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https://gitee.com/mirrors_PX4/PX4-Autopilot.git
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975 lines
27 KiB
C++
975 lines
27 KiB
C++
/****************************************************************************
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*
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* Copyright (c) 2012-2014 PX4 Development Team. All rights reserved.
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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.cpp
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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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* @author Anton Babushkin <anton.babushkin@me.com>
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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 <drivers/drv_hrt.h>
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#include <drivers/drv_accel.h>
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#include <drivers/drv_gyro.h>
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#include <drivers/drv_mag.h>
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#include <drivers/drv_baro.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 <mathlib/mathlib.h>
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#include <systemlib/param/param.h>
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#include <systemlib/systemlib.h>
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#include <systemlib/err.h>
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#include <systemlib/airspeed.h>
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#include <mavlink/mavlink_log.h>
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#include <commander/px4_custom_mode.h>
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#include <geo/geo.h>
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__BEGIN_DECLS
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#include "mavlink_bridge_header.h"
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#include "mavlink_receiver.h"
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#include "mavlink_main.h"
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__END_DECLS
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static const float mg2ms2 = CONSTANTS_ONE_G / 1000.0f;
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MavlinkReceiver::MavlinkReceiver(Mavlink *parent) :
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_mavlink(parent),
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status{},
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hil_local_pos{},
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_control_mode{},
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_global_pos_pub(-1),
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_local_pos_pub(-1),
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_attitude_pub(-1),
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_gps_pub(-1),
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_sensors_pub(-1),
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_gyro_pub(-1),
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_accel_pub(-1),
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_mag_pub(-1),
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_baro_pub(-1),
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_airspeed_pub(-1),
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_battery_pub(-1),
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_cmd_pub(-1),
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_flow_pub(-1),
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_offboard_control_sp_pub(-1),
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_local_pos_sp_pub(-1),
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_global_vel_sp_pub(-1),
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_att_sp_pub(-1),
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_rates_sp_pub(-1),
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_vicon_position_pub(-1),
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_telemetry_status_pub(-1),
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_rc_pub(-1),
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_manual_pub(-1),
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_radio_status_available(false),
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_control_mode_sub(orb_subscribe(ORB_ID(vehicle_control_mode))),
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_hil_frames(0),
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_old_timestamp(0),
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_hil_local_proj_inited(0),
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_hil_local_alt0(0.0f),
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_hil_local_proj_ref{}
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{
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// make sure the FTP server is started
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(void)MavlinkFTP::getServer();
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}
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MavlinkReceiver::~MavlinkReceiver()
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{
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}
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void
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MavlinkReceiver::handle_message(mavlink_message_t *msg)
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{
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switch (msg->msgid) {
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case MAVLINK_MSG_ID_COMMAND_LONG:
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handle_message_command_long(msg);
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break;
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case MAVLINK_MSG_ID_OPTICAL_FLOW:
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handle_message_optical_flow(msg);
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break;
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case MAVLINK_MSG_ID_SET_MODE:
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handle_message_set_mode(msg);
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break;
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case MAVLINK_MSG_ID_VICON_POSITION_ESTIMATE:
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handle_message_vicon_position_estimate(msg);
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break;
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case MAVLINK_MSG_ID_RADIO_STATUS:
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handle_message_radio_status(msg);
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break;
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case MAVLINK_MSG_ID_MANUAL_CONTROL:
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handle_message_manual_control(msg);
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break;
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case MAVLINK_MSG_ID_HEARTBEAT:
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handle_message_heartbeat(msg);
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break;
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case MAVLINK_MSG_ID_REQUEST_DATA_STREAM:
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handle_message_request_data_stream(msg);
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break;
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case MAVLINK_MSG_ID_ENCAPSULATED_DATA:
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MavlinkFTP::getServer()->handle_message(_mavlink, msg);
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break;
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default:
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break;
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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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* Accept HIL GPS messages if use_hil_gps flag is true.
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* This allows to provide fake gps measurements to the system.
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*/
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if (_mavlink->get_hil_enabled()) {
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switch (msg->msgid) {
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case MAVLINK_MSG_ID_HIL_SENSOR:
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handle_message_hil_sensor(msg);
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break;
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case MAVLINK_MSG_ID_HIL_STATE_QUATERNION:
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handle_message_hil_state_quaternion(msg);
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break;
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default:
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break;
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}
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}
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if (_mavlink->get_hil_enabled() || (_mavlink->get_use_hil_gps() && msg->sysid == mavlink_system.sysid)) {
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switch (msg->msgid) {
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case MAVLINK_MSG_ID_HIL_GPS:
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handle_message_hil_gps(msg);
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break;
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default:
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break;
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}
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}
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/* If we've received a valid message, mark the flag indicating so.
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This is used in the '-w' command-line flag. */
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_mavlink->set_has_received_messages(true);
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}
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void
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MavlinkReceiver::handle_message_command_long(mavlink_message_t *msg)
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{
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/* command */
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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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warnx("terminated by remote command");
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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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_mavlink->_task_should_exit = true;
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} else {
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if (msg->sysid == mavlink_system.sysid && msg->compid == mavlink_system.compid) {
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warnx("ignoring CMD spoofed with same SYS/COMP (%d/%d) ID",
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mavlink_system.sysid, mavlink_system.compid);
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return;
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}
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struct vehicle_command_s vcmd;
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memset(&vcmd, 0, sizeof(vcmd));
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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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// XXX do proper translation
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vcmd.command = (enum VEHICLE_CMD)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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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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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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}
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void
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MavlinkReceiver::handle_message_optical_flow(mavlink_message_t *msg)
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{
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/* 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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memset(&f, 0, sizeof(f));
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f.timestamp = hrt_absolute_time();
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f.flow_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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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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orb_publish(ORB_ID(optical_flow), _flow_pub, &f);
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}
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}
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void
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MavlinkReceiver::handle_message_set_mode(mavlink_message_t *msg)
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{
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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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struct vehicle_command_s vcmd;
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memset(&vcmd, 0, sizeof(vcmd));
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union px4_custom_mode custom_mode;
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custom_mode.data = new_mode.custom_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 = custom_mode.main_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 = VEHICLE_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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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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orb_publish(ORB_ID(vehicle_command), _cmd_pub, &vcmd);
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}
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}
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void
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MavlinkReceiver::handle_message_vicon_position_estimate(mavlink_message_t *msg)
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{
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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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struct vehicle_vicon_position_s vicon_position;
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memset(&vicon_position, 0, sizeof(vicon_position));
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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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void
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MavlinkReceiver::handle_message_radio_status(mavlink_message_t *msg)
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{
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/* telemetry status supported only on first TELEMETRY_STATUS_ORB_ID_NUM mavlink channels */
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if (_mavlink->get_channel() < TELEMETRY_STATUS_ORB_ID_NUM) {
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mavlink_radio_status_t rstatus;
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mavlink_msg_radio_status_decode(msg, &rstatus);
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struct telemetry_status_s &tstatus = _mavlink->get_rx_status();
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tstatus.timestamp = hrt_absolute_time();
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tstatus.telem_time = tstatus.timestamp;
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/* tstatus.heartbeat_time is set by system heartbeats */
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tstatus.type = TELEMETRY_STATUS_RADIO_TYPE_3DR_RADIO;
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tstatus.rssi = rstatus.rssi;
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tstatus.remote_rssi = rstatus.remrssi;
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tstatus.txbuf = rstatus.txbuf;
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tstatus.noise = rstatus.noise;
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tstatus.remote_noise = rstatus.remnoise;
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tstatus.rxerrors = rstatus.rxerrors;
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tstatus.fixed = rstatus.fixed;
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if (_telemetry_status_pub < 0) {
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_telemetry_status_pub = orb_advertise(telemetry_status_orb_id[_mavlink->get_channel()], &tstatus);
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} else {
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orb_publish(telemetry_status_orb_id[_mavlink->get_channel()], _telemetry_status_pub, &tstatus);
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}
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/* this means that heartbeats alone won't be published to the radio status no more */
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_radio_status_available = true;
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}
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}
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void
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MavlinkReceiver::handle_message_manual_control(mavlink_message_t *msg)
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{
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mavlink_manual_control_t man;
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mavlink_msg_manual_control_decode(msg, &man);
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struct manual_control_setpoint_s manual;
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memset(&manual, 0, sizeof(manual));
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manual.timestamp = hrt_absolute_time();
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manual.x = man.x / 1000.0f;
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manual.y = man.y / 1000.0f;
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manual.r = man.r / 1000.0f;
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manual.z = man.z / 1000.0f;
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warnx("pitch: %.2f, roll: %.2f, yaw: %.2f, throttle: %.2f", (double)manual.x, (double)manual.y, (double)manual.r, (double)manual.z);
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if (_manual_pub < 0) {
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_manual_pub = orb_advertise(ORB_ID(manual_control_setpoint), &manual);
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} else {
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orb_publish(ORB_ID(manual_control_setpoint), _manual_pub, &manual);
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}
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}
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void
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MavlinkReceiver::handle_message_heartbeat(mavlink_message_t *msg)
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{
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/* telemetry status supported only on first TELEMETRY_STATUS_ORB_ID_NUM mavlink channels */
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if (_mavlink->get_channel() < TELEMETRY_STATUS_ORB_ID_NUM) {
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mavlink_heartbeat_t hb;
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mavlink_msg_heartbeat_decode(msg, &hb);
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/* ignore own heartbeats, accept only heartbeats from GCS */
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if (msg->sysid != mavlink_system.sysid && hb.type == MAV_TYPE_GCS) {
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struct telemetry_status_s &tstatus = _mavlink->get_rx_status();
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hrt_abstime tnow = hrt_absolute_time();
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/* always set heartbeat, publish only if telemetry link not up */
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tstatus.heartbeat_time = tnow;
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/* if no radio status messages arrive, lets at least publish that heartbeats were received */
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if (!_radio_status_available) {
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tstatus.timestamp = tnow;
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/* telem_time indicates the timestamp of a telemetry status packet and we got none */
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tstatus.telem_time = 0;
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tstatus.type = TELEMETRY_STATUS_RADIO_TYPE_GENERIC;
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if (_telemetry_status_pub < 0) {
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_telemetry_status_pub = orb_advertise(telemetry_status_orb_id[_mavlink->get_channel()], &tstatus);
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} else {
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orb_publish(telemetry_status_orb_id[_mavlink->get_channel()], _telemetry_status_pub, &tstatus);
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}
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}
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}
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}
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}
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void
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MavlinkReceiver::handle_message_request_data_stream(mavlink_message_t *msg)
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{
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mavlink_request_data_stream_t req;
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mavlink_msg_request_data_stream_decode(msg, &req);
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if (req.target_system == mavlink_system.sysid && req.target_component == mavlink_system.compid) {
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float rate = req.start_stop ? (1000.0f / req.req_message_rate) : 0.0f;
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MavlinkStream *stream;
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LL_FOREACH(_mavlink->get_streams(), stream) {
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if (req.req_stream_id == stream->get_id()) {
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_mavlink->configure_stream_threadsafe(stream->get_name(), rate);
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}
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}
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}
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}
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void
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MavlinkReceiver::handle_message_hil_sensor(mavlink_message_t *msg)
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{
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mavlink_hil_sensor_t imu;
|
|
mavlink_msg_hil_sensor_decode(msg, &imu);
|
|
|
|
uint64_t timestamp = hrt_absolute_time();
|
|
|
|
/* airspeed */
|
|
{
|
|
struct airspeed_s airspeed;
|
|
memset(&airspeed, 0, sizeof(airspeed));
|
|
|
|
float ias = calc_indicated_airspeed(imu.diff_pressure * 1e2f);
|
|
// XXX need to fix this
|
|
float tas = ias;
|
|
|
|
airspeed.timestamp = timestamp;
|
|
airspeed.indicated_airspeed_m_s = ias;
|
|
airspeed.true_airspeed_m_s = tas;
|
|
|
|
if (_airspeed_pub < 0) {
|
|
_airspeed_pub = orb_advertise(ORB_ID(airspeed), &airspeed);
|
|
|
|
} else {
|
|
orb_publish(ORB_ID(airspeed), _airspeed_pub, &airspeed);
|
|
}
|
|
}
|
|
|
|
/* gyro */
|
|
{
|
|
struct gyro_report gyro;
|
|
memset(&gyro, 0, sizeof(gyro));
|
|
|
|
gyro.timestamp = timestamp;
|
|
gyro.x_raw = imu.xgyro * 1000.0f;
|
|
gyro.y_raw = imu.ygyro * 1000.0f;
|
|
gyro.z_raw = imu.zgyro * 1000.0f;
|
|
gyro.x = imu.xgyro;
|
|
gyro.y = imu.ygyro;
|
|
gyro.z = imu.zgyro;
|
|
gyro.temperature = imu.temperature;
|
|
|
|
if (_gyro_pub < 0) {
|
|
_gyro_pub = orb_advertise(ORB_ID(sensor_gyro0), &gyro);
|
|
|
|
} else {
|
|
orb_publish(ORB_ID(sensor_gyro0), _gyro_pub, &gyro);
|
|
}
|
|
}
|
|
|
|
/* accelerometer */
|
|
{
|
|
struct accel_report accel;
|
|
memset(&accel, 0, sizeof(accel));
|
|
|
|
accel.timestamp = timestamp;
|
|
accel.x_raw = imu.xacc / mg2ms2;
|
|
accel.y_raw = imu.yacc / mg2ms2;
|
|
accel.z_raw = imu.zacc / mg2ms2;
|
|
accel.x = imu.xacc;
|
|
accel.y = imu.yacc;
|
|
accel.z = imu.zacc;
|
|
accel.temperature = imu.temperature;
|
|
|
|
if (_accel_pub < 0) {
|
|
_accel_pub = orb_advertise(ORB_ID(sensor_accel0), &accel);
|
|
|
|
} else {
|
|
orb_publish(ORB_ID(sensor_accel0), _accel_pub, &accel);
|
|
}
|
|
}
|
|
|
|
/* magnetometer */
|
|
{
|
|
struct mag_report mag;
|
|
memset(&mag, 0, sizeof(mag));
|
|
|
|
mag.timestamp = timestamp;
|
|
mag.x_raw = imu.xmag * 1000.0f;
|
|
mag.y_raw = imu.ymag * 1000.0f;
|
|
mag.z_raw = imu.zmag * 1000.0f;
|
|
mag.x = imu.xmag;
|
|
mag.y = imu.ymag;
|
|
mag.z = imu.zmag;
|
|
|
|
if (_mag_pub < 0) {
|
|
_mag_pub = orb_advertise(ORB_ID(sensor_mag0), &mag);
|
|
|
|
} else {
|
|
orb_publish(ORB_ID(sensor_mag0), _mag_pub, &mag);
|
|
}
|
|
}
|
|
|
|
/* baro */
|
|
{
|
|
struct baro_report baro;
|
|
memset(&baro, 0, sizeof(baro));
|
|
|
|
baro.timestamp = timestamp;
|
|
baro.pressure = imu.abs_pressure;
|
|
baro.altitude = imu.pressure_alt;
|
|
baro.temperature = imu.temperature;
|
|
|
|
if (_baro_pub < 0) {
|
|
_baro_pub = orb_advertise(ORB_ID(sensor_baro0), &baro);
|
|
|
|
} else {
|
|
orb_publish(ORB_ID(sensor_baro0), _baro_pub, &baro);
|
|
}
|
|
}
|
|
|
|
/* sensor combined */
|
|
{
|
|
struct sensor_combined_s hil_sensors;
|
|
memset(&hil_sensors, 0, sizeof(hil_sensors));
|
|
|
|
hil_sensors.timestamp = timestamp;
|
|
|
|
hil_sensors.gyro_raw[0] = imu.xgyro * 1000.0f;
|
|
hil_sensors.gyro_raw[1] = imu.ygyro * 1000.0f;
|
|
hil_sensors.gyro_raw[2] = imu.zgyro * 1000.0f;
|
|
hil_sensors.gyro_rad_s[0] = imu.xgyro;
|
|
hil_sensors.gyro_rad_s[1] = imu.ygyro;
|
|
hil_sensors.gyro_rad_s[2] = imu.zgyro;
|
|
|
|
hil_sensors.accelerometer_raw[0] = imu.xacc / mg2ms2;
|
|
hil_sensors.accelerometer_raw[1] = imu.yacc / mg2ms2;
|
|
hil_sensors.accelerometer_raw[2] = imu.zacc / mg2ms2;
|
|
hil_sensors.accelerometer_m_s2[0] = imu.xacc;
|
|
hil_sensors.accelerometer_m_s2[1] = imu.yacc;
|
|
hil_sensors.accelerometer_m_s2[2] = imu.zacc;
|
|
hil_sensors.accelerometer_mode = 0; // TODO what is this?
|
|
hil_sensors.accelerometer_range_m_s2 = 32.7f; // int16
|
|
hil_sensors.accelerometer_timestamp = timestamp;
|
|
|
|
hil_sensors.adc_voltage_v[0] = 0.0f;
|
|
hil_sensors.adc_voltage_v[1] = 0.0f;
|
|
hil_sensors.adc_voltage_v[2] = 0.0f;
|
|
|
|
hil_sensors.magnetometer_raw[0] = imu.xmag * 1000.0f;
|
|
hil_sensors.magnetometer_raw[1] = imu.ymag * 1000.0f;
|
|
hil_sensors.magnetometer_raw[2] = imu.zmag * 1000.0f;
|
|
hil_sensors.magnetometer_ga[0] = imu.xmag;
|
|
hil_sensors.magnetometer_ga[1] = imu.ymag;
|
|
hil_sensors.magnetometer_ga[2] = imu.zmag;
|
|
hil_sensors.magnetometer_range_ga = 32.7f; // int16
|
|
hil_sensors.magnetometer_mode = 0; // TODO what is this
|
|
hil_sensors.magnetometer_cuttoff_freq_hz = 50.0f;
|
|
hil_sensors.magnetometer_timestamp = timestamp;
|
|
|
|
hil_sensors.baro_pres_mbar = imu.abs_pressure;
|
|
hil_sensors.baro_alt_meter = imu.pressure_alt;
|
|
hil_sensors.baro_temp_celcius = imu.temperature;
|
|
hil_sensors.baro_timestamp = timestamp;
|
|
|
|
hil_sensors.differential_pressure_pa = imu.diff_pressure * 1e2f; //from hPa to Pa
|
|
hil_sensors.differential_pressure_timestamp = timestamp;
|
|
|
|
/* publish combined sensor topic */
|
|
if (_sensors_pub < 0) {
|
|
_sensors_pub = orb_advertise(ORB_ID(sensor_combined), &hil_sensors);
|
|
|
|
} else {
|
|
orb_publish(ORB_ID(sensor_combined), _sensors_pub, &hil_sensors);
|
|
}
|
|
}
|
|
|
|
/* battery status */
|
|
{
|
|
struct battery_status_s hil_battery_status;
|
|
memset(&hil_battery_status, 0, sizeof(hil_battery_status));
|
|
|
|
hil_battery_status.timestamp = timestamp;
|
|
hil_battery_status.voltage_v = 11.1f;
|
|
hil_battery_status.voltage_filtered_v = 11.1f;
|
|
hil_battery_status.current_a = 10.0f;
|
|
hil_battery_status.discharged_mah = -1.0f;
|
|
|
|
if (_battery_pub < 0) {
|
|
_battery_pub = orb_advertise(ORB_ID(battery_status), &hil_battery_status);
|
|
|
|
} else {
|
|
orb_publish(ORB_ID(battery_status), _battery_pub, &hil_battery_status);
|
|
}
|
|
}
|
|
|
|
/* increment counters */
|
|
_hil_frames++;
|
|
|
|
/* print HIL sensors rate */
|
|
if ((timestamp - _old_timestamp) > 10000000) {
|
|
printf("receiving HIL sensors at %d hz\n", _hil_frames / 10);
|
|
_old_timestamp = timestamp;
|
|
_hil_frames = 0;
|
|
}
|
|
}
|
|
|
|
void
|
|
MavlinkReceiver::handle_message_hil_gps(mavlink_message_t *msg)
|
|
{
|
|
mavlink_hil_gps_t gps;
|
|
mavlink_msg_hil_gps_decode(msg, &gps);
|
|
|
|
uint64_t timestamp = hrt_absolute_time();
|
|
|
|
struct vehicle_gps_position_s hil_gps;
|
|
memset(&hil_gps, 0, sizeof(hil_gps));
|
|
|
|
hil_gps.timestamp_time = timestamp;
|
|
hil_gps.time_gps_usec = gps.time_usec;
|
|
|
|
hil_gps.timestamp_position = timestamp;
|
|
hil_gps.lat = gps.lat;
|
|
hil_gps.lon = gps.lon;
|
|
hil_gps.alt = gps.alt;
|
|
hil_gps.eph = (float)gps.eph * 1e-2f; // from cm to m
|
|
hil_gps.epv = (float)gps.epv * 1e-2f; // from cm to m
|
|
|
|
hil_gps.timestamp_variance = timestamp;
|
|
hil_gps.s_variance_m_s = 5.0f;
|
|
|
|
hil_gps.timestamp_velocity = timestamp;
|
|
hil_gps.vel_m_s = (float)gps.vel * 1e-2f; // from cm/s to m/s
|
|
hil_gps.vel_n_m_s = gps.vn * 1e-2f; // from cm to m
|
|
hil_gps.vel_e_m_s = gps.ve * 1e-2f; // from cm to m
|
|
hil_gps.vel_d_m_s = gps.vd * 1e-2f; // from cm to m
|
|
hil_gps.vel_ned_valid = true;
|
|
hil_gps.cog_rad = _wrap_pi(gps.cog * M_DEG_TO_RAD_F * 1e-2f);
|
|
|
|
hil_gps.fix_type = gps.fix_type;
|
|
hil_gps.satellites_used = gps.satellites_visible; //TODO: rename mavlink_hil_gps_t sats visible to used?
|
|
|
|
if (_gps_pub < 0) {
|
|
_gps_pub = orb_advertise(ORB_ID(vehicle_gps_position), &hil_gps);
|
|
|
|
} else {
|
|
orb_publish(ORB_ID(vehicle_gps_position), _gps_pub, &hil_gps);
|
|
}
|
|
}
|
|
|
|
void
|
|
MavlinkReceiver::handle_message_hil_state_quaternion(mavlink_message_t *msg)
|
|
{
|
|
mavlink_hil_state_quaternion_t hil_state;
|
|
mavlink_msg_hil_state_quaternion_decode(msg, &hil_state);
|
|
|
|
uint64_t timestamp = hrt_absolute_time();
|
|
|
|
/* airspeed */
|
|
{
|
|
struct airspeed_s airspeed;
|
|
memset(&airspeed, 0, sizeof(airspeed));
|
|
|
|
airspeed.timestamp = timestamp;
|
|
airspeed.indicated_airspeed_m_s = hil_state.ind_airspeed * 1e-2f;
|
|
airspeed.true_airspeed_m_s = hil_state.true_airspeed * 1e-2f;
|
|
|
|
if (_airspeed_pub < 0) {
|
|
_airspeed_pub = orb_advertise(ORB_ID(airspeed), &airspeed);
|
|
|
|
} else {
|
|
orb_publish(ORB_ID(airspeed), _airspeed_pub, &airspeed);
|
|
}
|
|
}
|
|
|
|
/* attitude */
|
|
struct vehicle_attitude_s hil_attitude;
|
|
{
|
|
memset(&hil_attitude, 0, sizeof(hil_attitude));
|
|
math::Quaternion q(hil_state.attitude_quaternion);
|
|
math::Matrix<3, 3> C_nb = q.to_dcm();
|
|
math::Vector<3> euler = C_nb.to_euler();
|
|
|
|
hil_attitude.timestamp = timestamp;
|
|
memcpy(hil_attitude.R, C_nb.data, sizeof(hil_attitude.R));
|
|
hil_attitude.R_valid = true;
|
|
|
|
hil_attitude.q[0] = q(0);
|
|
hil_attitude.q[1] = q(1);
|
|
hil_attitude.q[2] = q(2);
|
|
hil_attitude.q[3] = q(3);
|
|
hil_attitude.q_valid = true;
|
|
|
|
hil_attitude.roll = euler(0);
|
|
hil_attitude.pitch = euler(1);
|
|
hil_attitude.yaw = euler(2);
|
|
hil_attitude.rollspeed = hil_state.rollspeed;
|
|
hil_attitude.pitchspeed = hil_state.pitchspeed;
|
|
hil_attitude.yawspeed = hil_state.yawspeed;
|
|
|
|
if (_attitude_pub < 0) {
|
|
_attitude_pub = orb_advertise(ORB_ID(vehicle_attitude), &hil_attitude);
|
|
|
|
} else {
|
|
orb_publish(ORB_ID(vehicle_attitude), _attitude_pub, &hil_attitude);
|
|
}
|
|
}
|
|
|
|
/* global position */
|
|
{
|
|
struct vehicle_global_position_s hil_global_pos;
|
|
memset(&hil_global_pos, 0, sizeof(hil_global_pos));
|
|
|
|
hil_global_pos.timestamp = timestamp;
|
|
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.vel_n = hil_state.vx / 100.0f;
|
|
hil_global_pos.vel_e = hil_state.vy / 100.0f;
|
|
hil_global_pos.vel_d = hil_state.vz / 100.0f;
|
|
hil_global_pos.yaw = hil_attitude.yaw;
|
|
hil_global_pos.eph = 2.0f;
|
|
hil_global_pos.epv = 4.0f;
|
|
|
|
if (_global_pos_pub < 0) {
|
|
_global_pos_pub = orb_advertise(ORB_ID(vehicle_global_position), &hil_global_pos);
|
|
|
|
} else {
|
|
orb_publish(ORB_ID(vehicle_global_position), _global_pos_pub, &hil_global_pos);
|
|
}
|
|
}
|
|
|
|
/* local position */
|
|
{
|
|
double lat = hil_state.lat * 1e-7;
|
|
double lon = hil_state.lon * 1e-7;
|
|
|
|
if (!_hil_local_proj_inited) {
|
|
_hil_local_proj_inited = true;
|
|
_hil_local_alt0 = hil_state.alt / 1000.0f;
|
|
map_projection_init(&_hil_local_proj_ref, hil_state.lat, hil_state.lon);
|
|
hil_local_pos.ref_timestamp = timestamp;
|
|
hil_local_pos.ref_lat = lat;
|
|
hil_local_pos.ref_lon = lon;
|
|
hil_local_pos.ref_alt = _hil_local_alt0;
|
|
}
|
|
|
|
float x;
|
|
float y;
|
|
map_projection_project(&_hil_local_proj_ref, lat, lon, &x, &y);
|
|
hil_local_pos.timestamp = timestamp;
|
|
hil_local_pos.xy_valid = true;
|
|
hil_local_pos.z_valid = true;
|
|
hil_local_pos.v_xy_valid = true;
|
|
hil_local_pos.v_z_valid = true;
|
|
hil_local_pos.x = x;
|
|
hil_local_pos.y = y;
|
|
hil_local_pos.z = _hil_local_alt0 - hil_state.alt / 1000.0f;
|
|
hil_local_pos.vx = hil_state.vx / 100.0f;
|
|
hil_local_pos.vy = hil_state.vy / 100.0f;
|
|
hil_local_pos.vz = hil_state.vz / 100.0f;
|
|
hil_local_pos.yaw = hil_attitude.yaw;
|
|
hil_local_pos.xy_global = true;
|
|
hil_local_pos.z_global = true;
|
|
|
|
bool landed = (float)(hil_state.alt) / 1000.0f < (_hil_local_alt0 + 0.1f); // XXX improve?
|
|
hil_local_pos.landed = landed;
|
|
|
|
if (_local_pos_pub < 0) {
|
|
_local_pos_pub = orb_advertise(ORB_ID(vehicle_local_position), &hil_local_pos);
|
|
|
|
} else {
|
|
orb_publish(ORB_ID(vehicle_local_position), _local_pos_pub, &hil_local_pos);
|
|
}
|
|
}
|
|
|
|
/* accelerometer */
|
|
{
|
|
struct accel_report accel;
|
|
memset(&accel, 0, sizeof(accel));
|
|
|
|
accel.timestamp = timestamp;
|
|
accel.x_raw = hil_state.xacc / CONSTANTS_ONE_G * 1e3f;
|
|
accel.y_raw = hil_state.yacc / CONSTANTS_ONE_G * 1e3f;
|
|
accel.z_raw = hil_state.zacc / CONSTANTS_ONE_G * 1e3f;
|
|
accel.x = hil_state.xacc;
|
|
accel.y = hil_state.yacc;
|
|
accel.z = hil_state.zacc;
|
|
accel.temperature = 25.0f;
|
|
|
|
if (_accel_pub < 0) {
|
|
_accel_pub = orb_advertise(ORB_ID(sensor_accel0), &accel);
|
|
|
|
} else {
|
|
orb_publish(ORB_ID(sensor_accel0), _accel_pub, &accel);
|
|
}
|
|
}
|
|
|
|
/* battery status */
|
|
{
|
|
struct battery_status_s hil_battery_status;
|
|
memset(&hil_battery_status, 0, sizeof(hil_battery_status));
|
|
|
|
hil_battery_status.timestamp = timestamp;
|
|
hil_battery_status.voltage_v = 11.1f;
|
|
hil_battery_status.voltage_filtered_v = 11.1f;
|
|
hil_battery_status.current_a = 10.0f;
|
|
hil_battery_status.discharged_mah = -1.0f;
|
|
|
|
if (_battery_pub < 0) {
|
|
_battery_pub = orb_advertise(ORB_ID(battery_status), &hil_battery_status);
|
|
|
|
} else {
|
|
orb_publish(ORB_ID(battery_status), _battery_pub, &hil_battery_status);
|
|
}
|
|
}
|
|
}
|
|
|
|
|
|
/**
|
|
* Receive data from UART.
|
|
*/
|
|
void *
|
|
MavlinkReceiver::receive_thread(void *arg)
|
|
{
|
|
int uart_fd = _mavlink->get_uart_fd();
|
|
|
|
const int timeout = 500;
|
|
uint8_t buf[32];
|
|
|
|
mavlink_message_t msg;
|
|
|
|
/* set thread name */
|
|
char thread_name[24];
|
|
sprintf(thread_name, "mavlink_rcv_if%d", _mavlink->get_instance_id());
|
|
prctl(PR_SET_NAME, thread_name, getpid());
|
|
|
|
struct pollfd fds[1];
|
|
fds[0].fd = uart_fd;
|
|
fds[0].events = POLLIN;
|
|
|
|
ssize_t nread = 0;
|
|
|
|
while (!_mavlink->_task_should_exit) {
|
|
if (poll(fds, 1, timeout) > 0) {
|
|
|
|
/* non-blocking read. read may return negative values */
|
|
if ((nread = read(uart_fd, buf, sizeof(buf))) < (ssize_t)sizeof(buf)) {
|
|
/* to avoid reading very small chunks wait for data before reading */
|
|
usleep(1000);
|
|
}
|
|
|
|
/* if read failed, this loop won't execute */
|
|
for (ssize_t i = 0; i < nread; i++) {
|
|
if (mavlink_parse_char(_mavlink->get_channel(), buf[i], &msg, &status)) {
|
|
/* handle generic messages and commands */
|
|
handle_message(&msg);
|
|
|
|
/* handle packet with parent object */
|
|
_mavlink->handle_message(&msg);
|
|
}
|
|
}
|
|
|
|
/* count received bytes */
|
|
_mavlink->count_rxbytes(nread);
|
|
}
|
|
}
|
|
|
|
return NULL;
|
|
}
|
|
|
|
void MavlinkReceiver::print_status()
|
|
{
|
|
|
|
}
|
|
|
|
void *MavlinkReceiver::start_helper(void *context)
|
|
{
|
|
MavlinkReceiver *rcv = new MavlinkReceiver((Mavlink *)context);
|
|
|
|
rcv->receive_thread(NULL);
|
|
|
|
delete rcv;
|
|
|
|
return nullptr;
|
|
}
|
|
|
|
pthread_t
|
|
MavlinkReceiver::receive_start(Mavlink *parent)
|
|
{
|
|
pthread_attr_t receiveloop_attr;
|
|
pthread_attr_init(&receiveloop_attr);
|
|
|
|
// set to non-blocking read
|
|
int flags = fcntl(parent->get_uart_fd(), F_GETFL, 0);
|
|
fcntl(parent->get_uart_fd(), F_SETFL, flags | O_NONBLOCK);
|
|
|
|
struct sched_param param;
|
|
(void)pthread_attr_getschedparam(&receiveloop_attr, ¶m);
|
|
param.sched_priority = SCHED_PRIORITY_MAX - 40;
|
|
(void)pthread_attr_setschedparam(&receiveloop_attr, ¶m);
|
|
|
|
pthread_attr_setstacksize(&receiveloop_attr, 2900);
|
|
pthread_t thread;
|
|
pthread_create(&thread, &receiveloop_attr, MavlinkReceiver::start_helper, (void *)parent);
|
|
|
|
pthread_attr_destroy(&receiveloop_attr);
|
|
return thread;
|
|
}
|