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/*===================================================================
======================================================================*/
/**
* @file
* @brief Represents one unmanned aerial vehicle
*
* @author Lorenz Meier <mavteam@student.ethz.ch>
*
*/
#include <QList>
#include <QMessageBox>
#include <QTimer>
#include <iostream>
#include <QDebug>
#include <cmath>
#include "UAS.h"
#include "LinkInterface.h"
#include "UASManager.h"
#include "LinkManager.h"
#include "SerialLink.h"
#ifndef M_PI
#define M_PI 3.14159265358979323846 /* pi */
#endif
#ifndef M_PI_2
#define M_PI_2 1.57079632679489661923 /* pi/2 */
#endif
#ifndef M_PI_4
#define M_PI_4 0.78539816339744830962 /* pi/4 */
#endif
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UAS::UAS(MAVLinkProtocol* protocol, int id) : UASInterface(),
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uasId(id),
startTime(MG::TIME::getGroundTimeNow()),
commStatus(COMM_DISCONNECTED),
name(""),
autopilot(-1),
links(new QList<LinkInterface*>()),
unknownPackets(),
mavlink(protocol),
waypointManager(*this),
thrustSum(0),
thrustMax(10),
startVoltage(0),
currentVoltage(12.0f),
lpVoltage(12.0f),
mode(MAV_MODE_UNINIT),
status(MAV_STATE_UNINIT),
onboardTimeOffset(0),
controlRollManual(true),
controlPitchManual(true),
controlYawManual(true),
controlThrustManual(true),
manualRollAngle(0),
manualPitchAngle(0),
manualYawAngle(0),
manualThrust(0),
receiveDropRate(0),
sendDropRate(0),
lowBattAlarm(false),
positionLock(false),
localX(0.0),
localY(0.0),
localZ(0.0),
latitude(0.0),
longitude(0.0),
altitude(0.0),
roll(0.0),
pitch(0.0),
yaw(0.0),
statusTimeout(new QTimer(this)),
paramsOnceRequested(false),
airframe(0)
color = UASInterface::getNextColor();
connect(statusTimeout, SIGNAL(timeout()), this, SLOT(updateState()));
connect(this, SIGNAL(systemSpecsChanged(int)), this, SLOT(writeSettings()));
void UAS::writeSettings()
{
QSettings settings;
settings.beginGroup(QString("MAV%1").arg(uasId));
settings.setValue("NAME", this->name);
settings.setValue("AIRFRAME", this->airframe);
settings.setValue("AP_TYPE", this->autopilot);
settings.endGroup();
settings.sync();
}
void UAS::readSettings()
{
QSettings settings;
settings.beginGroup(QString("MAV%1").arg(uasId));
this->name = settings.value("NAME", this->name).toString();
this->airframe = settings.value("AIRFRAME", this->airframe).toInt();
this->autopilot = settings.value("AP_TYPE", this->autopilot).toInt();
settings.endGroup();
}
int UAS::getUASID() const
void UAS::updateState()
{
// Check if heartbeat timed out
quint64 heartbeatInterval = QGC::groundTimeUsecs() - lastHeartbeat;
if (heartbeatInterval > timeoutIntervalHeartbeat)
{
emit heartbeatTimeout(heartbeatInterval);
emit heartbeatTimeout();
}
// Position lock is set by the MAVLink message handler
// if no position lock is available, indicate an error
if (positionLock)
{
positionLock = false;
}
else
{
{
GAudioOutput::instance()->notifyNegative();
}
}
}
if (UASManager::instance()->getActiveUAS() != this)
{
UASManager::instance()->setActiveUAS(this);
emit systemSelected(true);
}
}
bool UAS::getSelected() const
{
return (UASManager::instance()->getActiveUAS() == this);
void UAS::receiveMessageNamedValue(const mavlink_message_t& message)
{
if (message.msgid == MAVLINK_MSG_ID_NAMED_VALUE_FLOAT)
{
mavlink_named_value_float_t val;
mavlink_msg_named_value_float_decode(&message, &val);
emit valueChanged(this->getUASID(), QString(val.name), tr("raw"), val.value, getUnixTime(0));
}
else if (message.msgid == MAVLINK_MSG_ID_NAMED_VALUE_INT)
{
mavlink_named_value_int_t val;
mavlink_msg_named_value_int_decode(&message, &val);
emit valueChanged(this->getUASID(), QString(val.name), tr("raw"), (float)val.value, getUnixTime(0));
}
}
void UAS::receiveMessage(LinkInterface* link, mavlink_message_t message)
{
// qDebug() << __FILE__ << __LINE__ << "ADDED LINK!" << link->getName();
// else
// {
// qDebug() << __FILE__ << __LINE__ << "DID NOT ADD LINK" << link->getName() << "ALREADY IN LIST";
// }
// qDebug() << "UAS RECEIVED from" << message.sysid << "component" << message.compid << "msg id" << message.msgid << "seq no" << message.seq;
if (message.sysid == uasId)
{
QString uasState;
QString stateDescription;
QString patternPath;
// Receive named value message
receiveMessageNamedValue(message);
switch (message.msgid)
{
case MAVLINK_MSG_ID_HEARTBEAT:
if (this->type != mavlink_msg_heartbeat_get_type(&message))
this->type = mavlink_msg_heartbeat_get_type(&message);
if (airframe == 0)
{
switch (type)
{
case MAV_FIXED_WING:
setAirframe(UASInterface::QGC_AIRFRAME_EASYSTAR);
break;
case MAV_QUADROTOR:
setAirframe(UASInterface::QGC_AIRFRAME_CHEETAH);
break;
default:
// Do nothing
break;
}
}
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this->autopilot = mavlink_msg_heartbeat_get_autopilot(&message);
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break;
case MAVLINK_MSG_ID_BOOT:
getStatusForCode((int)MAV_STATE_BOOT, uasState, stateDescription);
emit statusChanged(this, uasState, stateDescription);
onboardTimeOffset = 0; // Reset offset measurement
break;
mavlink_sys_status_t state;
mavlink_msg_sys_status_decode(&message, &state);
//qDebug() << "SYSTEM NAV MODE:" << state.nav_mode;
QString audiostring = "System " + QString::number(this->getUASID());
QString stateAudio = "";
QString modeAudio = "";
bool statechanged = false;
bool modechanged = false;
getStatusForCode((int)state.status, uasState, stateDescription);
emit statusChanged(this, uasState, stateDescription);
emit statusChanged(this->status);
emit loadChanged(this,state.load/10.0f);
emit valueChanged(uasId, "Load", "%", ((float)state.load)/1000.0f, MG::TIME::getGroundTimeNow());
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stateAudio = " changed status to " + uasState;
mode = "GUIDED MODE";
break;
case (uint8_t)MAV_MODE_RC_TRAINING:
mode = "RC TRAINING MODE";
break;
default:
mode = "UNINIT MODE";
break;
}
emit modeChanged(this->getUASID(), mode, "");
modeAudio = " is now in " + mode;
}
if (startVoltage == 0) startVoltage = currentVoltage;
timeRemaining = calculateTimeRemaining();
//qDebug() << "Voltage: " << currentVoltage << " Chargelevel: " << getChargeLevel() << " Time remaining " << timeRemaining;
emit batteryChanged(this, lpVoltage, getChargeLevel(), timeRemaining);
emit voltageChanged(message.sysid, state.vbat/1000.0f);
// LOW BATTERY ALARM
float chargeLevel = getChargeLevel();
{
startLowBattAlarm();
}
else
{
stopLowBattAlarm();
}
emit dropRateChanged(this->getUASID(), state.packet_drop/1000.0f);
//qDebug() << __FILE__ << __LINE__ << "RCV LOSS: " << state.packet_drop;
if (modechanged && statechanged)
{
// Output both messages
audiostring += modeAudio + " and " + stateAudio;
}
else
{
// Output the one message
audiostring += modeAudio + stateAudio;
}
if ((int)state.status == (int)MAV_STATE_CRITICAL || state.status == (int)MAV_STATE_EMERGENCY)
{
GAudioOutput::instance()->startEmergency();
}
else if (modechanged || statechanged)
{
GAudioOutput::instance()->stopEmergency();
GAudioOutput::instance()->say(audiostring);
}
if (state.status == MAV_STATE_POWEROFF)
{
emit systemRemoved(this);
emit systemRemoved();
}
mavlink_raw_imu_t raw;
mavlink_msg_raw_imu_decode(&message, &raw);
quint64 time = getUnixTime(raw.usec);
emit valueChanged(uasId, "accel x", "raw", static_cast<double>(raw.xacc), time);
emit valueChanged(uasId, "accel y", "raw", static_cast<double>(raw.yacc), time);
emit valueChanged(uasId, "accel z", "raw", static_cast<double>(raw.zacc), time);
emit valueChanged(uasId, "gyro roll", "raw", static_cast<double>(raw.xgyro), time);
emit valueChanged(uasId, "gyro pitch", "raw", static_cast<double>(raw.ygyro), time);
emit valueChanged(uasId, "gyro yaw", "raw", static_cast<double>(raw.zgyro), time);
emit valueChanged(uasId, "mag x", "raw", static_cast<double>(raw.xmag), time);
emit valueChanged(uasId, "mag y", "raw", static_cast<double>(raw.ymag), time);
emit valueChanged(uasId, "mag z", "raw", static_cast<double>(raw.zmag), time);
}
break;
case MAVLINK_MSG_ID_ATTITUDE:
//std::cerr << std::endl;
//std::cerr << "Decoded attitude message:" << " roll: " << std::dec << mavlink_msg_attitude_get_roll(message.payload) << " pitch: " << mavlink_msg_attitude_get_pitch(message.payload) << " yaw: " << mavlink_msg_attitude_get_yaw(message.payload) << std::endl;
mavlink_attitude_t attitude;
mavlink_msg_attitude_decode(&message, &attitude);
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quint64 time = getUnixTime(attitude.usec);
roll = attitude.roll;
pitch = attitude.pitch;
yaw = attitude.yaw;
roll = QGC::limitAngleToPMPI(roll);
pitch = QGC::limitAngleToPMPI(pitch);
yaw = QGC::limitAngleToPMPI(yaw);
// emit valueChanged(uasId, "roll IMU", mavlink_msg_attitude_get_roll(&message), time);
// emit valueChanged(uasId, "pitch IMU", mavlink_msg_attitude_get_pitch(&message), time);
// emit valueChanged(uasId, "yaw IMU", mavlink_msg_attitude_get_yaw(&message), time);
emit valueChanged(uasId, "roll", "rad", mavlink_msg_attitude_get_roll(&message), time);
emit valueChanged(uasId, "pitch", "rad", mavlink_msg_attitude_get_pitch(&message), time);
emit valueChanged(uasId, "yaw", "rad", mavlink_msg_attitude_get_yaw(&message), time);
emit valueChanged(uasId, "rollspeed", "rad/s", attitude.rollspeed, time);
emit valueChanged(uasId, "pitchspeed", "rad/s", attitude.pitchspeed, time);
emit valueChanged(uasId, "yawspeed", "rad/s", attitude.yawspeed, time);
// Emit in angles
emit valueChanged(uasId, "roll", "deg", (attitude.roll/M_PI)*180.0, time);
emit valueChanged(uasId, "pitch", "deg", (attitude.pitch/M_PI)*180.0, time);
emit valueChanged(uasId, "rollspeed", "deg/s", (attitude.rollspeed/M_PI)*180.0, time);
emit valueChanged(uasId, "pitchspeed", "deg/s", (attitude.pitchspeed/M_PI)*180.0, time);
// Force yaw to 180 deg range
double yaw = ((attitude.yaw/M_PI)*180.0);
double sign = 1.0;
if (yaw < 0)
{
sign = -1.0;
yaw = -yaw;
}
while (yaw > 180.0)
{
yaw -= 180.0;
}
yaw *= sign;
emit valueChanged(uasId, "yaw", "deg", yaw, time);
emit valueChanged(uasId, "yawspeed", "deg/s", (attitude.yawspeed/M_PI)*180.0, time);
emit attitudeChanged(this, attitude.roll, attitude.pitch, attitude.yaw, time);
case MAVLINK_MSG_ID_LOCAL_POSITION:
//std::cerr << "Decoded attitude message:" << " roll: " << std::dec << mavlink_msg_attitude_get_roll(message.payload) << " pitch: " << mavlink_msg_attitude_get_pitch(message.payload) << " yaw: " << mavlink_msg_attitude_get_yaw(message.payload) << std::endl;
mavlink_local_position_t pos;
mavlink_msg_local_position_decode(&message, &pos);
quint64 time = getUnixTime(pos.usec);
localX = pos.x;
localY = pos.y;
localZ = pos.z;
emit valueChanged(uasId, "x", "m", pos.x, time);
emit valueChanged(uasId, "y", "m", pos.y, time);
emit valueChanged(uasId, "z", "m", pos.z, time);
emit valueChanged(uasId, "x speed", "m/s", pos.vx, time);
emit valueChanged(uasId, "y speed", "m/s", pos.vy, time);
emit valueChanged(uasId, "z speed", "m/s", pos.vz, time);
emit localPositionChanged(this, pos.x, pos.y, pos.z, time);
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emit speedChanged(this, pos.vx, pos.vy, pos.vz, time);
// qDebug()<<"Local Position = "<<pos.x<<" - "<<pos.y<<" - "<<pos.z;
// qDebug()<<"Speed Local Position = "<<pos.vx<<" - "<<pos.vy<<" - "<<pos.vz;
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//emit attitudeChanged(this, pos.roll, pos.pitch, pos.yaw, time);
// Set internal state
if (!positionLock)
{
// If position was not locked before, notify positive
GAudioOutput::instance()->notifyPositive();
}
positionLock = true;
case MAVLINK_MSG_ID_GLOBAL_POSITION_INT:
//std::cerr << std::endl;
//std::cerr << "Decoded attitude message:" << " roll: " << std::dec << mavlink_msg_attitude_get_roll(message.payload) << " pitch: " << mavlink_msg_attitude_get_pitch(message.payload) << " yaw: " << mavlink_msg_attitude_get_yaw(message.payload) << std::endl;
{
mavlink_global_position_int_t pos;
mavlink_msg_global_position_int_decode(&message, &pos);
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quint64 time = QGC::groundTimeUsecs()/1000;
latitude = pos.lat/(double)1E7;
longitude = pos.lon/(double)1E7;
altitude = pos.alt/1000.0;
speedX = pos.vx/100.0;
speedY = pos.vy/100.0;
speedZ = pos.vz/100.0;
emit valueChanged(uasId, "latitude", "deg", latitude, time);
emit valueChanged(uasId, "longitude", "deg", longitude, time);
emit valueChanged(uasId, "altitude", "m", altitude, time);
emit valueChanged(uasId, "gps x speed", "m/s", speedX, time);
emit valueChanged(uasId, "gps y speed", "m/s", speedY, time);
emit valueChanged(uasId, "gps z speed", "m/s", speedZ, time);
emit globalPositionChanged(this, longitude, latitude, altitude, time);
emit speedChanged(this, speedX, speedY, speedZ, time);
// Set internal state
if (!positionLock)
{
// If position was not locked before, notify positive
GAudioOutput::instance()->notifyPositive();
}
positionLock = true;
//TODO fix this hack for forwarding of global position for patch antenna tracking
forwardMessage(message);
}
break;
case MAVLINK_MSG_ID_GPS_RAW:
//std::cerr << std::endl;
//std::cerr << "Decoded attitude message:" << " roll: " << std::dec << mavlink_msg_attitude_get_roll(message.payload) << " pitch: " << mavlink_msg_attitude_get_pitch(message.payload) << " yaw: " << mavlink_msg_attitude_get_yaw(message.payload) << std::endl;
{
mavlink_gps_raw_t pos;
mavlink_msg_gps_raw_decode(&message, &pos);
// SANITY CHECK
// only accept values in a realistic range
// quint64 time = getUnixTime(pos.usec);
emit valueChanged(uasId, "latitude", "deg", pos.lat, time);
emit valueChanged(uasId, "longitude", "deg", pos.lon, time);
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// FIXME REMOVE
longitude = pos.lon;
latitude = pos.lat;
altitude = pos.alt;
emit globalPositionChanged(this, longitude, latitude, altitude, time);
emit globalPositionChanged(this, pos.lon, pos.lat, pos.alt, time);
// Check for NaN
int alt = pos.alt;
if (alt != alt)
{
alt = 0;
emit textMessageReceived(uasId, message.compid, 255, "GCS ERROR: RECEIVED NaN FOR ALTITUDE");
}
emit valueChanged(uasId, "altitude", "m", pos.alt, time);
// Smaller than threshold and not NaN
if (pos.v < 1000000 && pos.v == pos.v)
{
emit valueChanged(uasId, "speed", "m/s", pos.v, time);
// emit speedChanged(this, (double)pos.v, 0.0, 0.0, time);
}
else
{
emit textMessageReceived(uasId, message.compid, 255, QString("GCS ERROR: RECEIVED INVALID SPEED OF %1 m/s").arg(pos.v));
}
case MAVLINK_MSG_ID_GPS_STATUS:
{
mavlink_gps_status_t pos;
mavlink_msg_gps_status_decode(&message, &pos);
emit gpsSatelliteStatusChanged(uasId, (unsigned char)pos.satellite_prn[i], (unsigned char)pos.satellite_elevation[i], (unsigned char)pos.satellite_azimuth[i], (unsigned char)pos.satellite_snr[i], static_cast<bool>(pos.satellite_used[i]));
case MAVLINK_MSG_ID_GPS_LOCAL_ORIGIN_SET:
{
mavlink_gps_local_origin_set_t pos;
mavlink_msg_gps_local_origin_set_decode(&message, &pos);
// FIXME Emit to other components
}
break;
case MAVLINK_MSG_ID_RAW_PRESSURE:
{
mavlink_raw_pressure_t pressure;
mavlink_msg_raw_pressure_decode(&message, &pressure);
quint64 time = this->getUnixTime(0);
emit valueChanged(uasId, "abs pressure", "hP", pressure.press_abs, time);
emit valueChanged(uasId, "diff pressure 1", "hP", pressure.press_diff1, time);
emit valueChanged(uasId, "diff pressure 2", "hP", pressure.press_diff2, time);
}
break;
case MAVLINK_MSG_ID_RC_CHANNELS_RAW:
mavlink_rc_channels_raw_t channels;
mavlink_msg_rc_channels_raw_decode(&message, &channels);
emit remoteControlRSSIChanged(channels.rssi/255.0f);
emit remoteControlChannelRawChanged(0, channels.chan1_raw);
emit remoteControlChannelRawChanged(1, channels.chan2_raw);
emit remoteControlChannelRawChanged(2, channels.chan3_raw);
emit remoteControlChannelRawChanged(3, channels.chan4_raw);
emit remoteControlChannelRawChanged(4, channels.chan5_raw);
emit remoteControlChannelRawChanged(5, channels.chan6_raw);
emit remoteControlChannelRawChanged(6, channels.chan7_raw);
emit remoteControlChannelRawChanged(7, channels.chan8_raw);
}
break;
case MAVLINK_MSG_ID_RC_CHANNELS_SCALED:
{
mavlink_rc_channels_scaled_t channels;
mavlink_msg_rc_channels_scaled_decode(&message, &channels);
emit remoteControlRSSIChanged(channels.rssi/255.0f);
emit remoteControlChannelScaledChanged(0, channels.chan1_scaled/10000.0f);
emit remoteControlChannelScaledChanged(1, channels.chan2_scaled/10000.0f);
emit remoteControlChannelScaledChanged(2, channels.chan3_scaled/10000.0f);
emit remoteControlChannelScaledChanged(3, channels.chan4_scaled/10000.0f);
emit remoteControlChannelScaledChanged(4, channels.chan5_scaled/10000.0f);
emit remoteControlChannelScaledChanged(5, channels.chan6_scaled/10000.0f);
emit remoteControlChannelScaledChanged(6, channels.chan7_scaled/10000.0f);
emit remoteControlChannelScaledChanged(7, channels.chan8_scaled/10000.0f);
case MAVLINK_MSG_ID_PARAM_VALUE:
{
mavlink_param_value_t value;
mavlink_msg_param_value_decode(&message, &value);
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QString parameterName = QString((char*)value.param_id);
int component = message.compid;
float val = value.param_value;
// Insert component if necessary
if (!parameters.contains(component))
{
parameters.insert(component, new QMap<QString, float>());
}
// Insert parameter into registry
if (parameters.value(component)->contains(parameterName)) parameters.value(component)->remove(parameterName);
parameters.value(component)->insert(parameterName, val);
// Emit change
emit parameterChanged(uasId, message.compid, parameterName, val);
}
break;
emit valueChanged(uasId, QString("debug ") + QString::number(mavlink_msg_debug_get_ind(&message)), "raw", mavlink_msg_debug_get_value(&message), MG::TIME::getGroundTimeNow());
case MAVLINK_MSG_ID_ATTITUDE_CONTROLLER_OUTPUT:
{
mavlink_attitude_controller_output_t out;
mavlink_msg_attitude_controller_output_decode(&message, &out);
quint64 time = MG::TIME::getGroundTimeNowUsecs();
emit attitudeThrustSetPointChanged(this, out.roll/127.0f, out.pitch/127.0f, out.yaw/127.0f, (uint8_t)out.thrust, time);
emit valueChanged(uasId, "att control roll", "raw", out.roll, time/1000.0f);
emit valueChanged(uasId, "att control pitch", "raw", out.pitch, time/1000.0f);
emit valueChanged(uasId, "att control yaw", "raw", out.yaw, time/1000.0f);
}
break;
case MAVLINK_MSG_ID_POSITION_CONTROLLER_OUTPUT:
{
mavlink_position_controller_output_t out;
mavlink_msg_position_controller_output_decode(&message, &out);
//emit positionSetPointsChanged(uasId, out.x/127.0f, out.y/127.0f, out.z/127.0f, out.yaw, time);
emit valueChanged(uasId, "pos control x", "raw", out.x, time);
emit valueChanged(uasId, "pos control y", "raw", out.y, time);
emit valueChanged(uasId, "pos control z", "raw", out.z, time);
case MAVLINK_MSG_ID_WAYPOINT_COUNT:
{
mavlink_waypoint_count_t wpc;
mavlink_msg_waypoint_count_decode(&message, &wpc);
if (wpc.target_system == mavlink->getSystemId() && wpc.target_component == mavlink->getComponentId())
{
waypointManager.handleWaypointCount(message.sysid, message.compid, wpc.count);
}
case MAVLINK_MSG_ID_WAYPOINT:
mavlink_waypoint_t wp;
mavlink_msg_waypoint_decode(&message, &wp);
//qDebug() << "got waypoint (" << wp.seq << ") from ID " << message.sysid << " x=" << wp.x << " y=" << wp.y << " z=" << wp.z;
if(wp.target_system == mavlink->getSystemId() && wp.target_component == mavlink->getComponentId())
{
waypointManager.handleWaypoint(message.sysid, message.compid, &wp);
}
case MAVLINK_MSG_ID_WAYPOINT_ACK:
{
mavlink_waypoint_ack_t wpa;
mavlink_msg_waypoint_ack_decode(&message, &wpa);
if(wpa.target_system == mavlink->getSystemId() && wpa.target_component == mavlink->getComponentId())
{
waypointManager.handleWaypointAck(message.sysid, message.compid, &wpa);
}
}
break;
case MAVLINK_MSG_ID_WAYPOINT_REQUEST:
{
mavlink_waypoint_request_t wpr;
mavlink_msg_waypoint_request_decode(&message, &wpr);
if(wpr.target_system == mavlink->getSystemId() && wpr.target_component == mavlink->getComponentId())
{
waypointManager.handleWaypointRequest(message.sysid, message.compid, &wpr);
}
case MAVLINK_MSG_ID_WAYPOINT_REACHED:
mavlink_waypoint_reached_t wpr;
mavlink_msg_waypoint_reached_decode(&message, &wpr);
waypointManager.handleWaypointReached(message.sysid, message.compid, &wpr);
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case MAVLINK_MSG_ID_WAYPOINT_CURRENT:
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mavlink_waypoint_current_t wpc;
mavlink_msg_waypoint_current_decode(&message, &wpc);
waypointManager.handleWaypointCurrent(message.sysid, message.compid, &wpc);
case MAVLINK_MSG_ID_LOCAL_POSITION_SETPOINT:
{
mavlink_local_position_setpoint_t p;
mavlink_msg_local_position_setpoint_decode(&message, &p);
emit positionSetPointsChanged(uasId, p.x, p.y, p.z, p.yaw, QGC::groundTimeUsecs());
}
break;
case MAVLINK_MSG_ID_STATUSTEXT:
mavlink_msg_statustext_get_text(&message, (int8_t*)b.data());
int severity = mavlink_msg_statustext_get_severity(&message);
//qDebug() << "RECEIVED STATUS:" << text;false
emit textMessageReceived(uasId, message.compid, severity, text);
case MAVLINK_MSG_ID_DEBUG_VECT:
{
mavlink_debug_vect_t vect;
mavlink_msg_debug_vect_decode(&message, &vect);
QString str((const char*)vect.name);
quint64 time = getUnixTime(vect.usec);
emit valueChanged(uasId, str+".x", "raw", vect.x, time);
emit valueChanged(uasId, str+".y", "raw", vect.y, time);
emit valueChanged(uasId, str+".z", "raw", vect.z, time);
//#ifdef MAVLINK_ENABLED_PIXHAWK
// case MAVLINK_MSG_ID_POINT_OF_INTEREST:
// {
// mavlink_point_of_interest_t poi;
// mavlink_msg_point_of_interest_decode(&message, &poi);
// emit poiFound(this, poi.type, poi.color, QString((QChar*)poi.name, MAVLINK_MSG_POINT_OF_INTEREST_FIELD_NAME_LEN), poi.x, poi.y, poi.z);
// }
// break;
// case MAVLINK_MSG_ID_POINT_OF_INTEREST_CONNECTION:
// {
// mavlink_point_of_interest_connection_t poi;
// mavlink_msg_point_of_interest_connection_decode(&message, &poi);
// emit poiConnectionFound(this, poi.type, poi.color, QString((QChar*)poi.name, MAVLINK_MSG_POINT_OF_INTEREST_CONNECTION_FIELD_NAME_LEN), poi.x1, poi.y1, poi.z1, poi.x2, poi.y2, poi.z2);
// }
// break;
//#endif
case MAVLINK_MSG_ID_NAV_FILTER_BIAS:
{
mavlink_nav_filter_bias_t bias;
mavlink_msg_nav_filter_bias_decode(&message, &bias);
quint64 time = MG::TIME::getGroundTimeNow();
emit valueChanged(uasId, "b_f[0]", "raw", bias.accel_0, time);
emit valueChanged(uasId, "b_f[1]", "raw", bias.accel_1, time);
emit valueChanged(uasId, "b_f[2]", "raw", bias.accel_2, time);
emit valueChanged(uasId, "b_w[0]", "raw", bias.gyro_0, time);
emit valueChanged(uasId, "b_w[1]", "raw", bias.gyro_1, time);
emit valueChanged(uasId, "b_w[2]", "raw", bias.gyro_2, time);
case MAVLINK_MSG_ID_RADIO_CALIBRATION:
{
mavlink_radio_calibration_t radioMsg;
mavlink_msg_radio_calibration_decode(&message, &radioMsg);
QVector<float> aileron;
QVector<float> elevator;
QVector<float> rudder;
QVector<float> gyro;
QVector<float> pitch;
QVector<float> throttle;
for (int i=0; i<MAVLINK_MSG_RADIO_CALIBRATION_FIELD_AILERON_LEN; ++i)
aileron << radioMsg.aileron[i];
for (int i=0; i<MAVLINK_MSG_RADIO_CALIBRATION_FIELD_ELEVATOR_LEN; ++i)
elevator << radioMsg.elevator[i];
for (int i=0; i<MAVLINK_MSG_RADIO_CALIBRATION_FIELD_RUDDER_LEN; ++i)
rudder << radioMsg.rudder[i];
for (int i=0; i<MAVLINK_MSG_RADIO_CALIBRATION_FIELD_GYRO_LEN; ++i)
gyro << radioMsg.gyro[i];
for (int i=0; i<MAVLINK_MSG_RADIO_CALIBRATION_FIELD_PITCH_LEN; ++i)
pitch << radioMsg.pitch[i];
for (int i=0; i<MAVLINK_MSG_RADIO_CALIBRATION_FIELD_THROTTLE_LEN; ++i)
throttle << radioMsg.throttle[i];
QPointer<RadioCalibrationData> radioData = new RadioCalibrationData(aileron, elevator, rudder, gyro, pitch, throttle);
emit radioCalibrationReceived(radioData);
delete radioData;
}
break;
{
if (!unknownPackets.contains(message.msgid))
{
unknownPackets.append(message.msgid);
//GAudioOutput::instance()->say("UNABLE TO DECODE MESSAGE WITH ID " + QString::number(message.msgid) + " FROM SYSTEM " + QString::number(message.sysid));
std::cout << "Unable to decode message from system " << std::dec << static_cast<int>(message.sysid) << " with message id:" << static_cast<int>(message.msgid) << std::endl;
//qDebug() << std::cerr << "Unable to decode message from system " << std::dec << static_cast<int>(message.acid) << " with message id:" << static_cast<int>(message.msgid) << std::endl;
}
}
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void UAS::setLocalOriginAtCurrentGPSPosition()
{
bool result = false;
QMessageBox msgBox;
msgBox.setIcon(QMessageBox::Warning);
msgBox.setText("Setting new World Coordinate Frame Origin");
msgBox.setInformativeText("Do you want to set a new origin? Waypoints defined in the local frame will be shifted in their physical location");
msgBox.setStandardButtons(QMessageBox::Yes | QMessageBox::Cancel);
msgBox.setDefaultButton(QMessageBox::Cancel);
int ret = msgBox.exec();
// Close the message box shortly after the click to prevent accidental clicks
QTimer::singleShot(5000, &msgBox, SLOT(reject()));
if (ret == QMessageBox::Yes)
{
mavlink_message_t msg;
mavlink_msg_action_pack(mavlink->getSystemId(), mavlink->getSystemId(), &msg, this->getUASID(), 0, MAV_ACTION_SET_ORIGIN);
// Send message twice to increase chance that it reaches its goal
sendMessage(msg);
// Wait 5 ms
MG::SLEEP::usleep(5000);
// Send again
sendMessage(msg);
result = true;
}
}
void UAS::setLocalPositionSetpoint(float x, float y, float z, float yaw)
{
#ifdef MAVLINK_ENABLED_PIXHAWK
mavlink_msg_position_control_setpoint_set_pack(mavlink->getSystemId(), mavlink->getComponentId(), &msg, uasId, 0, 0, x, y, z, yaw);
sendMessage(msg);
#else
Q_UNUSED(x);
Q_UNUSED(y);
Q_UNUSED(z);
Q_UNUSED(yaw);
#endif
void UAS::setLocalPositionOffset(float x, float y, float z, float yaw)
{
mavlink_message_t msg;
mavlink_msg_position_control_offset_set_pack(mavlink->getSystemId(), mavlink->getComponentId(), &msg, uasId, 0, x, y, z, yaw);
sendMessage(msg);
Q_UNUSED(x);
Q_UNUSED(y);
Q_UNUSED(z);
Q_UNUSED(yaw);
#endif
}
void UAS::startRadioControlCalibration()
{
mavlink_message_t msg;
mavlink_msg_action_pack(mavlink->getSystemId(), mavlink->getComponentId(), &msg, uasId, MAV_COMP_ID_IMU, MAV_ACTION_CALIBRATE_RC);
sendMessage(msg);
mavlink_message_t msg;
mavlink_msg_action_pack(mavlink->getSystemId(), mavlink->getComponentId(), &msg, uasId, MAV_COMP_ID_IMU, MAV_ACTION_REC_START);
sendMessage(msg);
mavlink_message_t msg;
mavlink_msg_action_pack(mavlink->getSystemId(), mavlink->getComponentId(), &msg, uasId, MAV_COMP_ID_IMU, MAV_ACTION_REC_PAUSE);
sendMessage(msg);
mavlink_message_t msg;
mavlink_msg_action_pack(mavlink->getSystemId(), mavlink->getComponentId(), &msg, uasId, MAV_COMP_ID_IMU, MAV_ACTION_REC_STOP);
sendMessage(msg);
void UAS::startMagnetometerCalibration()
{
mavlink_message_t msg;
mavlink_msg_action_pack(mavlink->getSystemId(), mavlink->getComponentId(), &msg, uasId, MAV_COMP_ID_IMU, MAV_ACTION_CALIBRATE_MAG);
sendMessage(msg);
}
void UAS::startGyroscopeCalibration()
{
mavlink_message_t msg;
mavlink_msg_action_pack(mavlink->getSystemId(), mavlink->getComponentId(), &msg, uasId, MAV_COMP_ID_IMU, MAV_ACTION_CALIBRATE_GYRO);
sendMessage(msg);
}
void UAS::startPressureCalibration()
{
mavlink_message_t msg;
mavlink_msg_action_pack(mavlink->getSystemId(), mavlink->getComponentId(), &msg, uasId, MAV_COMP_ID_IMU, MAV_ACTION_CALIBRATE_PRESSURE);
sendMessage(msg);
}
quint64 UAS::getUnixTime(quint64 time)
{
if (time == 0)
{
return MG::TIME::getGroundTimeNow();
}
// Check if time is smaller than 40 years,
// assuming no system without Unix timestamp
// runs longer than 40 years continuously without
// reboot. In worst case this will add/subtract the
// communication delay between GCS and MAV,
// it will never alter the timestamp in a safety
// critical way.
//
// Calculation:
// 40 years
// 365 days
// 24 hours
// 60 minutes
// 60 seconds
// 1000 milliseconds
// 1000 microseconds
#ifndef _MSC_VER
else if (time < 1261440000000000LLU)
else if (time < 1261440000000000)
if (onboardTimeOffset == 0)
{
onboardTimeOffset = MG::TIME::getGroundTimeNow() - time/1000;
}
return time/1000 + onboardTimeOffset;
}
else
{
// Time is not zero and larger than 40 years -> has to be
// a Unix epoch timestamp. Do nothing.
return time/1000;
}
}
lm
committed
QList<QString> UAS::getParameterNames(int component)
{
if (parameters.contains(component))
{
return parameters.value(component)->keys();
}
else
{
return QList<QString>();
}
}
QList<int> UAS::getComponentIds()
{
return parameters.keys();
}
if ((uint8_t)mode >= MAV_MODE_LOCKED && (uint8_t)mode <= MAV_MODE_RC_TRAINING)
mavlink_msg_set_mode_pack(mavlink->getSystemId(), mavlink->getComponentId(), &msg, (uint8_t)uasId, (uint8_t)mode);
qDebug() << "SENDING REQUEST TO SET MODE TO SYSTEM" << uasId << ", REQUEST TO SET MODE " << (uint8_t)mode;