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}
else
{
// Attempt to set HIL mode
Thomas Gubler
committed
setMode(base_mode | MAV_MODE_FLAG_HIL_ENABLED, custom_mode);
qDebug() << __FILE__ << __LINE__ << "HIL is onboard not enabled, trying to enable.";
}
}
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committed
/*
* @param abs_pressure Absolute Pressure (hPa)
* @param diff_pressure Differential Pressure (hPa)
*/
void UAS::sendHilSensors(quint64 time_us, float xacc, float yacc, float zacc, float rollspeed, float pitchspeed, float yawspeed,
float xmag, float ymag, float zmag, float abs_pressure, float diff_pressure, float pressure_alt, float temperature, quint32 fields_changed)
if (this->base_mode & MAV_MODE_FLAG_HIL_ENABLED)
mavlink_msg_hil_sensor_pack(mavlink->getSystemId(), mavlink->getComponentId(), &msg,
time_us, xacc, yacc, zacc, rollspeed, pitchspeed, yawspeed,
xmag, ymag, zmag, abs_pressure, diff_pressure, pressure_alt, temperature,
fields_changed);
sendMessage(msg);
lastSendTimeSensors = QGC::groundTimeMilliseconds();
}
else
{
// Attempt to set HIL mode
Thomas Gubler
committed
setMode(base_mode | MAV_MODE_FLAG_HIL_ENABLED, custom_mode);
qDebug() << __FILE__ << __LINE__ << "HIL is onboard not enabled, trying to enable.";
}
}
void UAS::sendHilOpticalFlow(quint64 time_us, qint16 flow_x, qint16 flow_y, float flow_comp_m_x,
float flow_comp_m_y, quint8 quality, float ground_distance)
{
// FIXME: This needs to be updated for new mavlink_msg_hil_optical_flow_pack api
Q_UNUSED(time_us);
Q_UNUSED(flow_x);
Q_UNUSED(flow_y);
Q_UNUSED(flow_comp_m_x);
Q_UNUSED(flow_comp_m_y);
Q_UNUSED(quality);
Q_UNUSED(ground_distance);
if (this->base_mode & MAV_MODE_FLAG_HIL_ENABLED)
{
mavlink_message_t msg;
mavlink_msg_hil_optical_flow_pack(mavlink->getSystemId(), mavlink->getComponentId(), &msg,
time_us, 0, 0 /* hack */, flow_x, flow_y, 0.0f /* hack */, 0.0f /* hack */, 0.0f /* hack */, 0 /* hack */, quality, ground_distance);
sendMessage(msg);
lastSendTimeOpticalFlow = QGC::groundTimeMilliseconds();
}
else
{
// Attempt to set HIL mode
setMode(base_mode | MAV_MODE_FLAG_HIL_ENABLED, custom_mode);
qDebug() << __FILE__ << __LINE__ << "HIL is onboard not enabled, trying to enable.";
}
}
void UAS::sendHilGps(quint64 time_us, double lat, double lon, double alt, int fix_type, float eph, float epv, float vel, float vn, float ve, float vd, float cog, int satellites)
// Only send at 10 Hz max rate
if (QGC::groundTimeMilliseconds() - lastSendTimeGPS < 100)
return;
if (this->base_mode & MAV_MODE_FLAG_HIL_ENABLED)
float course = cog;
// map to 0..2pi
if (course < 0)
// scale from radians to degrees
course = (course / M_PI) * 180.0f;
mavlink_msg_hil_gps_pack(mavlink->getSystemId(), mavlink->getComponentId(), &msg,
time_us, fix_type, lat*1e7, lon*1e7, alt*1e3, eph*1e2, epv*1e2, vel*1e2, vn*1e2, ve*1e2, vd*1e2, course*1e2, satellites);
lastSendTimeGPS = QGC::groundTimeMilliseconds();
sendMessage(msg);
}
else
{
// Attempt to set HIL mode
Thomas Gubler
committed
setMode(base_mode | MAV_MODE_FLAG_HIL_ENABLED, custom_mode);
qDebug() << __FILE__ << __LINE__ << "HIL is onboard not enabled, trying to enable.";
}
}
/**
* Connect flight gear link.
**/
void UAS::startHil()
{
if (hilEnabled) return;
hilEnabled = true;
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committed
setMode(base_mode | MAV_MODE_FLAG_HIL_ENABLED, custom_mode);
Lorenz Meier
committed
qDebug() << __FILE__ << __LINE__ << "HIL is onboard not enabled, trying to enable.";
// Connect HIL simulation link
simulation->connectSimulation();
}
/**
* disable flight gear link.
*/
void UAS::stopHil()
{
Lorenz Meier
committed
if (simulation && simulation->isConnected()) {
simulation->disconnectSimulation();
setMode(base_mode & ~MAV_MODE_FLAG_HIL_ENABLED, custom_mode);
qDebug() << __FILE__ << __LINE__ << "HIL is onboard not enabled, trying to disable.";
}
hilEnabled = false;
}
void UAS::shutdown()
{
QMessageBox::StandardButton button = QGCMessageBox::question(tr("Shutting down the UAS"),
tr("Do you want to shut down the onboard computer?"),
QMessageBox::Yes | QMessageBox::Cancel,
QMessageBox::Cancel);
if (button == QMessageBox::Yes)
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{
// If the active UAS is set, execute command
mavlink_message_t msg;
mavlink_msg_command_long_pack(mavlink->getSystemId(), mavlink->getComponentId(), &msg, uasId, MAV_COMP_ID_ALL, MAV_CMD_PREFLIGHT_REBOOT_SHUTDOWN, 1, 0, 2, 0, 0, 0, 0, 0);
sendMessage(msg);
}
}
/**
* @param x position
* @param y position
* @param z position
* @param yaw
*/
void UAS::setTargetPosition(float x, float y, float z, float yaw)
{
mavlink_message_t msg;
mavlink_msg_command_long_pack(mavlink->getSystemId(), mavlink->getComponentId(), &msg, uasId, MAV_COMP_ID_ALL, MAV_CMD_NAV_PATHPLANNING, 1, 1, 1, 0, yaw, x, y, z);
sendMessage(msg);
}
/**
* @return The name of this system as string in human-readable form
*/
QString UAS::getUASName(void) const
{
QString result;
if (name == "")
{
result = tr("MAV ") + result.sprintf("%03d", getUASID());
}
else
{
result = name;
}
return result;
}
/**
* @return the state of the uas as a short text.
*/
const QString& UAS::getShortState() const
{
return shortStateText;
}
/**
* The mode can be autonomous, guided, manual or armed. It will also return if
* hardware in the loop is being used.
* @return the audio mode text for the id given.
*/
QString UAS::getAudioModeTextFor(int id)
{
QString mode;
uint8_t modeid = id;
// BASE MODE DECODING
if (modeid & (uint8_t)MAV_MODE_FLAG_DECODE_POSITION_AUTO)
{
mode += "autonomous";
}
else if (modeid & (uint8_t)MAV_MODE_FLAG_DECODE_POSITION_GUIDED)
{
mode += "guided";
}
else if (modeid & (uint8_t)MAV_MODE_FLAG_DECODE_POSITION_STABILIZE)
{
mode += "stabilized";
}
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else if (modeid & (uint8_t)MAV_MODE_FLAG_DECODE_POSITION_MANUAL)
{
mode += "manual";
}
else
{
// Nothing else applies, we're in preflight
mode += "preflight";
}
if (modeid != 0)
{
mode += " mode";
}
// ARMED STATE DECODING
if (modeid & (uint8_t)MAV_MODE_FLAG_DECODE_POSITION_SAFETY)
{
mode.append(" and armed");
}
// HARDWARE IN THE LOOP DECODING
if (modeid & (uint8_t)MAV_MODE_FLAG_DECODE_POSITION_HIL)
{
mode.append(" using hardware in the loop simulation");
}
return mode;
}
/**
* The mode returned can be auto, stabilized, test, manual, preflight or unknown.
* @return the short text of the mode for the id given.
*/
* The mode returned can be auto, stabilized, test, manual, preflight or unknown.
* @return the short text of the mode for the id given.
*/
QString UAS::getShortModeTextFor(uint8_t base_mode, uint32_t custom_mode) const
QString mode = AutoPilotPluginManager::instance()->getShortModeText(base_mode, custom_mode, autopilot);
{
mode = "|UNKNOWN";
qDebug() << __FILE__ << __LINE__ << " Unknown mode: base_mode=" << base_mode << " custom_mode=" << custom_mode << " autopilot=" << autopilot;
}
// ARMED STATE DECODING
if (base_mode & MAV_MODE_FLAG_DECODE_POSITION_SAFETY)
{
mode.prepend("A");
}
else
{
mode.prepend("D");
}
// HARDWARE IN THE LOOP DECODING
if (base_mode & MAV_MODE_FLAG_DECODE_POSITION_HIL)
{
mode.prepend("HIL:");
}
//qDebug() << "base_mode=" << base_mode << " custom_mode=" << custom_mode << " autopilot=" << autopilot << ": " << mode;
return mode;
}
const QString& UAS::getShortMode() const
{
return shortModeText;
}
/**
* Add the link and connect a signal to it which will be set off when it is destroyed.
*/
void UAS::addLink(LinkInterface* link)
{
if (!links.contains(link))
links.append(link);
qCDebug(UASLog) << "addLink:" << QString("%1").arg((ulong)link, 0, 16);
connect(link, SIGNAL(destroyed(QObject*)), this, SLOT(removeLink(QObject*)));
}
}
void UAS::removeLink(QObject* object)
{
qCDebug(UASLog) << "removeLink:" << QString("%1").arg((ulong)object, 0, 16);
qCDebug(UASLog) << "link count:" << links.count();
// Do not dynamic cast or de-reference QObject, since object is either in destructor or may have already
// been destroyed.
int index = links.indexOf(link);
}
/**
* @return the list of links
*/
QList<LinkInterface*> UAS::getLinks()
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{
return links;
}
/**
* @rerturn the map of the components
*/
QMap<int, QString> UAS::getComponents()
{
return components;
}
/**
* Set the battery type and the number of cells.
* @param type of the battery
* @param cells Number of cells.
*/
void UAS::setBattery(BatteryType type, int cells)
{
this->batteryType = type;
this->cells = cells;
switch (batteryType)
{
case NICD:
break;
case NIMH:
break;
case LIION:
break;
case LIPOLY:
fullVoltage = this->cells * lipoFull;
emptyVoltage = this->cells * lipoEmpty;
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break;
case LIFE:
break;
case AGZN:
break;
}
}
/**
* Set the battery specificaitons: empty voltage, warning voltage, and full voltage.
* @param specifications of the battery
*/
void UAS::setBatterySpecs(const QString& specs)
{
if (specs.length() == 0 || specs.contains("%"))
{
batteryRemainingEstimateEnabled = false;
bool ok;
QString percent = specs;
percent = percent.remove("%");
float temp = percent.toFloat(&ok);
if (ok)
{
warnLevelPercent = temp;
}
else
{
emit textMessageReceived(0, 0, MAV_SEVERITY_WARNING, "Could not set battery options, format is wrong");
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}
}
else
{
batteryRemainingEstimateEnabled = true;
QString stringList = specs;
stringList = stringList.remove("V");
stringList = stringList.remove("v");
QStringList parts = stringList.split(",");
if (parts.length() == 3)
{
float temp;
bool ok;
// Get the empty voltage
temp = parts.at(0).toFloat(&ok);
if (ok) emptyVoltage = temp;
// Get the warning voltage
temp = parts.at(1).toFloat(&ok);
if (ok) warnVoltage = temp;
// Get the full voltage
temp = parts.at(2).toFloat(&ok);
if (ok) fullVoltage = temp;
}
else
{
emit textMessageReceived(0, 0, MAV_SEVERITY_WARNING, "Could not set battery options, format is wrong");
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}
}
}
/**
* @return the battery specifications(empty voltage, warning voltage, full voltage)
*/
QString UAS::getBatterySpecs()
{
if (batteryRemainingEstimateEnabled)
{
return QString("%1V,%2V,%3V").arg(emptyVoltage).arg(warnVoltage).arg(fullVoltage);
}
else
{
return QString("%1%").arg(warnLevelPercent);
}
}
/**
* @return the time remaining.
*/
int UAS::calculateTimeRemaining()
{
quint64 dt = QGC::groundTimeMilliseconds() - startTime;
double seconds = dt / 1000.0f;
double voltDifference = startVoltage - currentVoltage;
if (voltDifference <= 0) voltDifference = 0.00000000001f;
double dischargePerSecond = voltDifference / seconds;
int remaining = static_cast<int>((currentVoltage - emptyVoltage) / dischargePerSecond);
// Can never be below 0
if (remaining < 0) remaining = 0;
return remaining;
}
/**
* @return charge level in percent - 0 - 100
*/
float UAS::getChargeLevel()
{
if (batteryRemainingEstimateEnabled)
{
if (lpVoltage < emptyVoltage)
{
chargeLevel = 0.0f;
}
else if (lpVoltage > fullVoltage)
{
chargeLevel = 100.0f;
}
else
{
chargeLevel = 100.0f * ((lpVoltage - emptyVoltage)/(fullVoltage - emptyVoltage));
}
}
return chargeLevel;
}
void UAS::startLowBattAlarm()
{
if (!lowBattAlarm)
{
GAudioOutput::instance()->alert(tr("system %1 has low battery").arg(getUASName()));
QTimer::singleShot(3000, GAudioOutput::instance(), SLOT(startEmergency()));
lowBattAlarm = true;
}
}
void UAS::stopLowBattAlarm()
{
if (lowBattAlarm)
{
GAudioOutput::instance()->stopEmergency();
lowBattAlarm = false;
}
}