mirror of https://github.com/ArduPilot/ardupilot
Bug located in quad position loop, improved hil.
This commit is contained in:
parent
715a7cb748
commit
1c5db5e963
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@ -90,6 +90,7 @@ private:
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autoAttitudeLoop(dt);
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}
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void autoPositionLoop(float dt) {
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// XXX need to add waypoint coordinates
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float cmdNorthTilt = pidPN.update(_nav->getPN(),_nav->getVN(),dt);
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float cmdEastTilt = pidPE.update(_nav->getPE(),_nav->getVE(),dt);
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float cmdDown = pidPD.update(_nav->getPD(),_nav->getVD(),dt);
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@ -101,11 +102,6 @@ private:
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_cmdPitch = cmdEastTilt * trigCos - cmdNorthTilt * trigSin;
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_cmdRoll = -cmdEastTilt * trigSin + cmdNorthTilt * trigCos;
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// note that the north tilt is negative of the pitch
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Serial.print(" trigSin: ");
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Serial.print(trigSin);
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Serial.print(" trigCos: ");
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Serial.print(trigCos);
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}
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_cmdYawRate = 0;
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@ -117,34 +113,9 @@ private:
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if (fabs(_cmdPitch) > 0.5) _thrustMix *= 1.13949393;
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else _thrustMix /= cos(_cmdPitch);
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//debug statements
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Serial.print(" getPN: ");
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Serial.print(_nav->getPN());
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Serial.print(" getPE: ");
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Serial.print(_nav->getPE());
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Serial.print(" getPD: ");
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Serial.print(_nav->getPD());
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Serial.print(" getVN: ");
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Serial.print(_nav->getVN());
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Serial.print(" getVE: ");
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Serial.print(_nav->getVE());
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Serial.print(" getVD: ");
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Serial.println(_nav->getVD());
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//Serial.print("Roll: ");
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//Serial.print(_cmdRoll);
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//Serial.print(" Pitch");
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//Serial.print(_cmdPitch);
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//Serial.print(" YawRate");
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//Serial.print(_cmdYawRate);
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//Serial.print(" ThrustMix");
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//Serial.print(_thrustMix);
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//Serial.print(" North Tilt");
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//Serial.print(cmdNorthTilt);
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//Serial.print(" East Tilt");
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//Serial.print(cmdEastTilt);
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//Serial.print(" Down");
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//Serial.println(cmdDown);
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// debug for position loop
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_hal->debug->printf_P(PSTR("cmd: north tilt(%f), east tilt(%f), down(%f), pitch(%f), roll(%f)\n"),cmdNorthTilt,cmdEastTilt,cmdDown,_cmdPitch,_cmdRoll);
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}
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void autoAttitudeLoop(float dt) {
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_rollMix = pidRoll.update(_cmdRoll - _nav->getRoll(),
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@ -152,26 +123,6 @@ private:
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_pitchMix = pidPitch.update(_cmdPitch - _nav->getPitch(),
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_nav->getPitchRate(), dt);
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_yawMix = pidYawRate.update(_cmdYawRate - _nav->getYawRate(), dt);
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//debug statements
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//Serial.print("Roll Cmd: ");
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//Serial.print(_cmdRoll*1000);
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//Serial.print(" Nav_GetRoll: ");
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//Serial.print(_nav->getRoll()*1000);
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//Serial.print(" Roll Error: ");
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//Serial.print((_cmdRoll - _nav->getRoll())*1000);
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//Serial.print(" Pitch Cmd: ");
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//Serial.print(_cmdPitch*1000);
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//Serial.print(" Nav_GetPitch: ");
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//Serial.print(_nav->getPitch()*1000);
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//Serial.print(" Pitch Error: ");
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//Serial.println((_cmdPitch - _nav->getPitch())*1000);
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//Serial.print(" YawRate Cmd: ");
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//Serial.print(_cmdYawRate);
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//Serial.print(" Nav_GetYawRate: ");
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//Serial.print( _nav->getYawRate());
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//Serial.print(" YawRate Error: ");
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//Serial.println(_cmdYawRate - _nav->getYawRate());
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}
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void setMotorsActive() {
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@ -12,7 +12,7 @@
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static const apo::vehicle_t vehicle = apo::VEHICLE_QUAD;
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static const apo::halMode_t halMode = apo::MODE_HIL_CNTL;
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static const apo::board_t board = apo::BOARD_ARDUPILOTMEGA_1280;
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static const uint8_t heartBeatTimeout = 3;
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static const uint8_t heartBeatTimeout = 0;
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// algorithm selection
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#define CONTROLLER_CLASS ControllerQuad
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@ -30,7 +30,7 @@ static const uint8_t heartBeatTimeout = 3;
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static const uint32_t debugBaud = 57600;
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static const uint32_t telemBaud = 57600;
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static const uint32_t gpsBaud = 38400;
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static const uint32_t hilBaud = 57600;
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static const uint32_t hilBaud = 115200;
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// optional sensors
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static const bool gpsEnabled = false;
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@ -66,10 +66,10 @@ static const float PID_POS_I = 0;
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static const float PID_POS_D = 0;
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static const float PID_POS_LIM = 0; // about 5 deg
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static const float PID_POS_AWU = 0; // about 5 deg
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static const float PID_POS_Z_P = 0;
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static const float PID_POS_Z_P = 0.1;
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static const float PID_POS_Z_I = 0;
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static const float PID_POS_Z_D = 0;
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static const float PID_POS_Z_LIM = 0;
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static const float PID_POS_Z_D = 0.2;
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static const float PID_POS_Z_LIM = 0.1;
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static const float PID_POS_Z_AWU = 0;
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static const float PID_POS_DFCUT = 10; // cut derivative feedback at 10 hz
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@ -609,6 +609,3 @@ mark_as_advanced(ARDUINO_CORES_PATH
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ARDUINO_OBJCOPY_EEP_FLAGS
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ARDUINO_OBJCOPY_HEX_FLAGS)
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load_board_settings()
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endif()
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@ -131,21 +131,23 @@ void MavlinkComm::sendMessage(uint8_t id, uint32_t param) {
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*/
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case MAVLINK_MSG_ID_SCALED_IMU: {
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/*
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* accel/gyro debug
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*/
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/*
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Vector3f accel = _hal->imu->get_accel();
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Vector3f gyro = _hal->imu->get_gyro();
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Serial.printf_P(PSTR("accel: %f %f %f gyro: %f %f %f\n"),
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accel.x,accel.y,accel.z,gyro.x,gyro.y,gyro.z);
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*/
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Vector3f accel = _hal->imu->get_accel();
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Vector3f gyro = _hal->imu->get_gyro();
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mavlink_msg_raw_imu_send(_channel, timeStamp, 1000 * accel.x,
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1000 * accel.y, 1000 * accel.z, 1000 * gyro.x,
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1000 * gyro.y, 1000 * gyro.z, _hal->compass->mag_x,
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_hal->compass->mag_y, _hal->compass->mag_z); // XXX THIS IS NOT SCALED FOR MAG
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int16_t xmag, ymag, zmag;
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xmag = ymag = zmag = 0;
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if (_hal->compass) {
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// XXX THIS IS NOT SCALED
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xmag = _hal->compass->mag_x;
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ymag = _hal->compass->mag_y;
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zmag = _hal->compass->mag_z;
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}
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mavlink_msg_scaled_imu_send(_channel, timeStamp,
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_navigator->getXAccel()*1e3,
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_navigator->getYAccel()*1e3,
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_navigator->getZAccel()*1e3,
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_navigator->getRollRate()*1e3,
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_navigator->getPitchRate()*1e3,
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_navigator->getYawRate()*1e3,
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xmag, ymag, zmag);
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break;
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}
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case MAVLINK_MSG_ID_RC_CHANNELS_SCALED: {
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@ -352,6 +354,9 @@ void MavlinkComm::_handleMessage(mavlink_message_t * msg) {
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_navigator->setLat_degInt(packet.lat);
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_navigator->setLon_degInt(packet.lon);
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_navigator->setAlt(packet.alt / 1e3);
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_navigator->setXAccel(packet.xacc/ 1e3);
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_navigator->setYAccel(packet.xacc/ 1e3);
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_navigator->setZAccel(packet.xacc/ 1e3);
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break;
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}
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@ -391,31 +396,68 @@ void MavlinkComm::_handleMessage(mavlink_message_t * msg) {
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AP_Var::save_all();
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break;
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case MAV_ACTION_CALIBRATE_RC:
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case MAV_ACTION_MOTORS_START:
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_hal->setState(MAV_STATE_ACTIVE);
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break;
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case MAV_ACTION_CALIBRATE_GYRO:
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case MAV_ACTION_CALIBRATE_MAG:
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case MAV_ACTION_CALIBRATE_ACC:
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case MAV_ACTION_CALIBRATE_PRESSURE:
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_hal->setState(MAV_STATE_STANDBY);
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_navigator->calibrate();
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break;
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case MAV_ACTION_EMCY_KILL:
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case MAV_ACTION_CONFIRM_KILL:
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case MAV_ACTION_MOTORS_STOP:
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case MAV_ACTION_SHUTDOWN:
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_hal->setState(MAV_STATE_STANDBY);
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_controller->setMode(MAV_MODE_LOCKED);
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break;
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case MAV_ACTION_LAUNCH:
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case MAV_ACTION_TAKEOFF:
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_controller->setMode(MAV_MODE_AUTO);
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_guide->setMode(MAV_NAV_LIFTOFF);
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break;
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case MAV_ACTION_LAND:
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_guide->setCurrentIndex(0);
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_guide->setMode(MAV_NAV_LANDING);
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break;
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case MAV_ACTION_EMCY_LAND:
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_guide->setMode(MAV_NAV_LANDING);
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break;
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case MAV_ACTION_LOITER:
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case MAV_ACTION_HALT:
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_guide->setMode(MAV_NAV_LOITER);
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break;
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case MAV_ACTION_SET_AUTO:
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_controller->setMode(MAV_MODE_AUTO);
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break;
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case MAV_ACTION_SET_MANUAL:
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_controller->setMode(MAV_MODE_MANUAL);
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break;
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case MAV_ACTION_RETURN:
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_guide->setMode(MAV_NAV_RETURNING);
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break;
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case MAV_ACTION_NAVIGATE:
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case MAV_ACTION_CONTINUE:
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_guide->setMode(MAV_NAV_WAYPOINT);
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break;
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case MAV_ACTION_CALIBRATE_RC:
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case MAV_ACTION_REBOOT:
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case MAV_ACTION_REC_START:
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case MAV_ACTION_REC_PAUSE:
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case MAV_ACTION_REC_STOP:
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case MAV_ACTION_TAKEOFF:
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case MAV_ACTION_LAND:
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case MAV_ACTION_NAVIGATE:
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case MAV_ACTION_LOITER:
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case MAV_ACTION_MOTORS_START:
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case MAV_ACTION_CONFIRM_KILL:
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case MAV_ACTION_EMCY_KILL:
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case MAV_ACTION_MOTORS_STOP:
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case MAV_ACTION_SHUTDOWN:
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case MAV_ACTION_CONTINUE:
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case MAV_ACTION_SET_MANUAL:
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case MAV_ACTION_SET_AUTO:
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case MAV_ACTION_LAUNCH:
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case MAV_ACTION_RETURN:
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case MAV_ACTION_EMCY_LAND:
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case MAV_ACTION_HALT:
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sendText(SEVERITY_LOW, PSTR("action not implemented"));
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break;
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default:
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@ -49,18 +49,22 @@ void AP_Controller::update(const float dt) {
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//
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// check for heartbeat from gcs, if not found go to failsafe
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if (_hal->heartBeatLost()) {
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_mode = MAV_MODE_FAILSAFE;
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setMode(MAV_MODE_FAILSAFE);
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_hal->gcs->sendText(SEVERITY_HIGH, PSTR("configure gcs to send heartbeat"));
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// if battery less than 5%, go to failsafe
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} else if (_hal->batteryMonitor && _hal->batteryMonitor->getPercentage() < 5) {
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_mode = MAV_MODE_FAILSAFE;
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setMode(MAV_MODE_FAILSAFE);
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_hal->gcs->sendText(SEVERITY_HIGH, PSTR("recharge battery"));
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// manual/auto switch
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} else {
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// if all emergencies cleared, fall back to standby
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if (_hal->getState()==MAV_STATE_EMERGENCY) _hal->setState(MAV_STATE_STANDBY);
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if (_hal->rc[_chMode]->getRadioPosition() > 0) _mode = MAV_MODE_MANUAL;
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else _mode = MAV_MODE_AUTO;
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// if in auto mode and manual switch set, change to manual
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if (getMode()==MAV_MODE_AUTO && (_hal->rc[_chMode]->getRadioPosition() > 0)) setMode(MAV_MODE_MANUAL);
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// if in manual mode and auto switch set, switch to auto
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if (getMode()==MAV_MODE_MANUAL && (_hal->rc[_chMode]->getRadioPosition() < 0)) setMode(MAV_MODE_AUTO);
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}
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// handle flight modes
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@ -64,6 +64,10 @@ public:
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AP_Uint8 getMode() {
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return _mode;
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}
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void setMode(MAV_MODE mode) {
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_mode = mode;
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}
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protected:
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AP_Navigator * _nav;
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AP_Guide * _guide;
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@ -146,7 +146,7 @@ void MavlinkGuide::handleCommand() {
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// check if we are at waypoint or if command
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// radius is zero within tolerance
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if (distanceToNext < _command.getRadius() | distanceToNext < 1e-5) {
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if ( (distanceToNext < _command.getRadius()) | (distanceToNext < 1e-5) ) {
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_hal->gcs->sendText(SEVERITY_LOW,PSTR("waypoint reached (distance)"));
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_hal->debug->printf_P(PSTR("waypoint reached (distance)"));
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nextCommand();
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@ -217,9 +217,9 @@ void MavlinkGuide::handleCommand() {
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_pDCmd = _command.getPD(_navigator->getAlt_intM());
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// debug
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_hal->debug->printf_P(
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PSTR("guide loop, number: %d, current index: %d, previous index: %d\n"),
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getNumberOfCommands(), getCurrentIndex(), getPreviousIndex());
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//_hal->debug->printf_P(
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//PSTR("guide loop, number: %d, current index: %d, previous index: %d\n"),
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//getNumberOfCommands(), getCurrentIndex(), getPreviousIndex());
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}
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} // namespace apo
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@ -48,6 +48,11 @@ public:
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MAV_NAV getMode() const {
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return _mode;
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}
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void setMode(MAV_NAV mode) {
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_mode = mode;
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}
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uint8_t getCurrentIndex() {
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return _cmdIndex;
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}
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@ -187,15 +187,15 @@ public:
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_vD = vD;
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}
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void setXAcc(float xAccel) {
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void setXAccel(float xAccel) {
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_xAccel = xAccel;
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}
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void setYAcc(float yAccel) {
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void setYAccel(float yAccel) {
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_yAccel = yAccel;
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}
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void setZAcc(float zAccel) {
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void setZAccel(float zAccel) {
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_zAccel = zAccel;
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}
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