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void Vehicle::_handleDistanceSensor(mavlink_message_t& message)
{
mavlink_distance_sensor_t distanceSensor;
mavlink_msg_distance_sensor_decode(&message, &distanceSensor);\
if (!_distanceSensorFactGroup.idSet()) {
_distanceSensorFactGroup.setIdSet(true);
_distanceSensorFactGroup.setId(distanceSensor.id);
if (_distanceSensorFactGroup.id() != distanceSensor.id) {
// We can only handle a single sensor reporting
return;
}
struct orientation2Fact_s {
MAV_SENSOR_ORIENTATION orientation;
Fact* fact;
};
orientation2Fact_s rgOrientation2Fact[] =
{
{ MAV_SENSOR_ROTATION_NONE, _distanceSensorFactGroup.rotationNone() },
{ MAV_SENSOR_ROTATION_YAW_45, _distanceSensorFactGroup.rotationYaw45() },
{ MAV_SENSOR_ROTATION_YAW_90, _distanceSensorFactGroup.rotationYaw90() },
{ MAV_SENSOR_ROTATION_YAW_135, _distanceSensorFactGroup.rotationYaw135() },
{ MAV_SENSOR_ROTATION_YAW_180, _distanceSensorFactGroup.rotationYaw180() },
{ MAV_SENSOR_ROTATION_YAW_225, _distanceSensorFactGroup.rotationYaw225() },
{ MAV_SENSOR_ROTATION_YAW_270, _distanceSensorFactGroup.rotationYaw270() },
{ MAV_SENSOR_ROTATION_YAW_315, _distanceSensorFactGroup.rotationYaw315() },
{ MAV_SENSOR_ROTATION_PITCH_90, _distanceSensorFactGroup.rotationPitch90() },
{ MAV_SENSOR_ROTATION_PITCH_270, _distanceSensorFactGroup.rotationPitch270() },
};
for (size_t i=0; i<sizeof(rgOrientation2Fact)/sizeof(rgOrientation2Fact[0]); i++) {
const orientation2Fact_s& orientation2Fact = rgOrientation2Fact[i];
if (orientation2Fact.orientation == distanceSensor.orientation) {
orientation2Fact.fact->setRawValue(distanceSensor.current_distance / 100.0); // cm to meters
void Vehicle::_handleAttitudeTarget(mavlink_message_t& message)
{
mavlink_attitude_target_t attitudeTarget;
mavlink_msg_attitude_target_decode(&message, &attitudeTarget);
float roll, pitch, yaw;
mavlink_quaternion_to_euler(attitudeTarget.q, &roll, &pitch, &yaw);
_setpointFactGroup.roll()->setRawValue(qRadiansToDegrees(roll));
_setpointFactGroup.pitch()->setRawValue(qRadiansToDegrees(pitch));
_setpointFactGroup.yaw()->setRawValue(qRadiansToDegrees(yaw));
_setpointFactGroup.rollRate()->setRawValue(qRadiansToDegrees(attitudeTarget.body_roll_rate));
_setpointFactGroup.pitchRate()->setRawValue(qRadiansToDegrees(attitudeTarget.body_pitch_rate));
_setpointFactGroup.yawRate()->setRawValue(qRadiansToDegrees(attitudeTarget.body_yaw_rate));
}
void Vehicle::_handleAttitudeWorker(double rollRadians, double pitchRadians, double yawRadians)
double roll, pitch, yaw;
roll = QGC::limitAngleToPMPIf(rollRadians);
pitch = QGC::limitAngleToPMPIf(pitchRadians);
yaw = QGC::limitAngleToPMPIf(yawRadians);
roll = qRadiansToDegrees(roll);
pitch = qRadiansToDegrees(pitch);
yaw = qRadiansToDegrees(yaw);
if (yaw < 0.0) {
yaw += 360.0;
}
// truncate to integer so widget never displays 360
yaw = trunc(yaw);
_rollFact.setRawValue(roll);
_pitchFact.setRawValue(pitch);
_headingFact.setRawValue(yaw);
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}
void Vehicle::_handleAttitude(mavlink_message_t& message)
{
if (_receivingAttitudeQuaternion) {
return;
}
mavlink_attitude_t attitude;
mavlink_msg_attitude_decode(&message, &attitude);
_handleAttitudeWorker(attitude.roll, attitude.pitch, attitude.yaw);
}
void Vehicle::_handleAttitudeQuaternion(mavlink_message_t& message)
{
_receivingAttitudeQuaternion = true;
mavlink_attitude_quaternion_t attitudeQuaternion;
mavlink_msg_attitude_quaternion_decode(&message, &attitudeQuaternion);
float roll, pitch, yaw;
float q[] = { attitudeQuaternion.q1, attitudeQuaternion.q2, attitudeQuaternion.q3, attitudeQuaternion.q4 };
mavlink_quaternion_to_euler(q, &roll, &pitch, &yaw);
_handleAttitudeWorker(roll, pitch, yaw);
rollRate()->setRawValue(qRadiansToDegrees(attitudeQuaternion.rollspeed));
pitchRate()->setRawValue(qRadiansToDegrees(attitudeQuaternion.pitchspeed));
yawRate()->setRawValue(qRadiansToDegrees(attitudeQuaternion.yawspeed));
void Vehicle::_handleGpsRawInt(mavlink_message_t& message)
{
mavlink_gps_raw_int_t gpsRawInt;
mavlink_msg_gps_raw_int_decode(&message, &gpsRawInt);
_gpsRawIntMessageAvailable = true;
if (gpsRawInt.fix_type >= GPS_FIX_TYPE_3D_FIX) {
if (!_globalPositionIntMessageAvailable) {
QGeoCoordinate newPosition(gpsRawInt.lat / (double)1E7, gpsRawInt.lon / (double)1E7, gpsRawInt.alt / 1000.0);
if (newPosition != _coordinate) {
_coordinate = newPosition;
emit coordinateChanged(_coordinate);
}
_altitudeAMSLFact.setRawValue(gpsRawInt.alt / 1000.0);
}
}
_gpsFactGroup.lat()->setRawValue(gpsRawInt.lat * 1e-7);
_gpsFactGroup.lon()->setRawValue(gpsRawInt.lon * 1e-7);
_gpsFactGroup.count()->setRawValue(gpsRawInt.satellites_visible == 255 ? 0 : gpsRawInt.satellites_visible);
_gpsFactGroup.hdop()->setRawValue(gpsRawInt.eph == UINT16_MAX ? std::numeric_limits<double>::quiet_NaN() : gpsRawInt.eph / 100.0);
_gpsFactGroup.vdop()->setRawValue(gpsRawInt.epv == UINT16_MAX ? std::numeric_limits<double>::quiet_NaN() : gpsRawInt.epv / 100.0);
_gpsFactGroup.courseOverGround()->setRawValue(gpsRawInt.cog == UINT16_MAX ? std::numeric_limits<double>::quiet_NaN() : gpsRawInt.cog / 100.0);
_gpsFactGroup.lock()->setRawValue(gpsRawInt.fix_type);
}
void Vehicle::_handleGlobalPositionInt(mavlink_message_t& message)
{
mavlink_global_position_int_t globalPositionInt;
mavlink_msg_global_position_int_decode(&message, &globalPositionInt);
_altitudeRelativeFact.setRawValue(globalPositionInt.relative_alt / 1000.0);
_altitudeAMSLFact.setRawValue(globalPositionInt.alt / 1000.0);
// ArduPilot sends bogus GLOBAL_POSITION_INT messages with lat/lat 0/0 even when it has no gps signal
// Apparently, this is in order to transport relative altitude information.
if (globalPositionInt.lat == 0 && globalPositionInt.lon == 0) {
_globalPositionIntMessageAvailable = true;
QGeoCoordinate newPosition(globalPositionInt.lat / (double)1E7, globalPositionInt.lon / (double)1E7, globalPositionInt.alt / 1000.0);
if (newPosition != _coordinate) {
_coordinate = newPosition;
emit coordinateChanged(_coordinate);
}
void Vehicle::_handleHighLatency2(mavlink_message_t& message)
{
mavlink_high_latency2_t highLatency2;
mavlink_msg_high_latency2_decode(&message, &highLatency2);
QString previousFlightMode;
if (_base_mode != 0 || _custom_mode != 0){
// Vehicle is initialized with _base_mode=0 and _custom_mode=0. Don't pass this to flightMode() since it will complain about
// bad modes while unit testing.
previousFlightMode = flightMode();
}
_base_mode = MAV_MODE_FLAG_CUSTOM_MODE_ENABLED;
_custom_mode = _firmwarePlugin->highLatencyCustomModeTo32Bits(highLatency2.custom_mode);
if (previousFlightMode != flightMode()) {
emit flightModeChanged(flightMode());
}
// Assume armed since we don't know
if (_armed != true) {
_armed = true;
emit armedChanged(_armed);
}
_coordinate.setLatitude(highLatency2.latitude / (double)1E7);
_coordinate.setLongitude(highLatency2.longitude / (double)1E7);
_coordinate.setAltitude(highLatency2.altitude);
emit coordinateChanged(_coordinate);
_airSpeedFact.setRawValue((double)highLatency2.airspeed / 5.0);
_groundSpeedFact.setRawValue((double)highLatency2.groundspeed / 5.0);
_climbRateFact.setRawValue((double)highLatency2.climb_rate / 10.0);
_headingFact.setRawValue((double)highLatency2.heading * 2.0);
_altitudeRelativeFact.setRawValue(std::numeric_limits<double>::quiet_NaN());
_altitudeAMSLFact.setRawValue(highLatency2.altitude);
_windFactGroup.direction()->setRawValue((double)highLatency2.wind_heading * 2.0);
_windFactGroup.speed()->setRawValue((double)highLatency2.windspeed / 5.0);
_battery1FactGroup.percentRemaining()->setRawValue(highLatency2.battery);
_temperatureFactGroup.temperature1()->setRawValue(highLatency2.temperature_air);
_gpsFactGroup.lat()->setRawValue(highLatency2.latitude * 1e-7);
_gpsFactGroup.lon()->setRawValue(highLatency2.longitude * 1e-7);
_gpsFactGroup.count()->setRawValue(0);
_gpsFactGroup.hdop()->setRawValue(highLatency2.eph == UINT8_MAX ? std::numeric_limits<double>::quiet_NaN() : highLatency2.eph / 10.0);
_gpsFactGroup.vdop()->setRawValue(highLatency2.epv == UINT8_MAX ? std::numeric_limits<double>::quiet_NaN() : highLatency2.epv / 10.0);
MAV_SYS_STATUS_SENSOR sensorBit;
};
static const failure2Sensor_s rgFailure2Sensor[] = {
{ HL_FAILURE_FLAG_GPS, MAV_SYS_STATUS_SENSOR_GPS },
{ HL_FAILURE_FLAG_DIFFERENTIAL_PRESSURE, MAV_SYS_STATUS_SENSOR_DIFFERENTIAL_PRESSURE },
{ HL_FAILURE_FLAG_ABSOLUTE_PRESSURE, MAV_SYS_STATUS_SENSOR_ABSOLUTE_PRESSURE },
{ HL_FAILURE_FLAG_3D_ACCEL, MAV_SYS_STATUS_SENSOR_3D_ACCEL },
{ HL_FAILURE_FLAG_3D_GYRO, MAV_SYS_STATUS_SENSOR_3D_GYRO },
{ HL_FAILURE_FLAG_3D_MAG, MAV_SYS_STATUS_SENSOR_3D_MAG },
};
// Map from MAV_FAILURE bits to standard SYS_STATUS message handling
uint32_t newOnboardControlSensorsEnabled = 0;
for (size_t i=0; i<sizeof(rgFailure2Sensor)/sizeof(failure2Sensor_s); i++) {
const failure2Sensor_s* pFailure2Sensor = &rgFailure2Sensor[i];
if (highLatency2.failure_flags & pFailure2Sensor->failureBit) {
// Assume if reporting as unhealthy that is it present and enabled
newOnboardControlSensorsEnabled |= pFailure2Sensor->sensorBit;
}
}
if (newOnboardControlSensorsEnabled != _onboardControlSensorsEnabled) {
_onboardControlSensorsEnabled = newOnboardControlSensorsEnabled;
_onboardControlSensorsPresent = newOnboardControlSensorsEnabled;
_onboardControlSensorsUnhealthy = 0;
emit unhealthySensorsChanged();
}
void Vehicle::_handleAltitude(mavlink_message_t& message)
{
mavlink_altitude_t altitude;
mavlink_msg_altitude_decode(&message, &altitude);
// If data from GPS is available it takes precedence over ALTITUDE message
if (!_globalPositionIntMessageAvailable) {
_altitudeRelativeFact.setRawValue(altitude.altitude_relative);
if (!_gpsRawIntMessageAvailable) {
_altitudeAMSLFact.setRawValue(altitude.altitude_amsl);
}
}
void Vehicle::_setCapabilities(uint64_t capabilityBits)
{
_capabilityBits = capabilityBits;
emit capabilitiesKnownChanged(true);
emit capabilityBitsChanged(_capabilityBits);
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// This should potentially be turned into a user-facing warning
// if the general experience after deployment is that users want MAVLink 2
// but forget to upgrade their radio firmware
if (capabilityBits & MAV_PROTOCOL_CAPABILITY_MAVLINK2 && maxProtoVersion() < 200) {
qCDebug(VehicleLog) << QString("Vehicle does support MAVLink 2 but the link does not allow for it.");
}
QString supports("supports");
QString doesNotSupport("does not support");
qCDebug(VehicleLog) << QString("Vehicle %1 Mavlink 2.0").arg(_capabilityBits & MAV_PROTOCOL_CAPABILITY_MAVLINK2 ? supports : doesNotSupport);
qCDebug(VehicleLog) << QString("Vehicle %1 MISSION_ITEM_INT").arg(_capabilityBits & MAV_PROTOCOL_CAPABILITY_MISSION_INT ? supports : doesNotSupport);
qCDebug(VehicleLog) << QString("Vehicle %1 MISSION_COMMAND_INT").arg(_capabilityBits & MAV_PROTOCOL_CAPABILITY_COMMAND_INT ? supports : doesNotSupport);
qCDebug(VehicleLog) << QString("Vehicle %1 GeoFence").arg(_capabilityBits & MAV_PROTOCOL_CAPABILITY_MISSION_FENCE ? supports : doesNotSupport);
qCDebug(VehicleLog) << QString("Vehicle %1 RallyPoints").arg(_capabilityBits & MAV_PROTOCOL_CAPABILITY_MISSION_RALLY ? supports : doesNotSupport);
void Vehicle::_handleAutopilotVersion(LinkInterface *link, mavlink_message_t& message)
mavlink_autopilot_version_t autopilotVersion;
mavlink_msg_autopilot_version_decode(&message, &autopilotVersion);
_uid = (quint64)autopilotVersion.uid;
emit vehicleUIDChanged();
if (autopilotVersion.flight_sw_version != 0) {
int majorVersion, minorVersion, patchVersion;
FIRMWARE_VERSION_TYPE versionType;
majorVersion = (autopilotVersion.flight_sw_version >> (8*3)) & 0xFF;
minorVersion = (autopilotVersion.flight_sw_version >> (8*2)) & 0xFF;
patchVersion = (autopilotVersion.flight_sw_version >> (8*1)) & 0xFF;
versionType = (FIRMWARE_VERSION_TYPE)((autopilotVersion.flight_sw_version >> (8*0)) & 0xFF);
setFirmwareVersion(majorVersion, minorVersion, patchVersion, versionType);
if (px4Firmware()) {
// Lower 3 bytes is custom version
int majorVersion, minorVersion, patchVersion;
majorVersion = autopilotVersion.flight_custom_version[2];
minorVersion = autopilotVersion.flight_custom_version[1];
patchVersion = autopilotVersion.flight_custom_version[0];
setFirmwareCustomVersion(majorVersion, minorVersion, patchVersion);
// PX4 Firmware stores the first 16 characters of the git hash as binary, with the individual bytes in reverse order
_gitHash = "";
QByteArray array((char*)autopilotVersion.flight_custom_version, 8);
for (int i = 7; i >= 0; i--) {
_gitHash.append(QString("%1").arg(autopilotVersion.flight_custom_version[i], 2, 16, QChar('0')));
} else {
// APM Firmware stores the first 8 characters of the git hash as an ASCII character string
_gitHash = QString::fromUtf8((char*)autopilotVersion.flight_custom_version, 8);
if (_toolbox->corePlugin()->options()->checkFirmwareVersion()) {
_firmwarePlugin->checkIfIsLatestStable(this);
}
_setCapabilities(autopilotVersion.capabilities);
_startPlanRequest();
void Vehicle::_handleProtocolVersion(LinkInterface *link, mavlink_message_t& message)
{
Q_UNUSED(link);
mavlink_protocol_version_t protoVersion;
mavlink_msg_protocol_version_decode(&message, &protoVersion);
_setMaxProtoVersion(protoVersion.max_version);
}
void Vehicle::_setMaxProtoVersion(unsigned version) {
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// Set only once or if we need to reduce the max version
if (_maxProtoVersion == 0 || version < _maxProtoVersion) {
qCDebug(VehicleLog) << "_setMaxProtoVersion before:after" << _maxProtoVersion << version;
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_maxProtoVersion = version;
emit requestProtocolVersion(_maxProtoVersion);
// Now that the protocol version is known, the mission load is safe
// as it will use the right MAVLink version to enable all features
// the vehicle supports
_startPlanRequest();
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}
QString Vehicle::vehicleUIDStr()
{
QString uid;
uint8_t* pUid = (uint8_t*)(void*)&_uid;
uid.sprintf("%02X:%02X:%02X:%02X:%02X:%02X:%02X:%02X",
pUid[0] & 0xff,
pUid[1] & 0xff,
pUid[2] & 0xff,
pUid[3] & 0xff,
pUid[4] & 0xff,
pUid[5] & 0xff,
pUid[6] & 0xff,
pUid[7] & 0xff);
void Vehicle::_handleHilActuatorControls(mavlink_message_t &message)
{
mavlink_hil_actuator_controls_t hil;
mavlink_msg_hil_actuator_controls_decode(&message, &hil);
emit hilActuatorControlsChanged(hil.time_usec, hil.flags,
hil.controls[0],
hil.controls[1],
hil.controls[2],
hil.controls[3],
hil.controls[4],
hil.controls[5],
hil.controls[6],
hil.controls[7],
hil.controls[8],
hil.controls[9],
hil.controls[10],
hil.controls[11],
hil.controls[12],
hil.controls[13],
hil.controls[14],
hil.controls[15],
hil.mode);
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void Vehicle::_handleCommandLong(mavlink_message_t& message)
{
#ifdef NO_SERIAL_LINK
// If not using serial link, bail out.
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mavlink_command_long_t cmd;
mavlink_msg_command_long_decode(&message, &cmd);
switch (cmd.command) {
// Other component on the same system
// requests that QGC frees up the serial port of the autopilot
case MAV_CMD_PREFLIGHT_REBOOT_SHUTDOWN:
if (cmd.param6 > 0) {
// disconnect the USB link if its a direct connection to a Pixhawk
for (int i = 0; i < _links.length(); i++) {
SerialLink *sl = qobject_cast<SerialLink*>(_links.at(i));
if (sl && sl->getSerialConfig()->usbDirect()) {
qDebug() << "Disconnecting:" << _links.at(i)->getName();
qgcApp()->toolbox()->linkManager()->disconnectLink(_links.at(i));
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}
}
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break;
}
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}
void Vehicle::_handleExtendedSysState(mavlink_message_t& message)
{
mavlink_extended_sys_state_t extendedState;
mavlink_msg_extended_sys_state_decode(&message, &extendedState);
switch (extendedState.landed_state) {
case MAV_LANDED_STATE_ON_GROUND:
_setFlying(false);
_setLanding(false);
case MAV_LANDED_STATE_TAKEOFF:
_setFlying(true);
_setLanding(false);
break;
case MAV_LANDED_STATE_LANDING:
_setFlying(true);
_setLanding(true);
break;
default:
break;
bool vtolInFwdFlight = extendedState.vtol_state == MAV_VTOL_STATE_FW;
if (vtolInFwdFlight != _vtolInFwdFlight) {
_vtolInFwdFlight = vtolInFwdFlight;
emit vtolInFwdFlightChanged(vtolInFwdFlight);
}
void Vehicle::_handleVibration(mavlink_message_t& message)
{
mavlink_vibration_t vibration;
mavlink_msg_vibration_decode(&message, &vibration);
_vibrationFactGroup.xAxis()->setRawValue(vibration.vibration_x);
_vibrationFactGroup.yAxis()->setRawValue(vibration.vibration_y);
_vibrationFactGroup.zAxis()->setRawValue(vibration.vibration_z);
_vibrationFactGroup.clipCount1()->setRawValue(vibration.clipping_0);
_vibrationFactGroup.clipCount2()->setRawValue(vibration.clipping_1);
_vibrationFactGroup.clipCount3()->setRawValue(vibration.clipping_2);
}
void Vehicle::_handleWindCov(mavlink_message_t& message)
{
mavlink_wind_cov_t wind;
mavlink_msg_wind_cov_decode(&message, &wind);
float direction = qRadiansToDegrees(qAtan2(wind.wind_y, wind.wind_x));
float speed = qSqrt(qPow(wind.wind_x, 2) + qPow(wind.wind_y, 2));
_windFactGroup.direction()->setRawValue(direction);
_windFactGroup.speed()->setRawValue(speed);
_windFactGroup.verticalSpeed()->setRawValue(0);
}
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#if !defined(NO_ARDUPILOT_DIALECT)
void Vehicle::_handleWind(mavlink_message_t& message)
{
mavlink_wind_t wind;
mavlink_msg_wind_decode(&message, &wind);
// We don't want negative wind angles
float direction = wind.direction;
if (direction < 0) {
direction += 360;
}
_windFactGroup.direction()->setRawValue(direction);
_windFactGroup.speed()->setRawValue(wind.speed);
_windFactGroup.verticalSpeed()->setRawValue(wind.speed_z);
}
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#endif
bool Vehicle::_apmArmingNotRequired(void)
{
QString armingRequireParam("ARMING_REQUIRE");
return _parameterManager->parameterExists(FactSystem::defaultComponentId, armingRequireParam) &&
_parameterManager->getParameter(FactSystem::defaultComponentId, armingRequireParam)->rawValue().toInt() == 0;
}
void Vehicle::_handleSysStatus(mavlink_message_t& message)
{
mavlink_sys_status_t sysStatus;
mavlink_msg_sys_status_decode(&message, &sysStatus);
if (sysStatus.current_battery == -1) {
_battery1FactGroup.current()->setRawValue(VehicleBatteryFactGroup::_currentUnavailable);
// Current is in Amps, current_battery is 10 * milliamperes (1 = 10 milliampere)
_battery1FactGroup.current()->setRawValue((float)sysStatus.current_battery / 100.0f);
}
if (sysStatus.voltage_battery == UINT16_MAX) {
_battery1FactGroup.voltage()->setRawValue(VehicleBatteryFactGroup::_voltageUnavailable);
_battery1FactGroup.voltage()->setRawValue((double)sysStatus.voltage_battery / 1000.0);
// current_battery is 10 mA and voltage_battery is 1mV. (10/1e3 times 1/1e3 = 1/1e5)
_battery1FactGroup.instantPower()->setRawValue((float)(sysStatus.current_battery*sysStatus.voltage_battery)/(100000.0));
_battery1FactGroup.percentRemaining()->setRawValue(sysStatus.battery_remaining);
if (sysStatus.battery_remaining > 0) {
if (sysStatus.battery_remaining < _settingsManager->appSettings()->batteryPercentRemainingAnnounce()->rawValue().toInt() &&
sysStatus.battery_remaining < _lastAnnouncedLowBatteryPercent) {
_say(QString(tr("%1 low battery: %2 percent remaining")).arg(_vehicleIdSpeech()).arg(sysStatus.battery_remaining));
_lastAnnouncedLowBatteryPercent = sysStatus.battery_remaining;
if (_onboardControlSensorsPresent != sysStatus.onboard_control_sensors_present) {
_onboardControlSensorsPresent = sysStatus.onboard_control_sensors_present;
emit sensorsPresentBitsChanged(_onboardControlSensorsPresent);
}
if (_onboardControlSensorsEnabled != sysStatus.onboard_control_sensors_enabled) {
_onboardControlSensorsEnabled = sysStatus.onboard_control_sensors_enabled;
emit sensorsEnabledBitsChanged(_onboardControlSensorsEnabled);
}
if (_onboardControlSensorsHealth != sysStatus.onboard_control_sensors_health) {
_onboardControlSensorsHealth = sysStatus.onboard_control_sensors_health;
emit sensorsHealthBitsChanged(_onboardControlSensorsHealth);
}
// ArduPilot firmare has a strange case when ARMING_REQUIRE=0. This means the vehicle is always armed but the motors are not
// really powered up until the safety button is pressed. Because of this we can't depend on the heartbeat to tell us the true
// armed (and dangerous) state. We must instead rely on SYS_STATUS telling us that the motors are enabled.
if (apmFirmware() && _apmArmingNotRequired()) {
_updateArmed(_onboardControlSensorsEnabled & MAV_SYS_STATUS_SENSOR_MOTOR_OUTPUTS);
}
uint32_t newSensorsUnhealthy = _onboardControlSensorsEnabled & ~_onboardControlSensorsHealth;
if (newSensorsUnhealthy != _onboardControlSensorsUnhealthy) {
_onboardControlSensorsUnhealthy = newSensorsUnhealthy;
emit unhealthySensorsChanged();
emit sensorsUnhealthyBitsChanged(_onboardControlSensorsUnhealthy);
}
void Vehicle::_handleBatteryStatus(mavlink_message_t& message)
{
mavlink_battery_status_t bat_status;
mavlink_msg_battery_status_decode(&message, &bat_status);
VehicleBatteryFactGroup& batteryFactGroup = bat_status.id == 0 ? _battery1FactGroup : _battery2FactGroup;
batteryFactGroup.temperature()->setRawValue(VehicleBatteryFactGroup::_temperatureUnavailable);
batteryFactGroup.temperature()->setRawValue((double)bat_status.temperature / 100.0);
batteryFactGroup.mahConsumed()->setRawValue(VehicleBatteryFactGroup::_mahConsumedUnavailable);
batteryFactGroup.mahConsumed()->setRawValue(bat_status.current_consumed);
}
int cellCount = 0;
for (int i=0; i<10; i++) {
if (bat_status.voltages[i] != UINT16_MAX) {
cellCount++;
}
}
if (cellCount == 0) {
cellCount = -1;
}
batteryFactGroup.cellCount()->setRawValue(cellCount);
//-- Time remaining in seconds (0 means not supported)
batteryFactGroup.timeRemaining()->setRawValue(bat_status.time_remaining);
//-- Battery charge state (0 means not supported)
if(bat_status.charge_state <= MAV_BATTERY_CHARGE_STATE_UNHEALTHY) {
batteryFactGroup.chargeState()->setRawValue(bat_status.charge_state);
}
//-- TODO: Somewhere, actions would be taken based on this chargeState:
// MAV_BATTERY_CHARGE_STATE_CRITICAL: Battery state is critical, return / abort immediately
// MAV_BATTERY_CHARGE_STATE_EMERGENCY: Battery state is too low for ordinary abortion, fastest possible emergency stop preventing damage
// MAV_BATTERY_CHARGE_STATE_FAILED: Battery failed, damage unavoidable
// MAV_BATTERY_CHARGE_STATE_UNHEALTHY: Battery is diagnosed to be broken or an error occurred, usage is discouraged / prohibited
void Vehicle::_setHomePosition(QGeoCoordinate& homeCoord)
{
if (homeCoord != _homePosition) {
_homePosition = homeCoord;
emit homePositionChanged(_homePosition);
}
}
void Vehicle::_handleHomePosition(mavlink_message_t& message)
{
mavlink_home_position_t homePos;
mavlink_msg_home_position_decode(&message, &homePos);
QGeoCoordinate newHomePosition (homePos.latitude / 10000000.0,
homePos.longitude / 10000000.0,
homePos.altitude / 1000.0);
// We are transitioning to the armed state, begin tracking trajectory points for the map
if (_armed) {
_mapTrajectoryStart();
_clearCameraTriggerPoints();
// Also handle Video Streaming
if(qgcApp()->toolbox()->videoManager()->videoReceiver()) {
if(_settingsManager->videoSettings()->disableWhenDisarmed()->rawValue().toBool()) {
_settingsManager->videoSettings()->streamEnabled()->setRawValue(false);
qgcApp()->toolbox()->videoManager()->videoReceiver()->stop();
}
void Vehicle::_handlePing(LinkInterface* link, mavlink_message_t& message)
{
mavlink_ping_t ping;
mavlink_message_t msg;
mavlink_msg_ping_decode(&message, &ping);
mavlink_msg_ping_pack_chan(static_cast<uint8_t>(_mavlink->getSystemId()),
static_cast<uint8_t>(_mavlink->getComponentId()),
priorityLink()->mavlinkChannel(),
&msg,
ping.time_usec,
ping.seq,
message.sysid,
message.compid);
sendMessageOnLink(link, msg);
}
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void Vehicle::_handleHeartbeat(mavlink_message_t& message)
{
if (message.compid != _defaultComponentId) {
return;
}
mavlink_heartbeat_t heartbeat;
mavlink_msg_heartbeat_decode(&message, &heartbeat);
bool newArmed = heartbeat.base_mode & MAV_MODE_FLAG_DECODE_POSITION_SAFETY;
// ArduPilot firmare has a strange case when ARMING_REQUIRE=0. This means the vehicle is always armed but the motors are not
// really powered up until the safety button is pressed. Because of this we can't depend on the heartbeat to tell us the true
// armed (and dangerous) state. We must instead rely on SYS_STATUS telling us that the motors are enabled.
if (apmFirmware()) {
if (!_apmArmingNotRequired() || !(_onboardControlSensorsPresent & MAV_SYS_STATUS_SENSOR_MOTOR_OUTPUTS)) {
// If ARMING_REQUIRE!=0 or we haven't seen motor output status yet we use the hearbeat info for armed
_updateArmed(newArmed);
}
} else {
// Non-ArduPilot always updates from armed state in heartbeat
_updateArmed(newArmed);
}
if (heartbeat.base_mode != _base_mode || heartbeat.custom_mode != _custom_mode) {
QString previousFlightMode;
if (_base_mode != 0 || _custom_mode != 0){
// Vehicle is initialized with _base_mode=0 and _custom_mode=0. Don't pass this to flightMode() since it will complain about
// bad modes while unit testing.
previousFlightMode = flightMode();
}
_base_mode = heartbeat.base_mode;
_custom_mode = heartbeat.custom_mode;
if (previousFlightMode != flightMode()) {
emit flightModeChanged(flightMode());
}
void Vehicle::_handleRadioStatus(mavlink_message_t& message)
{
Lorenz Meier
committed
//-- Process telemetry status message
mavlink_radio_status_t rstatus;
mavlink_msg_radio_status_decode(&message, &rstatus);
Lorenz Meier
committed
int rssi = rstatus.rssi;
int remrssi = rstatus.remrssi;
int lnoise = (int)(int8_t)rstatus.noise;
int rnoise = (int)(int8_t)rstatus.remnoise;
//-- 3DR Si1k radio needs rssi fields to be converted to dBm
if (message.sysid == '3' && message.compid == 'D') {
/* Per the Si1K datasheet figure 23.25 and SI AN474 code
* samples the relationship between the RSSI register
* and received power is as follows:
*
* 10
* inputPower = rssi * ------ 127
* 19
*
* Additionally limit to the only realistic range [-120,0] dBm
*/
rssi = qMin(qMax(qRound(static_cast<qreal>(rssi) / 1.9 - 127.0), - 120), 0);
remrssi = qMin(qMax(qRound(static_cast<qreal>(remrssi) / 1.9 - 127.0), - 120), 0);
} else {
rssi = (int)(int8_t)rstatus.rssi;
remrssi = (int)(int8_t)rstatus.remrssi;
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}
//-- Check for changes
if(_telemetryLRSSI != rssi) {
_telemetryLRSSI = rssi;
emit telemetryLRSSIChanged(_telemetryLRSSI);
}
if(_telemetryRRSSI != remrssi) {
_telemetryRRSSI = remrssi;
emit telemetryRRSSIChanged(_telemetryRRSSI);
}
if(_telemetryRXErrors != rstatus.rxerrors) {
_telemetryRXErrors = rstatus.rxerrors;
emit telemetryRXErrorsChanged(_telemetryRXErrors);
}
if(_telemetryFixed != rstatus.fixed) {
_telemetryFixed = rstatus.fixed;
emit telemetryFixedChanged(_telemetryFixed);
}
if(_telemetryTXBuffer != rstatus.txbuf) {
_telemetryTXBuffer = rstatus.txbuf;
emit telemetryTXBufferChanged(_telemetryTXBuffer);
}
if(_telemetryLNoise != lnoise) {
_telemetryLNoise = lnoise;
emit telemetryLNoiseChanged(_telemetryLNoise);
}
if(_telemetryRNoise != rnoise) {
_telemetryRNoise = rnoise;
emit telemetryRNoiseChanged(_telemetryRNoise);
}
}
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void Vehicle::_handleRCChannels(mavlink_message_t& message)
{
mavlink_rc_channels_t channels;
mavlink_msg_rc_channels_decode(&message, &channels);
uint16_t* _rgChannelvalues[cMaxRcChannels] = {
&channels.chan1_raw,
&channels.chan2_raw,
&channels.chan3_raw,
&channels.chan4_raw,
&channels.chan5_raw,
&channels.chan6_raw,
&channels.chan7_raw,
&channels.chan8_raw,
&channels.chan9_raw,
&channels.chan10_raw,
&channels.chan11_raw,
&channels.chan12_raw,
&channels.chan13_raw,
&channels.chan14_raw,
&channels.chan15_raw,
&channels.chan16_raw,
&channels.chan17_raw,
&channels.chan18_raw,
};
int pwmValues[cMaxRcChannels];
for (int i=0; i<cMaxRcChannels; i++) {
uint16_t channelValue = *_rgChannelvalues[i];
if (i < channels.chancount) {
pwmValues[i] = channelValue == UINT16_MAX ? -1 : channelValue;
} else {
pwmValues[i] = -1;
}
}
emit remoteControlRSSIChanged(channels.rssi);
emit rcChannelsChanged(channels.chancount, pwmValues);
}
void Vehicle::_handleRCChannelsRaw(mavlink_message_t& message)
{
// We handle both RC_CHANNLES and RC_CHANNELS_RAW since different firmware will only
// send one or the other.
mavlink_rc_channels_raw_t channels;
mavlink_msg_rc_channels_raw_decode(&message, &channels);
uint16_t* _rgChannelvalues[cMaxRcChannels] = {
&channels.chan1_raw,
&channels.chan2_raw,
&channels.chan3_raw,
&channels.chan4_raw,
&channels.chan5_raw,
&channels.chan6_raw,
&channels.chan7_raw,
&channels.chan8_raw,
};
int pwmValues[cMaxRcChannels];
int channelCount = 0;
for (int i=0; i<cMaxRcChannels; i++) {
pwmValues[i] = -1;
}
for (int i=0; i<8; i++) {
uint16_t channelValue = *_rgChannelvalues[i];
if (channelValue == UINT16_MAX) {
pwmValues[i] = -1;
} else {
pwmValues[i] = channelValue;
}
}
for (int i=9; i<18; i++) {
pwmValues[i] = -1;
}
emit remoteControlRSSIChanged(channels.rssi);
emit rcChannelsChanged(channelCount, pwmValues);
}
void Vehicle::_handleScaledPressure(mavlink_message_t& message) {
mavlink_scaled_pressure_t pressure;
mavlink_msg_scaled_pressure_decode(&message, &pressure);
_temperatureFactGroup.temperature1()->setRawValue(pressure.temperature / 100.0);
}
void Vehicle::_handleScaledPressure2(mavlink_message_t& message) {
mavlink_scaled_pressure2_t pressure;
mavlink_msg_scaled_pressure2_decode(&message, &pressure);
_temperatureFactGroup.temperature2()->setRawValue(pressure.temperature / 100.0);
}
void Vehicle::_handleScaledPressure3(mavlink_message_t& message) {
mavlink_scaled_pressure3_t pressure;
mavlink_msg_scaled_pressure3_decode(&message, &pressure);
_temperatureFactGroup.temperature3()->setRawValue(pressure.temperature / 100.0);
}
bool Vehicle::_containsLink(LinkInterface* link)
{
}
void Vehicle::_addLink(LinkInterface* link)
{
if (!_containsLink(link)) {
qCDebug(VehicleLog) << "_addLink:" << QString("%1").arg((ulong)link, 0, 16);
if (_links.count() <= 1) {
_updatePriorityLink(true /* updateActive */, false /* sendCommand */);
_updatePriorityLink(true /* updateActive */, true /* sendCommand */);
connect(_toolbox->linkManager(), &LinkManager::linkInactive, this, &Vehicle::_linkInactiveOrDeleted);
connect(_toolbox->linkManager(), &LinkManager::linkDeleted, this, &Vehicle::_linkInactiveOrDeleted);
connect(link, &LinkInterface::highLatencyChanged, this, &Vehicle::_updateHighLatencyLink);
connect(link, &LinkInterface::activeChanged, this, &Vehicle::_linkActiveChanged);
void Vehicle::_linkInactiveOrDeleted(LinkInterface* link)
qCDebug(VehicleLog) << "_linkInactiveOrDeleted linkCount" << _links.count();
_updatePriorityLink(true /* updateActive */, true /* sendCommand */);
// Make sure to not send this more than one time
_allLinksInactiveSent = true;
emit allLinksInactive(this);
bool Vehicle::sendMessageOnLink(LinkInterface* link, mavlink_message_t message)
{
if (!link || !_links.contains(link) || !link->isConnected()) {
return false;
}
emit _sendMessageOnLinkOnThread(link, message);
return true;
}
void Vehicle::_sendMessageOnLink(LinkInterface* link, mavlink_message_t message)
{
// Make sure this is still a good link
if (!link || !_links.contains(link) || !link->isConnected()) {
return;
}
#if 0
// Leaving in for ease in Mav 2.0 testing
mavlink_status_t* mavlinkStatus = mavlink_get_channel_status(link->mavlinkChannel());
qDebug() << "_sendMessageOnLink" << mavlinkStatus << link->mavlinkChannel() << mavlinkStatus->flags << message.magic;
#endif
// Give the plugin a chance to adjust
_firmwarePlugin->adjustOutgoingMavlinkMessage(this, link, &message);
// Write message into buffer, prepending start sign
uint8_t buffer[MAVLINK_MAX_PACKET_LEN];
int len = mavlink_msg_to_send_buffer(buffer, &message);
link->writeBytesSafe((const char*)buffer, len);
_messagesSent++;
emit messagesSentChanged();
void Vehicle::_updatePriorityLink(bool updateActive, bool sendCommand)
// if the priority link is commanded and still active don't change anything
if (_priorityLinkCommanded) {
if (_priorityLink.data()->link_active(_id)) {
return;
} else {
_priorityLinkCommanded = false;
}
}
LinkInterface* newPriorityLink = nullptr;
// This routine specifically does not clear _priorityLink when there are no links remaining.
// By doing this we hold a reference on the last link as the Vehicle shuts down. Thus preventing shutdown
// ordering nullptr pointer crashes where priorityLink() is still called during shutdown sequence.
if (_links.count() == 0) {
return;
}
// Check for the existing priority link to still be valid
for (int i=0; i<_links.count(); i++) {
if (_priorityLink.data() == _links[i]) {
if (!_priorityLink.data()->highLatency() && _priorityLink->link_active(_id)) {
// Link is still valid. Continue to use it unless it is high latency. In that case we still look for a better
// link to use as priority link.
return;
}
}
}
// The previous priority link is no longer valid. We must no find the best link available in this priority order:
// First active direct USB connection
// Any active non high latency link
// An active high latency link
// Any link
#ifndef NO_SERIAL_LINK
// Search for an active direct usb connection
for (int i=0; i<_links.count(); i++) {
LinkInterface* link = _links[i];
SerialLink* pSerialLink = qobject_cast<SerialLink*>(link);
if (pSerialLink) {
LinkConfiguration* config = pSerialLink->getLinkConfiguration();
if (config) {
SerialConfiguration* pSerialConfig = qobject_cast<SerialConfiguration*>(config);
if (pSerialConfig && pSerialConfig->usbDirect()) {
if (_priorityLink.data() != link && link->link_active(_id)) {