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/****************************************************************************
*
* (c) 2009-2020 QGROUNDCONTROL PROJECT <http://www.qgroundcontrol.org>
*
* QGroundControl is licensed according to the terms in the file
* COPYING.md in the root of the source code directory.
*
****************************************************************************/
// NO NEW CODE HERE
// UASInterface, UAS.h/cc are deprecated. All new functionality should go into Vehicle.h/cc
//
#include <QList>
#include <QTimer>
#include <QSettings>
#include <iostream>
#include <QDebug>
#include <cmath>
#include <qmath.h>
#include <limits>
#include <cstdlib>
#include "UAS.h"
#include "LinkInterface.h"
#include "QGC.h"
#include "MAVLinkProtocol.h"
#include "QGCMAVLink.h"
#include "LinkManager.h"
#include "SerialLink.h"
#include "QGCLoggingCategory.h"
#include "QGCApplication.h"
QGC_LOGGING_CATEGORY(UASLog, "UASLog")
// THIS CLASS IS DEPRECATED. ALL NEW FUNCTIONALITY SHOULD GO INTO Vehicle class
UAS::UAS(MAVLinkProtocol* protocol, Vehicle* vehicle, FirmwarePluginManager * firmwarePluginManager) : UASInterface(),
lipoFull(4.2f),
lipoEmpty(3.5f),
unknownPackets(),
mavlink(protocol),
receiveDropRate(0),
sendDropRate(0),
status(-1),
startTime(QGC::groundTimeMilliseconds()),
onboardTimeOffset(0),
controlRollManual(true),
controlPitchManual(true),
controlYawManual(true),
controlThrustManual(true),
attitudeKnown(false),
attitudeStamped(false),
lastAttitude(0),
imagePackets(0), // We must initialize to 0, otherwise extended data packets maybe incorrectly thought to be images
// Note variances calculated from flight case from this log: http://dash.oznet.ch/view/MRjW8NUNYQSuSZkbn8dEjY
// TODO: calibrate stand-still pixhawk variances
xacc_var(0.6457f),
zacc_var(0.97885f),
rollspeed_var(0.8126f),
pitchspeed_var(0.6145f),
yawspeed_var(0.5852f),
xmag_var(0.2393f),
ymag_var(0.2283f),
zmag_var(0.1665f),
abs_pressure_var(0.5802f),
diff_pressure_var(0.5802f),
pressure_alt_var(0.5802f),
temperature_var(0.7145f),
Lorenz Meier
committed
/*
xacc_var(0.0f),
yacc_var(0.0f),
zacc_var(0.0f),
rollspeed_var(0.0f),
pitchspeed_var(0.0f),
yawspeed_var(0.0f),
xmag_var(0.0f),
ymag_var(0.0f),
zmag_var(0.0f),
abs_pressure_var(0.0f),
diff_pressure_var(0.0f),
pressure_alt_var(0.0f),
temperature_var(0.0f),
Lorenz Meier
committed
*/
// The protected members.
connectionLost(false),
lastVoltageWarning(0),
lastNonNullTime(0),
onboardTimeOffsetInvalidCount(0),
_vehicle(vehicle),
_firmwarePluginManager(firmwarePluginManager)
}
/**
* @ return the id of the uas
*/
int UAS::getUASID() const
{
return uasId;
}
// Ignore warnings from mavlink headers for both GCC/Clang and MSVC
#ifdef __GNUC__
#if __GNUC__ > 8
#pragma GCC diagnostic push
#pragma GCC diagnostic ignored "-Waddress-of-packed-member"
#elif defined(__clang__)
#pragma clang diagnostic push
#pragma clang diagnostic ignored "-Waddress-of-packed-member"
#else
#pragma GCC diagnostic push
#pragma GCC diagnostic ignored "-Wall"
#endif
#else
#pragma warning(push, 0)
#endif
void UAS::receiveMessage(mavlink_message_t message)
{
// Only accept messages from this system (condition 1)
// and only then if a) attitudeStamped is disabled OR b) attitudeStamped is enabled
// and we already got one attitude packet
if (message.sysid == uasId && (!attitudeStamped || lastAttitude != 0 || message.msgid == MAVLINK_MSG_ID_ATTITUDE))
{
bool multiComponentSourceDetected = false;
bool wrongComponent = false;
switch (message.compid)
{
case MAV_COMP_ID_IMU_2:
// Prefer IMU 2 over IMU 1 (FIXME)
componentID[message.msgid] = MAV_COMP_ID_IMU_2;
break;
default:
// Do nothing
break;
}
// Store component ID
{
// Prefer the first component
componentID[message.msgid] = message.compid;
}
else
{
// Got this message already
if (componentID[message.msgid] != message.compid)
{
componentMulti[message.msgid] = true;
wrongComponent = true;
}
}
if (componentMulti[message.msgid] == true) {
multiComponentSourceDetected = true;
}
switch (message.msgid)
{
case MAVLINK_MSG_ID_HEARTBEAT:
{
if (multiComponentSourceDetected && wrongComponent)
{
break;
}
mavlink_heartbeat_t state;
mavlink_msg_heartbeat_decode(&message, &state);
// Send the base_mode and system_status values to the plotter. This uses the ground time
// so the Ground Time checkbox must be ticked for these values to display
quint64 time = getUnixTime();
QString name = QString("M%1:HEARTBEAT.%2").arg(message.sysid);
emit valueChanged(uasId, name.arg("base_mode"), "bits", state.base_mode, time);
emit valueChanged(uasId, name.arg("custom_mode"), "bits", state.custom_mode, time);
emit valueChanged(uasId, name.arg("system_status"), "-", state.system_status, time);
case MAVLINK_MSG_ID_SYS_STATUS:
{
if (multiComponentSourceDetected && wrongComponent)
{
break;
}
mavlink_sys_status_t state;
mavlink_msg_sys_status_decode(&message, &state);
// Prepare for sending data to the realtime plotter, which is every field excluding onboard_control_sensors_present.
quint64 time = getUnixTime();
QString name = QString("M%1:SYS_STATUS.%2").arg(message.sysid);
emit valueChanged(uasId, name.arg("sensors_enabled"), "bits", state.onboard_control_sensors_enabled, time);
emit valueChanged(uasId, name.arg("sensors_health"), "bits", state.onboard_control_sensors_health, time);
emit valueChanged(uasId, name.arg("errors_comm"), "-", state.errors_comm, time);
emit valueChanged(uasId, name.arg("errors_count1"), "-", state.errors_count1, time);
emit valueChanged(uasId, name.arg("errors_count2"), "-", state.errors_count2, time);
emit valueChanged(uasId, name.arg("errors_count3"), "-", state.errors_count3, time);
emit valueChanged(uasId, name.arg("errors_count4"), "-", state.errors_count4, time);
// Process CPU load.
emit valueChanged(uasId, name.arg("load"), "%", state.load/10.0f, time);
emit valueChanged(uasId, name.arg("drop_rate_comm"), "%", state.drop_rate_comm/100.0f, time);
}
case MAVLINK_MSG_ID_PARAM_VALUE:
{
mavlink_param_value_t rawValue;
mavlink_msg_param_value_decode(&message, &rawValue);
QByteArray bytes(rawValue.param_id, MAVLINK_MSG_PARAM_VALUE_FIELD_PARAM_ID_LEN);
// Construct a string stopping at the first NUL (0) character, else copy the whole
// byte array (max MAVLINK_MSG_PARAM_VALUE_FIELD_PARAM_ID_LEN, so safe)
QString parameterName(bytes);
mavlink_param_union_t paramVal;
paramVal.param_float = rawValue.param_value;
paramVal.type = rawValue.param_type;
processParamValueMsg(message, parameterName,rawValue,paramVal);
}
Lorenz Meier
committed
case MAVLINK_MSG_ID_ATTITUDE_TARGET:
Lorenz Meier
committed
mavlink_attitude_target_t out;
mavlink_msg_attitude_target_decode(&message, &out);
float roll, pitch, yaw;
mavlink_quaternion_to_euler(out.q, &roll, &pitch, &yaw);
quint64 time = getUnixTimeFromMs(out.time_boot_ms);
// For plotting emit roll sp, pitch sp and yaw sp values
emit valueChanged(uasId, "roll sp", "rad", roll, time);
emit valueChanged(uasId, "pitch sp", "rad", pitch, time);
emit valueChanged(uasId, "yaw sp", "rad", yaw, time);
case MAVLINK_MSG_ID_DATA_TRANSMISSION_HANDSHAKE:
{
mavlink_data_transmission_handshake_t p;
mavlink_msg_data_transmission_handshake_decode(&message, &p);
imageSize = p.size;
imagePackets = p.packets;
imagePayload = p.payload;
imageQuality = p.jpg_quality;
imageType = p.type;
imageWidth = p.width;
imageHeight = p.height;
imageStart = QGC::groundTimeMilliseconds();
}
break;
case MAVLINK_MSG_ID_ENCAPSULATED_DATA:
{
mavlink_encapsulated_data_t img;
mavlink_msg_encapsulated_data_decode(&message, &img);
int seq = img.seqnr;
int pos = seq * imagePayload;
// Check if we have a valid transaction
if (imagePackets == 0)
{
// NO VALID TRANSACTION - ABORT
// Restart statemachine
imagePacketsArrived = 0;
}
for (int i = 0; i < imagePayload; ++i)
{
if (pos <= imageSize) {
imageRecBuffer[pos] = img.data[i];
}
++pos;
}
++imagePacketsArrived;
// emit signal if all packets arrived
if (imagePacketsArrived >= imagePackets)
{
// Restart statemachine
emit imageReady(this);
}
}
break;
case MAVLINK_MSG_ID_LOG_ENTRY:
{
mavlink_log_entry_t log;
mavlink_msg_log_entry_decode(&message, &log);
emit logEntry(this, log.time_utc, log.size, log.id, log.num_logs, log.last_log_num);
}
break;
case MAVLINK_MSG_ID_LOG_DATA:
{
mavlink_log_data_t log;
mavlink_msg_log_data_decode(&message, &log);
emit logData(this, log.ofs, log.id, log.count, log.data);
}
break;
default:
break;
}
}
}
// Pop warnings ignoring for mavlink headers for both GCC/Clang and MSVC
#ifdef __GNUC__
#if defined(__clang__)
#pragma clang diagnostic pop
#else
#pragma GCC diagnostic pop
#endif
#else
#pragma warning(pop, 0)
#endif
/**
* Check if time is smaller than 40 years, assuming no system without Unix
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* 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.
*/
quint64 UAS::getUnixReferenceTime(quint64 time)
{
// Same as getUnixTime, but does not react to attitudeStamped mode
if (time == 0)
{
// qDebug() << "XNEW time:" <<QGC::groundTimeMilliseconds();
return QGC::groundTimeMilliseconds();
}
// 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
else if (time < 1261440000000000)
#endif
{
// qDebug() << "GEN time:" << time/1000 + onboardTimeOffset;
if (onboardTimeOffset == 0)
{
onboardTimeOffset = QGC::groundTimeMilliseconds() - 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;
}
}
/**
* @warning If attitudeStamped is enabled, this function will not actually return
* the precise time stamp of this measurement augmented to UNIX time, but will
* MOVE the timestamp IN TIME to match the last measured attitude. There is no
* reason why one would want this, except for system setups where the onboard
* clock is not present or broken and datasets should be collected that are still
* roughly synchronized. PLEASE NOTE THAT ENABLING ATTITUDE STAMPED RUINS THE
* SCIENTIFIC NATURE OF THE CORRECT LOGGING FUNCTIONS OF QGROUNDCONTROL!
*/
quint64 UAS::getUnixTimeFromMs(quint64 time)
{
return getUnixTime(time*1000);
}
/**
* @warning If attitudeStamped is enabled, this function will not actually return
* the precise time stam of this measurement augmented to UNIX time, but will
* MOVE the timestamp IN TIME to match the last measured attitude. There is no
* reason why one would want this, except for system setups where the onboard
* clock is not present or broken and datasets should be collected that are
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* still roughly synchronized. PLEASE NOTE THAT ENABLING ATTITUDE STAMPED
* RUINS THE SCIENTIFIC NATURE OF THE CORRECT LOGGING FUNCTIONS OF QGROUNDCONTROL!
*/
quint64 UAS::getUnixTime(quint64 time)
{
quint64 ret = 0;
if (attitudeStamped)
{
ret = lastAttitude;
}
if (time == 0)
{
ret = QGC::groundTimeMilliseconds();
}
// 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
else if (time < 1261440000000000)
#endif
{
// qDebug() << "GEN time:" << time/1000 + onboardTimeOffset;
if (onboardTimeOffset == 0 || time < (lastNonNullTime - 100))
{
lastNonNullTime = time;
onboardTimeOffset = QGC::groundTimeMilliseconds() - time/1000;
}
if (time > lastNonNullTime) lastNonNullTime = time;
ret = time/1000 + onboardTimeOffset;
}
else
{
// Time is not zero and larger than 40 years -> has to be
// a Unix epoch timestamp. Do nothing.
ret = time/1000;
}
return ret;
}
/**
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* Get the status of the code and a description of the status.
* Status can be unitialized, booting up, calibrating sensors, active
* standby, cirtical, emergency, shutdown or unknown.
*/
void UAS::getStatusForCode(int statusCode, QString& uasState, QString& stateDescription)
{
switch (statusCode)
{
case MAV_STATE_UNINIT:
uasState = tr("UNINIT");
stateDescription = tr("Unitialized, booting up.");
break;
case MAV_STATE_BOOT:
uasState = tr("BOOT");
stateDescription = tr("Booting system, please wait.");
break;
case MAV_STATE_CALIBRATING:
uasState = tr("CALIBRATING");
stateDescription = tr("Calibrating sensors, please wait.");
break;
case MAV_STATE_ACTIVE:
uasState = tr("ACTIVE");
stateDescription = tr("Active, normal operation.");
break;
case MAV_STATE_STANDBY:
uasState = tr("STANDBY");
stateDescription = tr("Standby mode, ready for launch.");
break;
case MAV_STATE_CRITICAL:
uasState = tr("CRITICAL");
stateDescription = tr("FAILURE: Continuing operation.");
break;
case MAV_STATE_EMERGENCY:
uasState = tr("EMERGENCY");
stateDescription = tr("EMERGENCY: Land Immediately!");
break;
//case MAV_STATE_HILSIM:
//uasState = tr("HIL SIM");
//stateDescription = tr("HIL Simulation, Sensors read from SIM");
//break;
case MAV_STATE_POWEROFF:
uasState = tr("SHUTDOWN");
stateDescription = tr("Powering off system.");
break;
default:
uasState = tr("UNKNOWN");
stateDescription = tr("Unknown system state");
break;
}
}
QImage UAS::getImage()
{
// qDebug() << "IMAGE TYPE:" << imageType;
// RAW greyscale
if (imageType == MAVLINK_DATA_STREAM_IMG_RAW8U)
{
// Construct PGM header
QString header("P5\n%1 %2\n%3\n");
header = header.arg(imageWidth).arg(imageHeight).arg(imgColors);
QByteArray tmpImage(header.toStdString().c_str(), header.length());
tmpImage.append(imageRecBuffer);
//qDebug() << "IMAGE SIZE:" << tmpImage.size() << "HEADER SIZE: (15):" << header.size() << "HEADER: " << header;
if (imageRecBuffer.isNull())
{
qDebug()<< "could not convertToPGM()";
return QImage();
}
if (!image.loadFromData(tmpImage, "PGM"))
{
qDebug()<< __FILE__ << __LINE__ << "could not create extracted image";
return QImage();
}
}
// BMP with header
else if (imageType == MAVLINK_DATA_STREAM_IMG_BMP ||
imageType == MAVLINK_DATA_STREAM_IMG_JPEG ||
imageType == MAVLINK_DATA_STREAM_IMG_PGM ||
imageType == MAVLINK_DATA_STREAM_IMG_PNG)
{
if (!image.loadFromData(imageRecBuffer))
{
qDebug() << __FILE__ << __LINE__ << "Loading data from image buffer failed!";
// Restart statemachine
imagePacketsArrived = 0;
imagePackets = 0;
imageRecBuffer.clear();
return image;
}
void UAS::requestImage()
{
if (!_vehicle) {
return;
}
qDebug() << "trying to get an image from the uas...";
// check if there is already an image transmission going on
if (imagePacketsArrived == 0)
{
mavlink_message_t msg;
mavlink_msg_data_transmission_handshake_pack_chan(mavlink->getSystemId(),
mavlink->getComponentId(),
_vehicle->priorityLink()->mavlinkChannel(),
&msg,
MAVLINK_DATA_STREAM_IMG_JPEG,
0, 0, 0, 0, 0, 50);
}
}
/* MANAGEMENT */
/**
*
* @return The uptime in milliseconds
*
*/
quint64 UAS::getUptime() const
{
if(startTime == 0)
{
return 0;
}
else
{
return QGC::groundTimeMilliseconds() - startTime;
}
}
//TODO update this to use the parameter manager / param data model instead
void UAS::processParamValueMsg(mavlink_message_t& msg, const QString& paramName, const mavlink_param_value_t& rawValue, mavlink_param_union_t& paramUnion)
{
int compId = msg.compid;
// Insert with correct type
switch (rawValue.param_type) {
case MAV_PARAM_TYPE_REAL32:
case MAV_PARAM_TYPE_UINT16:
paramValue = QVariant(paramUnion.param_uint16);
break;
case MAV_PARAM_TYPE_UINT32:
//-- Note: These are not handled above:
//
// MAV_PARAM_TYPE_UINT64
// MAV_PARAM_TYPE_INT64
// MAV_PARAM_TYPE_REAL64
//
// No space in message (the only storage allocation is a "float") and not present in mavlink_param_union_t
default:
qCritical() << "INVALID DATA TYPE USED AS PARAMETER VALUE: " << rawValue.param_type;
qCDebug(UASLog) << "Received PARAM_VALUE" << paramName << paramValue << rawValue.param_type;
emit parameterUpdate(uasId, compId, paramName, rawValue.param_count, rawValue.param_index, rawValue.param_type, paramValue);
*/
void UAS::pairRX(int rxType, int rxSubType)
{
if (_vehicle) {
_vehicle->sendMavCommand(_vehicle->defaultComponentId(), // target component
MAV_CMD_START_RX_PAIR, // command id
true, // showError
rxType,
rxSubType);