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#ifndef __mobile__
float UAS::addZeroMeanNoise(float truth_meas, float noise_var)
{
/* Calculate normally distributed variable noise with mean = 0 and variance = noise_var. Calculated according to
Box-Muller transform */
static const float epsilon = std::numeric_limits<float>::min(); //used to ensure non-zero uniform numbers
static const float two_pi = 2.0*3.14159265358979323846; // 2*pi
static float z0; //calculated normal distribution random variables with mu = 0, var = 1;
float u1, u2; //random variables generated from c++ rand();
/*Generate random variables in range (0 1] */
do
{
//TODO seed rand() with srand(time) but srand(time should be called once on startup)
//currently this will generate repeatable random noise
u1 = rand() * (1.0 / RAND_MAX);
u2 = rand() * (1.0 / RAND_MAX);
}
while ( u1 <= epsilon ); //Have a catch to ensure non-zero for log()
z0 = sqrt(-2.0 * log(u1)) * cos(two_pi * u2); //calculate normally distributed variable with mu = 0, var = 1
//TODO add bias term that changes randomly to simulate accelerometer and gyro bias the exf should handle these
//as well
float noise = z0 * (noise_var*noise_var); //calculate normally distributed variable with mu = 0, std = var^2
//Finally gaurd against any case where the noise is not real
if(std::isfinite(noise)){
return truth_meas + noise;
}
else{
return truth_meas;
}
}
#endif
Thomas Gubler
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)
float xacc_corrupt = addZeroMeanNoise(xacc, xacc_var);
float yacc_corrupt = addZeroMeanNoise(yacc, yacc_var);
float zacc_corrupt = addZeroMeanNoise(zacc, zacc_var);
float rollspeed_corrupt = addZeroMeanNoise(rollspeed,rollspeed_var);
float pitchspeed_corrupt = addZeroMeanNoise(pitchspeed,pitchspeed_var);
float yawspeed_corrupt = addZeroMeanNoise(yawspeed,yawspeed_var);
float xmag_corrupt = addZeroMeanNoise(xmag, xmag_var);
float ymag_corrupt = addZeroMeanNoise(ymag, ymag_var);
float zmag_corrupt = addZeroMeanNoise(zmag, zmag_var);
float abs_pressure_corrupt = addZeroMeanNoise(abs_pressure,abs_pressure_var);
float diff_pressure_corrupt = addZeroMeanNoise(diff_pressure, diff_pressure_var);
float pressure_alt_corrupt = addZeroMeanNoise(pressure_alt, pressure_alt_var);
float temperature_corrupt = addZeroMeanNoise(temperature,temperature_var);
mavlink_msg_hil_sensor_pack(mavlink->getSystemId(), mavlink->getComponentId(), &msg,
time_us, xacc_corrupt, yacc_corrupt, zacc_corrupt, rollspeed_corrupt, pitchspeed_corrupt,
yawspeed_corrupt, xmag_corrupt, ymag_corrupt, zmag_corrupt, abs_pressure_corrupt,
diff_pressure_corrupt, pressure_alt_corrupt, temperature_corrupt, fields_changed);
lastSendTimeSensors = QGC::groundTimeMilliseconds();
}
else
{
// Attempt to set HIL mode
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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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setMode(base_mode | MAV_MODE_FLAG_HIL_ENABLED, custom_mode);
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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(uint8_t base_mode, uint32_t custom_mode) const
QString mode = AutoPilotPluginManager::instance()->getAudioModeText(base_mode, custom_mode, autopilot);
if (mode.length() == 0)
// Fall back to generic decoding
QString mode;
uint8_t modeid = base_mode;
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// 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";
}
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 depends on the specific autopilot used.
* @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 (!_containsLink(link))
_links.append(LinkManager::instance()->sharedPointerForLink(link));
qCDebug(UASLog) << "addLink:" << QString("%1").arg((ulong)link, 0, 16);
connect(LinkManager::instance(), &LinkManager::linkDisconnected, this, &UAS::_linkDisconnected);
void UAS::_linkDisconnected(LinkInterface* link)
qCDebug(UASLog) << "_linkDisconnected:" << link->getName();
qCDebug(UASLog) << "link count:" << _links.count();
for (int i=0; i<_links.count(); i++) {
if (_links[i].data() == link) {
_links.removeAt(i);
break;
}
}
if (_links.count() == 0) {
// Remove the UAS when all links to it close
UASManager::instance()->removeUAS(this);
}
}
/**
* @return the list of links
*/
QList<LinkInterface*> UAS::getLinks()
QList<LinkInterface*> list;
foreach (SharedLinkInterface sharedLink, _links) {
list << sharedLink.data();
}
return list;
}
/**
* @rerturn the map of the components
*/
QMap<int, QString> UAS::getComponents()
{
return components;
}
/**
* Set the battery specificaitons: empty voltage, warning voltage, and full voltage.
* @param specifications of the battery
*/
void UAS::setBatterySpecs(const QString& specs)
{
batteryRemainingEstimateEnabled = false;
bool ok;
QString percent = specs;
percent = percent.remove("%");
float temp = percent.toFloat(&ok);
if (ok)
}
else
{
emit textMessageReceived(0, 0, MAV_SEVERITY_WARNING, "Could not set battery options, format is wrong");
}
}
/**
* @return the battery specifications(empty voltage, warning voltage, full voltage)
*/
QString UAS::getBatterySpecs()
{
return QString("%1%").arg(warnLevelPercent);
}
/**
* @return the time remaining.
*/
int UAS::calculateTimeRemaining()
{
}
/**
* @return charge level in percent - 0 - 100
*/
float UAS::getChargeLevel()
{
return chargeLevel;
}
void UAS::startLowBattAlarm()
{
if (!lowBattAlarm)
{
GAudioOutput::instance()->alert(tr("System %1 has low battery").arg(getUASID()));
lowBattAlarm = true;
}
}
void UAS::stopLowBattAlarm()
{
if (lowBattAlarm)
{
lowBattAlarm = false;
}
}
void UAS::sendMapRCToParam(QString param_id, float scale, float value0, quint8 param_rc_channel_index, float valueMin, float valueMax)
{
mavlink_message_t message;
char param_id_cstr[MAVLINK_MSG_PARAM_MAP_RC_FIELD_PARAM_ID_LEN] = {};
// Copy string into buffer, ensuring not to exceed the buffer size
for (unsigned int i = 0; i < sizeof(param_id_cstr); i++)
{
if ((int)i < param_id.length())
{
param_id_cstr[i] = param_id.toLatin1()[i];
}
}
mavlink_msg_param_map_rc_pack(mavlink->getSystemId(),
mavlink->getComponentId(),
&message,
this->uasId,
0,
param_id_cstr,
value0,
scale,
valueMin,
valueMax);
sendMessage(message);
qDebug() << "Mavlink message sent";
}
void UAS::unsetRCToParameterMap()
{
char param_id_cstr[MAVLINK_MSG_PARAM_MAP_RC_FIELD_PARAM_ID_LEN] = {};
for (int i = 0; i < 3; i++) {
mavlink_message_t message;
mavlink_msg_param_map_rc_pack(mavlink->getSystemId(),
mavlink->getComponentId(),
&message,
this->uasId,
0,
param_id_cstr,
0.0f);
sendMessage(message);
}
}
bool UAS::_containsLink(LinkInterface* link)
{
foreach (SharedLinkInterface sharedLink, _links) {
if (sharedLink.data() == link) {
return true;
}
}
return false;
}