_command_long_t cmd_mavlink into command_t cmd */ |
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vcmd.param1 = cmd_mavlink.param1; |
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vcmd.param2 = cmd_mavlink.param2; |
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vcmd.param3 = cmd_mavlink.param3; |
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vcmd.param4 = cmd_mavlink.param4; |
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vcmd.param5 = cmd_mavlink.param5; |
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vcmd.param6 = cmd_mavlink.param6; |
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vcmd.param7 = cmd_mavlink.param7; |
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vcmd.command = cmd_mavlink.command; |
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vcmd.target_system = cmd_mavlink.target_system; |
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vcmd.target_component = cmd_mavlink.target_component; |
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vcmd.source_system = msg->sysid; |
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vcmd.source_component = msg->compid; |
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vcmd.confirmation = cmd_mavlink.confirmation; |
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/* check if topic is advertised */ |
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if (cmd_pub <= 0) { |
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cmd_pub = orb_advertise(ORB_ID(vehicle_command), &vcmd); |
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} |
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/* publish */ |
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orb_publish(ORB_ID(vehicle_command), cmd_pub, &vcmd); |
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} |
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} |
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} |
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if (msg->msgid == MAVLINK_MSG_ID_OPTICAL_FLOW) { |
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mavlink_optical_flow_t flow; |
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mavlink_msg_optical_flow_decode(msg, &flow); |
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struct optical_flow_s f; |
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f.timestamp = flow.time_usec; |
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f.flow_raw_x = flow.flow_x; |
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f.flow_raw_y = flow.flow_y; |
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f.flow_comp_x_m = flow.flow_comp_m_x; |
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f.flow_comp_y_m = flow.flow_comp_m_y; |
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f.ground_distance_m = flow.ground_distance; |
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f.quality = flow.quality; |
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f.sensor_id = flow.sensor_id; |
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/* check if topic is advertised */ |
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if (flow_pub <= 0) { |
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flow_pub = orb_advertise(ORB_ID(optical_flow), &f); |
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} else { |
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/* publish */ |
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orb_publish(ORB_ID(optical_flow), flow_pub, &f); |
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} |
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} |
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if (msg->msgid == MAVLINK_MSG_ID_SET_MODE) { |
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/* Set mode on request */ |
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mavlink_set_mode_t new_mode; |
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mavlink_msg_set_mode_decode(msg, &new_mode); |
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/* Copy the content of mavlink_command_long_t cmd_mavlink into command_t cmd */ |
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vcmd.param1 = new_mode.base_mode; |
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vcmd.param2 = new_mode.custom_mode; |
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vcmd.param3 = 0; |
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vcmd.param4 = 0; |
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vcmd.param5 = 0; |
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vcmd.param6 = 0; |
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vcmd.param7 = 0; |
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vcmd.command = MAV_CMD_DO_SET_MODE; |
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vcmd.target_system = new_mode.target_system; |
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vcmd.target_component = MAV_COMP_ID_ALL; |
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vcmd.source_system = msg->sysid; |
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vcmd.source_component = msg->compid; |
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vcmd.confirmation = 1; |
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/* check if topic is advertised */ |
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if (cmd_pub <= 0) { |
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cmd_pub = orb_advertise(ORB_ID(vehicle_command), &vcmd); |
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} else { |
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/* create command */ |
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orb_publish(ORB_ID(vehicle_command), cmd_pub, &vcmd); |
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} |
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} |
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/* Handle Vicon position estimates */ |
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if (msg->msgid == MAVLINK_MSG_ID_VICON_POSITION_ESTIMATE) { |
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mavlink_vicon_position_estimate_t pos; |
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mavlink_msg_vicon_position_estimate_decode(msg, &pos); |
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vicon_position.timestamp = hrt_absolute_time(); |
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vicon_position.x = pos.x; |
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vicon_position.y = pos.y; |
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vicon_position.z = pos.z; |
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vicon_position.roll = pos.roll; |
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vicon_position.pitch = pos.pitch; |
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vicon_position.yaw = pos.yaw; |
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if (vicon_position_pub <= 0) { |
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vicon_position_pub = orb_advertise(ORB_ID(vehicle_vicon_position), &vicon_position); |
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} else { |
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orb_publish(ORB_ID(vehicle_vicon_position), vicon_position_pub, &vicon_position); |
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} |
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} |
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/* Handle quadrotor motor setpoints */ |
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if (msg->msgid == MAVLINK_MSG_ID_SET_QUAD_SWARM_ROLL_PITCH_YAW_THRUST) { |
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mavlink_set_quad_swarm_roll_pitch_yaw_thrust_t quad_motors_setpoint; |
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mavlink_msg_set_quad_swarm_roll_pitch_yaw_thrust_decode(msg, &quad_motors_setpoint); |
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if (mavlink_system.sysid < 4) { |
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/* switch to a receiving link mode */ |
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gcs_link = false; |
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/*
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* rate control mode - defined by MAVLink |
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*/ |
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uint8_t ml_mode = 0; |
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bool ml_armed = false; |
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switch (quad_motors_setpoint.mode) { |
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case 0: |
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ml_armed = false; |
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break; |
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case 1: |
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ml_mode = OFFBOARD_CONTROL_MODE_DIRECT_RATES; |
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ml_armed = true; |
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break; |
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case 2: |
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ml_mode = OFFBOARD_CONTROL_MODE_DIRECT_ATTITUDE; |
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ml_armed = true; |
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break; |
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case 3: |
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ml_mode = OFFBOARD_CONTROL_MODE_DIRECT_VELOCITY; |
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break; |
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case 4: |
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ml_mode = OFFBOARD_CONTROL_MODE_DIRECT_POSITION; |
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break; |
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} |
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offboard_control_sp.p1 = (float)quad_motors_setpoint.roll[mavlink_system.sysid - 1] / (float)INT16_MAX; |
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offboard_control_sp.p2 = (float)quad_motors_setpoint.pitch[mavlink_system.sysid - 1] / (float)INT16_MAX; |
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offboard_control_sp.p3 = (float)quad_motors_setpoint.yaw[mavlink_system.sysid - 1] / (float)INT16_MAX; |
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offboard_control_sp.p4 = (float)quad_motors_setpoint.thrust[mavlink_system.sysid - 1] / (float)UINT16_MAX; |
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if (quad_motors_setpoint.thrust[mavlink_system.sysid - 1] == 0) { |
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ml_armed = false; |
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} |
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offboard_control_sp.armed = ml_armed; |
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offboard_control_sp.mode = ml_mode; |
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offboard_control_sp.timestamp = hrt_absolute_time(); |
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/* check if topic has to be advertised */ |
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if (offboard_control_sp_pub <= 0) { |
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offboard_control_sp_pub = orb_advertise(ORB_ID(offboard_control_setpoint), &offboard_control_sp); |
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} else { |
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/* Publish */ |
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orb_publish(ORB_ID(offboard_control_setpoint), offboard_control_sp_pub, &offboard_control_sp); |
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} |
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} |
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} |
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/*
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* Only decode hil messages in HIL mode. |
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* |
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* The HIL mode is enabled by the HIL bit flag |
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* in the system mode. Either send a set mode |
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* COMMAND_LONG message or a SET_MODE message |
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*/ |
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if (mavlink_hil_enabled) { |
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uint64_t timestamp = hrt_absolute_time(); |
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if (msg->msgid == MAVLINK_MSG_ID_HIGHRES_IMU) { |
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mavlink_highres_imu_t imu; |
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mavlink_msg_highres_imu_decode(msg, &imu); |
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/* packet counter */ |
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static uint16_t hil_counter = 0; |
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static uint16_t hil_frames = 0; |
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static uint64_t old_timestamp = 0; |
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/* sensors general */ |
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hil_sensors.timestamp = hrt_absolute_time(); |
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/* hil gyro */ |
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static const float mrad2rad = 1.0e-3f; |
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hil_sensors.gyro_counter = hil_counter; |
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hil_sensors.gyro_raw[0] = imu.xgyro / mrad2rad; |
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hil_sensors.gyro_raw[1] = imu.ygyro / mrad2rad; |
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hil_sensors.gyro_raw[2] = imu.zgyro / mrad2rad; |
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hil_sensors.gyro_rad_s[0] = imu.xgyro; |
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hil_sensors.gyro_rad_s[1] = imu.ygyro; |
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hil_sensors.gyro_rad_s[2] = imu.zgyro; |
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/* accelerometer */ |
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hil_sensors.accelerometer_counter = hil_counter; |
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static const float mg2ms2 = 9.8f / 1000.0f; |
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hil_sensors.accelerometer_raw[0] = imu.xacc / mg2ms2; |
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hil_sensors.accelerometer_raw[1] = imu.yacc / mg2ms2; |
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hil_sensors.accelerometer_raw[2] = imu.zacc / mg2ms2; |
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hil_sensors.accelerometer_m_s2[0] = imu.xacc; |
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hil_sensors.accelerometer_m_s2[1] = imu.yacc; |
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hil_sensors.accelerometer_m_s2[2] = imu.zacc; |
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hil_sensors.accelerometer_mode = 0; // TODO what is this?
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hil_sensors.accelerometer_range_m_s2 = 32.7f; // int16
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/* adc */ |
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hil_sensors.adc_voltage_v[0] = 0; |
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hil_sensors.adc_voltage_v[1] = 0; |
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hil_sensors.adc_voltage_v[2] = 0; |
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/* magnetometer */ |
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float mga2ga = 1.0e-3f; |
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hil_sensors.magnetometer_counter = hil_counter; |
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hil_sensors.magnetometer_raw[0] = imu.xmag / mga2ga; |
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hil_sensors.magnetometer_raw[1] = imu.ymag / mga2ga; |
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hil_sensors.magnetometer_raw[2] = imu.zmag / mga2ga; |
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hil_sensors.magnetometer_ga[0] = imu.xmag; |
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hil_sensors.magnetometer_ga[1] = imu.ymag; |
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hil_sensors.magnetometer_ga[2] = imu.zmag; |
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hil_sensors.magnetometer_range_ga = 32.7f; // int16
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hil_sensors.magnetometer_mode = 0; // TODO what is this
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hil_sensors.magnetometer_cuttoff_freq_hz = 50.0f; |
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/* baro */ |
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hil_sensors.baro_pres_mbar = imu.abs_pressure; |
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hil_sensors.baro_alt_meter = imu.pressure_alt; |
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hil_sensors.baro_temp_celcius = imu.temperature; |
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hil_sensors.gyro_counter = hil_counter; |
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hil_sensors.magnetometer_counter = hil_counter; |
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hil_sensors.accelerometer_counter = hil_counter; |
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/* publish */ |
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orb_publish(ORB_ID(sensor_combined), pub_hil_sensors, &hil_sensors); |
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// increment counters
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hil_counter++; |
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hil_frames++; |
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// output
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if ((timestamp - old_timestamp) > 10000000) { |
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printf("receiving hil imu at %d hz\n", hil_frames/10); |
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old_timestamp = timestamp; |
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hil_frames = 0; |
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} |
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} |
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if (msg->msgid == MAVLINK_MSG_ID_GPS_RAW_INT) { |
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mavlink_gps_raw_int_t gps; |
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mavlink_msg_gps_raw_int_decode(msg, &gps); |
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/* packet counter */ |
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static uint16_t hil_counter = 0; |
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static uint16_t hil_frames = 0; |
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static uint64_t old_timestamp = 0; |
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/* gps */ |
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hil_gps.timestamp_position = gps.time_usec; |
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hil_gps.time_gps_usec = gps.time_usec; |
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hil_gps.lat = gps.lat; |
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hil_gps.lon = gps.lon; |
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hil_gps.alt = gps.alt; |
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hil_gps.eph_m = (float)gps.eph * 1e-2f; // from cm to m
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hil_gps.epv_m = (float)gps.epv * 1e-2f; // from cm to m
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hil_gps.s_variance_m_s = 5.0f; |
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hil_gps.p_variance_m = hil_gps.eph_m * hil_gps.eph_m; |
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hil_gps.vel_m_s = (float)gps.vel * 1e-2f; // from cm/s to m/s
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/* gps.cog is in degrees 0..360 * 100, heading is -PI..+PI */ |
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float heading_rad = gps.cog * M_DEG_TO_RAD_F * 1e-2f; |
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/* go back to -PI..PI */ |
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if (heading_rad > M_PI_F) |
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heading_rad -= 2.0f * M_PI_F; |
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hil_gps.vel_n_m_s = (float)gps.vel * 1e-2f * cosf(heading_rad); |
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hil_gps.vel_e_m_s = (float)gps.vel * 1e-2f * sinf(heading_rad); |
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hil_gps.vel_d_m_s = 0.0f; |
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hil_gps.vel_ned_valid = true; |
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/* COG (course over ground) is speced as -PI..+PI */ |
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hil_gps.cog_rad = heading_rad; |
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hil_gps.fix_type = gps.fix_type; |
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hil_gps.satellites_visible = gps.satellites_visible; |
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/* publish */ |
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orb_publish(ORB_ID(vehicle_gps_position), pub_hil_gps, &hil_gps); |
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// increment counters
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hil_counter += 1 ; |
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hil_frames += 1 ; |
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// output
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// if ((timestamp - old_timestamp) > 10000000) {
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// printf("receiving hil gps at %d hz\n", hil_frames/10);
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// old_timestamp = timestamp;
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// hil_frames = 0;
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// }
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} |
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if (msg->msgid == MAVLINK_MSG_ID_HIL_STATE) { |
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mavlink_hil_state_t hil_state; |
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mavlink_msg_hil_state_decode(msg, &hil_state); |
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/* Calculate Rotation Matrix */ |
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//TODO: better clarification which app does this, atm we have a ekf for quadrotors which does this, but there is no such thing if fly in fixed wing mode
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if (mavlink_system.type == MAV_TYPE_FIXED_WING) { |
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//TODO: assuming low pitch and roll values for now
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hil_attitude.R[0][0] = cosf(hil_state.yaw); |
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hil_attitude.R[0][1] = sinf(hil_state.yaw); |
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hil_attitude.R[0][2] = 0.0f; |
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hil_attitude.R[1][0] = -sinf(hil_state.yaw); |
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hil_attitude.R[1][1] = cosf(hil_state.yaw); |
||||
hil_attitude.R[1][2] = 0.0f; |
||||
|
||||
hil_attitude.R[2][0] = 0.0f; |
||||
hil_attitude.R[2][1] = 0.0f; |
||||
hil_attitude.R[2][2] = 1.0f; |
||||
|
||||
hil_attitude.R_valid = true; |
||||
} |
||||
|
||||
hil_global_pos.lat = hil_state.lat; |
||||
hil_global_pos.lon = hil_state.lon; |
||||
hil_global_pos.alt = hil_state.alt / 1000.0f; |
||||
hil_global_pos.vx = hil_state.vx / 100.0f; |
||||
hil_global_pos.vy = hil_state.vy / 100.0f; |
||||
hil_global_pos.vz = hil_state.vz / 100.0f; |
||||
|
||||
|
||||
/* set timestamp and notify processes (broadcast) */ |
||||
hil_global_pos.timestamp = hrt_absolute_time(); |
||||
orb_publish(ORB_ID(vehicle_global_position), pub_hil_global_pos, &hil_global_pos); |
||||
|
||||
hil_attitude.roll = hil_state.roll; |
||||
hil_attitude.pitch = hil_state.pitch; |
||||
hil_attitude.yaw = hil_state.yaw; |
||||
hil_attitude.rollspeed = hil_state.rollspeed; |
||||
hil_attitude.pitchspeed = hil_state.pitchspeed; |
||||
hil_attitude.yawspeed = hil_state.yawspeed; |
||||
|
||||
/* set timestamp and notify processes (broadcast) */ |
||||
hil_attitude.timestamp = hrt_absolute_time(); |
||||
orb_publish(ORB_ID(vehicle_attitude), pub_hil_attitude, &hil_attitude); |
||||
} |
||||
|
||||
if (msg->msgid == MAVLINK_MSG_ID_MANUAL_CONTROL) { |
||||
mavlink_manual_control_t man; |
||||
mavlink_msg_manual_control_decode(msg, &man); |
||||
|
||||
struct rc_channels_s rc_hil; |
||||
memset(&rc_hil, 0, sizeof(rc_hil)); |
||||
static orb_advert_t rc_pub = 0; |
||||
|
||||
rc_hil.timestamp = hrt_absolute_time(); |
||||
rc_hil.chan_count = 4; |
||||
|
||||
rc_hil.chan[0].scaled = man.x / 1000.0f; |
||||
rc_hil.chan[1].scaled = man.y / 1000.0f; |
||||
rc_hil.chan[2].scaled = man.r / 1000.0f; |
||||
rc_hil.chan[3].scaled = man.z / 1000.0f; |
||||
|
||||
struct manual_control_setpoint_s mc; |
||||
static orb_advert_t mc_pub = 0; |
||||
|
||||
int manual_sub = orb_subscribe(ORB_ID(manual_control_setpoint)); |
||||
|
||||
/* get a copy first, to prevent altering values that are not sent by the mavlink command */ |
||||
orb_copy(ORB_ID(manual_control_setpoint), manual_sub, &mc); |
||||
|
||||
mc.timestamp = rc_hil.timestamp; |
||||
mc.roll = man.x / 1000.0f; |
||||
mc.pitch = man.y / 1000.0f; |
||||
mc.yaw = man.r / 1000.0f; |
||||
mc.throttle = man.z / 1000.0f; |
||||
|
||||
/* fake RC channels with manual control input from simulator */ |
||||
|
||||
|
||||
if (rc_pub == 0) { |
||||
rc_pub = orb_advertise(ORB_ID(rc_channels), &rc_hil); |
||||
|
||||
} else { |
||||
orb_publish(ORB_ID(rc_channels), rc_pub, &rc_hil); |
||||
} |
||||
|
||||
if (mc_pub == 0) { |
||||
mc_pub = orb_advertise(ORB_ID(manual_control_setpoint), &mc); |
||||
|
||||
} else { |
||||
orb_publish(ORB_ID(manual_control_setpoint), mc_pub, &mc); |
||||
} |
||||
} |
||||
} |
||||
} |
||||
|
||||
|
||||
/**
|
||||
* Receive data from UART. |
||||
*/ |
||||
static void * |
||||
receive_thread(void *arg) |
||||
{ |
||||
int uart_fd = *((int *)arg); |
||||
|
||||
const int timeout = 1000; |
||||
uint8_t buf[32]; |
||||
|
||||
mavlink_message_t msg; |
||||
|
||||
prctl(PR_SET_NAME, "mavlink uart rcv", getpid()); |
||||
|
||||
while (!thread_should_exit) { |
||||
|
||||
struct pollfd fds[] = { { .fd = uart_fd, .events = POLLIN } }; |
||||
|
||||
if (poll(fds, 1, timeout) > 0) { |
||||
/* non-blocking read. read may return negative values */ |
||||
ssize_t nread = read(uart_fd, buf, sizeof(buf)); |
||||
|
||||
/* if read failed, this loop won't execute */ |
||||
for (ssize_t i = 0; i < nread; i++) { |
||||
if (mavlink_parse_char(chan, buf[i], &msg, &status)) { |
||||
/* handle generic messages and commands */ |
||||
handle_message(&msg); |
||||
|
||||
/* Handle packet with waypoint component */ |
||||
mavlink_wpm_message_handler(&msg, &global_pos, &local_pos); |
||||
|
||||
/* Handle packet with parameter component */ |
||||
mavlink_pm_message_handler(MAVLINK_COMM_0, &msg); |
||||
} |
||||
} |
||||
} |
||||
} |
||||
|
||||
return NULL; |
||||
} |
||||
|
||||
pthread_t |
||||
receive_start(int uart) |
||||
{ |
||||
pthread_attr_t receiveloop_attr; |
||||
pthread_attr_init(&receiveloop_attr); |
||||
|
||||
// set to non-blocking read
|
||||
int flags = fcntl(uart, F_GETFL, 0); |
||||
fcntl(uart, F_SETFL, flags | O_NONBLOCK); |
||||
|
||||
struct sched_param param; |
||||
param.sched_priority = SCHED_PRIORITY_MAX - 40; |
||||
(void)pthread_attr_setschedparam(&receiveloop_attr, ¶m); |
||||
|
||||
pthread_attr_setstacksize(&receiveloop_attr, 2048); |
||||
|
||||
pthread_t thread; |
||||
pthread_create(&thread, &receiveloop_attr, receive_thread, &uart); |
||||
return thread; |
||||
} |
Loading…
Reference in new issue