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/****************************************************************************
*
* (c) 2009-2016 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
//
#ifndef _UAS_H_
#define _UAS_H_
#include "UASInterface.h"
#include <MAVLinkProtocol.h>
#include <QVector3D>
#include "QGCMAVLink.h"
#include "QGCHilLink.h"
#include "QGCFlightGearLink.h"
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#include "QGCJSBSimLink.h"
#include "QGCXPlaneLink.h"
Q_DECLARE_LOGGING_CATEGORY(UASLog)
/**
* @brief A generic MAVLINK-connected MAV/UAV
*
* This class represents one vehicle. It can be used like the real vehicle, e.g. a call to halt()
* will automatically send the appropriate messages to the vehicle. The vehicle state will also be
* automatically updated by the comm architecture, so when writing code to e.g. control the vehicle
* no knowledge of the communication infrastructure is needed.
*/
class UAS : public UASInterface
{
Q_OBJECT
public:
UAS(MAVLinkProtocol* protocol, Vehicle* vehicle, FirmwarePluginManager * firmwarePluginManager);
float lipoFull; ///< 100% charged voltage
float lipoEmpty; ///< Discharged voltage
/* MANAGEMENT */
/** @brief Get the unique system id */
int getUASID() const;
/** @brief Get the components */
QMap<int, QString> getComponents();
/** @brief The time interval the robot is switched on */
quint64 getUptime() const;
Q_PROPERTY(double roll READ getRoll WRITE setRoll NOTIFY rollChanged)
Q_PROPERTY(double pitch READ getPitch WRITE setPitch NOTIFY pitchChanged)
Q_PROPERTY(double yaw READ getYaw WRITE setYaw NOTIFY yawChanged)
/// Vehicle is about to go away
void shutdownVehicle(void);
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void setRoll(double val)
{
roll = val;
emit rollChanged(val,"roll");
}
double getRoll() const
{
return roll;
}
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void setPitch(double val)
{
pitch = val;
emit pitchChanged(val,"pitch");
}
double getPitch() const
{
return pitch;
}
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void setYaw(double val)
{
yaw = val;
emit yawChanged(val,"yaw");
}
double getYaw() const
{
return yaw;
}
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// Setters for HIL noise variance
void setXaccVar(float var){
xacc_var = var;
}
void setYaccVar(float var){
yacc_var = var;
}
void setZaccVar(float var){
zacc_var = var;
}
void setRollSpeedVar(float var){
rollspeed_var = var;
}
void setPitchSpeedVar(float var){
pitchspeed_var = var;
}
void setYawSpeedVar(float var){
pitchspeed_var = var;
}
void setXmagVar(float var){
xmag_var = var;
}
void setYmagVar(float var){
ymag_var = var;
}
void setZmagVar(float var){
zmag_var = var;
}
void setAbsPressureVar(float var){
abs_pressure_var = var;
}
void setDiffPressureVar(float var){
diff_pressure_var = var;
}
void setPressureAltVar(float var){
pressure_alt_var = var;
}
void setTemperatureVar(float var){
temperature_var = var;
}
protected: //COMMENTS FOR TEST UNIT
int uasId; ///< Unique system ID
QMap<int, QString> components;///< IDs and names of all detected onboard components
QList<int> unknownPackets; ///< Packet IDs which are unknown and have been received
MAVLinkProtocol* mavlink; ///< Reference to the MAVLink instance
float receiveDropRate; ///< Percentage of packets that were dropped on the MAV's receiving link (from GCS and other MAVs)
float sendDropRate; ///< Percentage of packets that were not received from the MAV by the GCS
/// BASIC UAS TYPE, NAME AND STATE
int status; ///< The current status of the MAV
/// TIMEKEEPING
quint64 startTime; ///< The time the UAS was switched on
quint64 onboardTimeOffset;
bool controlRollManual; ///< status flag, true if roll is controlled manually
bool controlPitchManual; ///< status flag, true if pitch is controlled manually
bool controlYawManual; ///< status flag, true if yaw is controlled manually
bool controlThrustManual; ///< status flag, true if thrust is controlled manually
double manualRollAngle; ///< Roll angle set by human pilot (radians)
double manualPitchAngle; ///< Pitch angle set by human pilot (radians)
double manualYawAngle; ///< Yaw angle set by human pilot (radians)
double manualThrust; ///< Thrust set by human pilot (radians)
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bool isGlobalPositionKnown; ///< If the global position has been received for this MAV
/// ATTITUDE
bool attitudeKnown; ///< True if attitude was received, false else
bool attitudeStamped; ///< Should arriving data be timestamped with the last attitude? This helps with broken system time clocks on the MAV
quint64 lastAttitude; ///< Timestamp of last attitude measurement
double roll;
double pitch;
double yaw;
// dongfang: This looks like a candidate for being moved off to a separate class.
/// IMAGING
int imageSize; ///< Image size being transmitted (bytes)
int imagePackets; ///< Number of data packets being sent for this image
int imagePacketsArrived; ///< Number of data packets received
int imagePayload; ///< Payload size per transmitted packet (bytes). Standard is 254, and decreases when image resolution increases.
int imageQuality; ///< Quality of the transmitted image (percentage)
int imageType; ///< Type of the transmitted image (BMP, PNG, JPEG, RAW 8 bit, RAW 32 bit)
int imageWidth; ///< Width of the image stream
int imageHeight; ///< Width of the image stream
QByteArray imageRecBuffer; ///< Buffer for the incoming bytestream
QImage image; ///< Image data of last completely transmitted image
quint64 imageStart;
bool blockHomePositionChanges; ///< Block changes to the home position
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bool receivedMode; ///< True if mode was retrieved from current conenction to UAS
/// SIMULATION NOISE
float xacc_var; ///< variance of x acclerometer noise for HIL sim (mg)
float yacc_var; ///< variance of y acclerometer noise for HIL sim (mg)
float zacc_var; ///< variance of z acclerometer noise for HIL sim (mg)
float rollspeed_var; ///< variance of x gyroscope noise for HIL sim (rad/s)
float pitchspeed_var; ///< variance of y gyroscope noise for HIL sim (rad/s)
float yawspeed_var; ///< variance of z gyroscope noise for HIL sim (rad/s)
float xmag_var; ///< variance of x magnatometer noise for HIL sim (???)
float ymag_var; ///< variance of y magnatometer noise for HIL sim (???)
float zmag_var; ///< variance of z magnatometer noise for HIL sim (???)
float abs_pressure_var; ///< variance of absolute pressure noise for HIL sim (hPa)
float diff_pressure_var; ///< variance of differential pressure noise for HIL sim (hPa)
float pressure_alt_var; ///< variance of altitude pressure noise for HIL sim (hPa)
float temperature_var; ///< variance of temperature noise for HIL sim (C)
QGCHilLink* simulation; ///< Hardware in the loop simulation link
public:
/** @brief Get the human-readable status message for this code */
void getStatusForCode(int statusCode, QString& uasState, QString& stateDescription);
#ifndef __mobile__
virtual FileManager* getFileManager() { return &fileManager; }
#endif
/** @brief Get the HIL simulation */
QGCHilLink* getHILSimulation() const {
return simulation;
}
QImage getImage();
void requestImage();
public slots:
/** @brief Order the robot to pair its receiver **/
void pairRX(int rxType, int rxSubType);
/** @brief Enable / disable HIL */
void enableHilFlightGear(bool enable, QString options, bool sensorHil, QObject * configuration);
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void enableHilJSBSim(bool enable, QString options);
void enableHilXPlane(bool enable);
/** @brief Send the full HIL state to the MAV */
void sendHilState(quint64 time_us, float roll, float pitch, float yaw, float rollRotationRate,
float pitchRotationRate, float yawRotationRate, double lat, double lon, double alt,
float vx, float vy, float vz, float ind_airspeed, float true_airspeed, float xacc, float yacc, float zacc);
void sendHilGroundTruth(quint64 time_us, float roll, float pitch, float yaw, float rollRotationRate,
float pitchRotationRate, float yawRotationRate, double lat, double lon, double alt,
float vx, float vy, float vz, float ind_airspeed, float true_airspeed, float xacc, float yacc, float zacc);
void 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);
/** @brief Send Optical Flow sensor message for HIL, (arguments and units accoding to mavlink documentation*/
void 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);
float addZeroMeanNoise(float truth_meas, float noise_var);
/**
* @param time_us
* @param lat
* @param lon
* @param alt
* @param fix_type
* @param eph
* @param epv
* @param vel
* @param cog course over ground, in radians, -pi..pi
* @param satellites
*/
void 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);
/** @brief Places the UAV in Hardware-in-the-Loop simulation status **/
void startHil();
/** @brief Stops the UAV's Hardware-in-the-Loop simulation status **/
void stopHil();
/** @brief Set the values for the manual control of the vehicle */
void setExternalControlSetpoint(float roll, float pitch, float yaw, float thrust, quint16 buttons, int joystickMode);
/** @brief Set the values for the 6dof manual control of the vehicle */
void setManual6DOFControlCommands(double x, double y, double z, double roll, double pitch, double yaw);
/** @brief Receive a message from one of the communication links. */
virtual void receiveMessage(mavlink_message_t message);
void startCalibration(StartCalibrationType calType);
void stopCalibration(void);
void startBusConfig(StartBusConfigType calType);
void stopBusConfig(void);
/** @brief Send command to map a RC channel to a parameter */
void sendMapRCToParam(QString param_id, float scale, float value0, quint8 param_rc_channel_index, float valueMin, float valueMax);
/** @brief Send command to disable all bindings/maps between RC and parameters */
void unsetRCToParameterMap();
signals:
void imageStarted(quint64 timestamp);
/** @brief A new camera image has arrived */
void imageReady(UASInterface* uas);
/** @brief HIL controls have changed */
void hilControlsChanged(quint64 time, float rollAilerons, float pitchElevator, float yawRudder, float throttle, quint8 systemMode, quint8 navMode);
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void rollChanged(double val,QString name);
void pitchChanged(double val,QString name);
void yawChanged(double val,QString name);
protected:
/** @brief Get the UNIX timestamp in milliseconds, enter microseconds */
quint64 getUnixTime(quint64 time=0);
/** @brief Get the UNIX timestamp in milliseconds, enter milliseconds */
quint64 getUnixTimeFromMs(quint64 time);
/** @brief Get the UNIX timestamp in milliseconds, ignore attitudeStamped mode */
quint64 getUnixReferenceTime(quint64 time);
virtual void processParamValueMsg(mavlink_message_t& msg, const QString& paramName,const mavlink_param_value_t& rawValue, mavlink_param_union_t& paramValue);
int componentID[256];
bool componentMulti[256];
bool connectionLost; ///< Flag indicates a timed out connection
quint64 connectionLossTime; ///< Time the connection was interrupted
quint64 lastVoltageWarning; ///< Time at which the last voltage warning occurred
quint64 lastNonNullTime; ///< The last timestamp from the MAV that was not null
unsigned int onboardTimeOffsetInvalidCount; ///< Count when the offboard time offset estimation seemed wrong
bool sensorHil; ///< True if sensor HIL is enabled
quint64 lastSendTimeGPS; ///< Last HIL GPS message sent
quint64 lastSendTimeSensors; ///< Last HIL Sensors message sent
quint64 lastSendTimeOpticalFlow; ///< Last HIL Optical Flow message sent
private:
void _say(const QString& text, int severity = 6);
Vehicle* _vehicle;
FirmwarePluginManager* _firmwarePluginManager;
};
#endif // _UAS_H_