int do_level_calibration(orb_advert_t *mavlink_log_pub) {
const unsigned cal_time = 5;
const unsigned cal_hz = 100;
unsigned settle_time = 30;
bool success = false;
int att_sub = orb_subscribe(ORB_ID(vehicle_attitude));
struct vehicle_attitude_s att;
memset(&att, 0, sizeof(att));
calibration_log_info(mavlink_log_pub, CAL_QGC_STARTED_MSG, "level");
param_t roll_offset_handle = param_find("SENS_BOARD_X_OFF");
param_t pitch_offset_handle = param_find("SENS_BOARD_Y_OFF");
param_t board_rot_handle = param_find("SENS_BOARD_ROT");
// save old values if calibration fails
float roll_offset_current;
float pitch_offset_current;
int32_t board_rot_current = 0;
param_get(roll_offset_handle, &roll_offset_current);
param_get(pitch_offset_handle, &pitch_offset_current);
param_get(board_rot_handle, &board_rot_current);
// give attitude some time to settle if there have been changes to the board rotation parameters
if (board_rot_current == 0 && fabsf(roll_offset_current) < FLT_EPSILON && fabsf(pitch_offset_current) < FLT_EPSILON ) {
settle_time = 0;
}
float zero = 0.0f;
param_set_no_notification(roll_offset_handle, &zero);
param_set_no_notification(pitch_offset_handle, &zero);
param_notify_changes();
px4_pollfd_struct_t fds[1];
fds[0].fd = att_sub;
fds[0].events = POLLIN;
float roll_mean = 0.0f;
float pitch_mean = 0.0f;
unsigned counter = 0;
// sleep for some time
hrt_abstime start = hrt_absolute_time();
while(hrt_elapsed_time(&start) < settle_time * 1000000) {
calibration_log_info(mavlink_log_pub, CAL_QGC_PROGRESS_MSG, (int)(90*hrt_elapsed_time(&start)/1e6f/(float)settle_time));
sleep(settle_time / 10);
}
start = hrt_absolute_time();
// average attitude for 5 seconds
while(hrt_elapsed_time(&start) < cal_time * 1000000) {
int pollret = px4_poll(&fds[0], (sizeof(fds) / sizeof(fds[0])), 100);
if (pollret <= 0) {
// attitude estimator is not running
calibration_log_critical(mavlink_log_pub, "attitude estimator not running - check system boot");
calibration_log_critical(mavlink_log_pub, CAL_QGC_FAILED_MSG, "level");
goto out;
}
orb_copy(ORB_ID(vehicle_attitude), att_sub, &att);
matrix::Eulerf euler = matrix::Quatf(att.q);
roll_mean += euler.phi();
pitch_mean += euler.theta();
counter++;
}
calibration_log_info(mavlink_log_pub, CAL_QGC_PROGRESS_MSG, 100);
if (counter > (cal_time * cal_hz / 2 )) {
roll_mean /= counter;
pitch_mean /= counter;
} else {
calibration_log_info(mavlink_log_pub, "not enough measurements taken");
success = false;
goto out;
}
if (fabsf(roll_mean) > 0.8f ) {
calibration_log_critical(mavlink_log_pub, "excess roll angle");
} else if (fabsf(pitch_mean) > 0.8f ) {
calibration_log_critical(mavlink_log_pub, "excess pitch angle");
} else {
roll_mean *= (float)M_RAD_TO_DEG;
pitch_mean *= (float)M_RAD_TO_DEG;
param_set_no_notification(roll_offset_handle, &roll_mean);
param_set_no_notification(pitch_offset_handle, &pitch_mean);
param_notify_changes();
success = true;
}
out:
if (success) {
calibration_log_info(mavlink_log_pub, CAL_QGC_DONE_MSG, "level");
return 0;
} else {
// set old parameters
param_set_no_notification(roll_offset_handle, &roll_offset_current);
param_set_no_notification(pitch_offset_handle, &pitch_offset_current);
param_notify_changes();
calibration_log_critical(mavlink_log_pub, CAL_QGC_FAILED_MSG, "level");
return 1;
}
}
bool MulticopterLandDetector::get_landed_state()
{
// Time base for this function
const uint64_t now = hrt_absolute_time();
float sys_min_throttle = (_params.maxThrottle + 0.01f);
// Determine the system min throttle based on flight mode
if (!_ctrl_mode.flag_control_altitude_enabled) {
sys_min_throttle = (_params.minManThrottle + 0.01f);
}
// Check if thrust output is less than the minimum auto throttle param.
bool minimalThrust = (_actuators.control[3] <= sys_min_throttle);
if (minimalThrust && _min_trust_start == 0) {
_min_trust_start = now;
} else if (!minimalThrust) {
_min_trust_start = 0;
}
// only trigger flight conditions if we are armed
if (!_arming.armed) {
_arming_time = 0;
return true;
} else if (_arming_time == 0) {
_arming_time = now;
}
// If in manual flight mode never report landed if the user has more than idle throttle
// Check if user commands throttle and if so, report not landed based on
// the user intent to take off (even if the system might physically still have
// ground contact at this point).
if (_manual.timestamp > 0 && _manual.z > 0.15f && _ctrl_mode.flag_control_manual_enabled) {
return false;
}
// Return status based on armed state and throttle if no position lock is available.
if (_vehicleLocalPosition.timestamp == 0 ||
hrt_elapsed_time(&_vehicleLocalPosition.timestamp) > 500000 ||
!_vehicleLocalPosition.xy_valid ||
!_vehicleLocalPosition.z_valid) {
// The system has minimum trust set (manual or in failsafe)
// if this persists for 8 seconds AND the drone is not
// falling consider it to be landed. This should even sustain
// quite acrobatic flight.
if ((_min_trust_start > 0) &&
(hrt_elapsed_time(&_min_trust_start) > 8 * 1000 * 1000)) {
return !get_freefall_state();
} else {
return false;
}
}
float armThresholdFactor = 1.0f;
// Widen acceptance thresholds for landed state right after arming
// so that motor spool-up and other effects do not trigger false negatives.
if (hrt_elapsed_time(&_arming_time) < LAND_DETECTOR_ARM_PHASE_TIME) {
armThresholdFactor = 2.5f;
}
// Check if we are moving vertically - this might see a spike after arming due to
// throttle-up vibration. If accelerating fast the throttle thresholds will still give
// an accurate in-air indication.
bool verticalMovement = fabsf(_vehicleLocalPosition.vz) > _params.maxClimbRate * armThresholdFactor;
// Check if we are moving horizontally.
bool horizontalMovement = sqrtf(_vehicleLocalPosition.vx * _vehicleLocalPosition.vx
+ _vehicleLocalPosition.vy * _vehicleLocalPosition.vy) > _params.maxVelocity;
// Next look if all rotation angles are not moving.
float maxRotationScaled = _params.maxRotation_rad_s * armThresholdFactor;
bool rotating = (fabsf(_vehicleAttitude.rollspeed) > maxRotationScaled) ||
(fabsf(_vehicleAttitude.pitchspeed) > maxRotationScaled) ||
(fabsf(_vehicleAttitude.yawspeed) > maxRotationScaled);
if (verticalMovement || rotating || !minimalThrust || horizontalMovement) {
// Sensed movement or thottle high, so reset the land detector.
_landTimer = now;
return false;
}
return (now - _landTimer > LAND_DETECTOR_TRIGGER_TIME);
}
void
FixedwingEstimator::task_main()
{
_mavlink_fd = open(MAVLINK_LOG_DEVICE, 0);
_ekf = new AttPosEKF();
float dt = 0.0f; // time lapsed since last covariance prediction
_filter_start_time = hrt_absolute_time();
if (!_ekf) {
errx(1, "OUT OF MEM!");
}
/*
* do subscriptions
*/
_baro_sub = orb_subscribe(ORB_ID(sensor_baro));
_airspeed_sub = orb_subscribe(ORB_ID(airspeed));
_gps_sub = orb_subscribe(ORB_ID(vehicle_gps_position));
_vstatus_sub = orb_subscribe(ORB_ID(vehicle_status));
_params_sub = orb_subscribe(ORB_ID(parameter_update));
_home_sub = orb_subscribe(ORB_ID(home_position));
/* rate limit vehicle status updates to 5Hz */
orb_set_interval(_vstatus_sub, 200);
#ifndef SENSOR_COMBINED_SUB
_gyro_sub = orb_subscribe(ORB_ID(sensor_gyro));
_accel_sub = orb_subscribe(ORB_ID(sensor_accel));
_mag_sub = orb_subscribe(ORB_ID(sensor_mag));
/* rate limit gyro updates to 50 Hz */
/* XXX remove this!, BUT increase the data buffer size! */
orb_set_interval(_gyro_sub, 4);
#else
_sensor_combined_sub = orb_subscribe(ORB_ID(sensor_combined));
/* XXX remove this!, BUT increase the data buffer size! */
orb_set_interval(_sensor_combined_sub, 9);
#endif
/* sets also parameters in the EKF object */
parameters_update();
Vector3f lastAngRate;
Vector3f lastAccel;
/* wakeup source(s) */
struct pollfd fds[2];
/* Setup of loop */
fds[0].fd = _params_sub;
fds[0].events = POLLIN;
#ifndef SENSOR_COMBINED_SUB
fds[1].fd = _gyro_sub;
fds[1].events = POLLIN;
#else
fds[1].fd = _sensor_combined_sub;
fds[1].events = POLLIN;
#endif
bool newDataGps = false;
bool newHgtData = false;
bool newAdsData = false;
bool newDataMag = false;
float posNED[3] = {0.0f, 0.0f, 0.0f}; // North, East Down position (m)
uint64_t last_gps = 0;
_gps.vel_n_m_s = 0.0f;
_gps.vel_e_m_s = 0.0f;
_gps.vel_d_m_s = 0.0f;
while (!_task_should_exit) {
/* wait for up to 500ms for data */
int pret = poll(&fds[0], (sizeof(fds) / sizeof(fds[0])), 100);
/* timed out - periodic check for _task_should_exit, etc. */
if (pret == 0)
continue;
/* this is undesirable but not much we can do - might want to flag unhappy status */
if (pret < 0) {
warn("POLL ERR %d, %d", pret, errno);
continue;
}
perf_begin(_loop_perf);
/* only update parameters if they changed */
if (fds[0].revents & POLLIN) {
/* read from param to clear updated flag */
struct parameter_update_s update;
orb_copy(ORB_ID(parameter_update), _params_sub, &update);
/* update parameters from storage */
parameters_update();
}
/* only run estimator if gyro updated */
if (fds[1].revents & POLLIN) {
/* check vehicle status for changes to publication state */
bool prev_hil = (_vstatus.hil_state == HIL_STATE_ON);
vehicle_status_poll();
bool accel_updated;
bool mag_updated;
perf_count(_perf_gyro);
/* Reset baro reference if switching to HIL, reset sensor states */
if (!prev_hil && (_vstatus.hil_state == HIL_STATE_ON)) {
/* system is in HIL now, wait for measurements to come in one last round */
usleep(60000);
#ifndef SENSOR_COMBINED_SUB
orb_copy(ORB_ID(sensor_gyro), _gyro_sub, &_gyro);
orb_copy(ORB_ID(sensor_accel), _accel_sub, &_accel);
orb_copy(ORB_ID(sensor_mag), _mag_sub, &_mag);
#else
/* now read all sensor publications to ensure all real sensor data is purged */
orb_copy(ORB_ID(sensor_combined), _sensor_combined_sub, &_sensor_combined);
#endif
/* set sensors to de-initialized state */
_gyro_valid = false;
_accel_valid = false;
_mag_valid = false;
_baro_init = false;
_gps_initialized = false;
_last_sensor_timestamp = hrt_absolute_time();
_last_run = _last_sensor_timestamp;
_ekf->ZeroVariables();
_ekf->dtIMU = 0.01f;
_filter_start_time = _last_sensor_timestamp;
/* now skip this loop and get data on the next one, which will also re-init the filter */
continue;
}
/**
* PART ONE: COLLECT ALL DATA
**/
/* load local copies */
#ifndef SENSOR_COMBINED_SUB
orb_copy(ORB_ID(sensor_gyro), _gyro_sub, &_gyro);
orb_check(_accel_sub, &accel_updated);
if (accel_updated) {
orb_copy(ORB_ID(sensor_accel), _accel_sub, &_accel);
}
_last_sensor_timestamp = _gyro.timestamp;
IMUmsec = _gyro.timestamp / 1e3f;
float deltaT = (_gyro.timestamp - _last_run) / 1e6f;
_last_run = _gyro.timestamp;
/* guard against too large deltaT's */
if (!isfinite(deltaT) || deltaT > 1.0f || deltaT < 0.000001f) {
deltaT = 0.01f;
}
// Always store data, independent of init status
/* fill in last data set */
_ekf->dtIMU = deltaT;
if (isfinite(_gyro.x) &&
isfinite(_gyro.y) &&
isfinite(_gyro.z)) {
_ekf->angRate.x = _gyro.x;
_ekf->angRate.y = _gyro.y;
_ekf->angRate.z = _gyro.z;
if (!_gyro_valid) {
lastAngRate = _ekf->angRate;
}
_gyro_valid = true;
}
if (accel_updated) {
_ekf->accel.x = _accel.x;
_ekf->accel.y = _accel.y;
_ekf->accel.z = _accel.z;
if (!_accel_valid) {
lastAccel = _ekf->accel;
}
_accel_valid = true;
}
_ekf->dAngIMU = 0.5f * (angRate + lastAngRate) * dtIMU;
_ekf->lastAngRate = angRate;
_ekf->dVelIMU = 0.5f * (accel + lastAccel) * dtIMU;
_ekf->lastAccel = accel;
#else
orb_copy(ORB_ID(sensor_combined), _sensor_combined_sub, &_sensor_combined);
static hrt_abstime last_accel = 0;
static hrt_abstime last_mag = 0;
if (last_accel != _sensor_combined.accelerometer_timestamp) {
accel_updated = true;
} else {
accel_updated = false;
}
last_accel = _sensor_combined.accelerometer_timestamp;
// Copy gyro and accel
_last_sensor_timestamp = _sensor_combined.timestamp;
IMUmsec = _sensor_combined.timestamp / 1e3f;
float deltaT = (_sensor_combined.timestamp - _last_run) / 1e6f;
/* guard against too large deltaT's */
if (!isfinite(deltaT) || deltaT > 1.0f || deltaT < 0.000001f) {
deltaT = 0.01f;
}
_last_run = _sensor_combined.timestamp;
// Always store data, independent of init status
/* fill in last data set */
_ekf->dtIMU = deltaT;
if (isfinite(_sensor_combined.gyro_rad_s[0]) &&
isfinite(_sensor_combined.gyro_rad_s[1]) &&
isfinite(_sensor_combined.gyro_rad_s[2])) {
_ekf->angRate.x = _sensor_combined.gyro_rad_s[0];
_ekf->angRate.y = _sensor_combined.gyro_rad_s[1];
_ekf->angRate.z = _sensor_combined.gyro_rad_s[2];
if (!_gyro_valid) {
lastAngRate = _ekf->angRate;
}
_gyro_valid = true;
perf_count(_perf_gyro);
}
if (accel_updated) {
_ekf->accel.x = _sensor_combined.accelerometer_m_s2[0];
_ekf->accel.y = _sensor_combined.accelerometer_m_s2[1];
_ekf->accel.z = _sensor_combined.accelerometer_m_s2[2];
if (!_accel_valid) {
lastAccel = _ekf->accel;
}
_accel_valid = true;
}
_ekf->dAngIMU = 0.5f * (_ekf->angRate + lastAngRate) * _ekf->dtIMU;
lastAngRate = _ekf->angRate;
_ekf->dVelIMU = 0.5f * (_ekf->accel + lastAccel) * _ekf->dtIMU;
lastAccel = _ekf->accel;
if (last_mag != _sensor_combined.magnetometer_timestamp) {
mag_updated = true;
newDataMag = true;
} else {
newDataMag = false;
}
last_mag = _sensor_combined.magnetometer_timestamp;
#endif
//warnx("dang: %8.4f %8.4f dvel: %8.4f %8.4f", _ekf->dAngIMU.x, _ekf->dAngIMU.z, _ekf->dVelIMU.x, _ekf->dVelIMU.z);
bool airspeed_updated;
orb_check(_airspeed_sub, &airspeed_updated);
if (airspeed_updated) {
orb_copy(ORB_ID(airspeed), _airspeed_sub, &_airspeed);
perf_count(_perf_airspeed);
_ekf->VtasMeas = _airspeed.true_airspeed_m_s;
newAdsData = true;
} else {
newAdsData = false;
}
bool gps_updated;
orb_check(_gps_sub, &gps_updated);
if (gps_updated) {
last_gps = _gps.timestamp_position;
orb_copy(ORB_ID(vehicle_gps_position), _gps_sub, &_gps);
perf_count(_perf_gps);
if (_gps.fix_type < 3) {
newDataGps = false;
} else {
/* store time of valid GPS measurement */
_gps_start_time = hrt_absolute_time();
/* check if we had a GPS outage for a long time */
if (hrt_elapsed_time(&last_gps) > 5 * 1000 * 1000) {
_ekf->ResetPosition();
_ekf->ResetVelocity();
_ekf->ResetStoredStates();
}
/* fuse GPS updates */
//_gps.timestamp / 1e3;
_ekf->GPSstatus = _gps.fix_type;
_ekf->velNED[0] = _gps.vel_n_m_s;
_ekf->velNED[1] = _gps.vel_e_m_s;
_ekf->velNED[2] = _gps.vel_d_m_s;
// warnx("GPS updated: status: %d, vel: %8.4f %8.4f %8.4f", (int)GPSstatus, velNED[0], velNED[1], velNED[2]);
_ekf->gpsLat = math::radians(_gps.lat / (double)1e7);
_ekf->gpsLon = math::radians(_gps.lon / (double)1e7) - M_PI;
_ekf->gpsHgt = _gps.alt / 1e3f;
// if (_gps.s_variance_m_s > 0.25f && _gps.s_variance_m_s < 100.0f * 100.0f) {
// _ekf->vneSigma = sqrtf(_gps.s_variance_m_s);
// } else {
// _ekf->vneSigma = _parameters.velne_noise;
// }
// if (_gps.p_variance_m > 0.25f && _gps.p_variance_m < 100.0f * 100.0f) {
// _ekf->posNeSigma = sqrtf(_gps.p_variance_m);
// } else {
// _ekf->posNeSigma = _parameters.posne_noise;
// }
// warnx("vel: %8.4f pos: %8.4f", _gps.s_variance_m_s, _gps.p_variance_m);
newDataGps = true;
}
}
bool baro_updated;
orb_check(_baro_sub, &baro_updated);
if (baro_updated) {
orb_copy(ORB_ID(sensor_baro), _baro_sub, &_baro);
_ekf->baroHgt = _baro.altitude;
if (!_baro_init) {
_baro_ref = _baro.altitude;
_baro_init = true;
warnx("ALT REF INIT");
}
perf_count(_perf_baro);
newHgtData = true;
} else {
newHgtData = false;
}
#ifndef SENSOR_COMBINED_SUB
orb_check(_mag_sub, &mag_updated);
#endif
if (mag_updated) {
_mag_valid = true;
perf_count(_perf_mag);
#ifndef SENSOR_COMBINED_SUB
orb_copy(ORB_ID(sensor_mag), _mag_sub, &_mag);
// XXX we compensate the offsets upfront - should be close to zero.
// 0.001f
_ekf->magData.x = _mag.x;
_ekf->magBias.x = 0.000001f; // _mag_offsets.x_offset
_ekf->magData.y = _mag.y;
_ekf->magBias.y = 0.000001f; // _mag_offsets.y_offset
_ekf->magData.z = _mag.z;
_ekf->magBias.z = 0.000001f; // _mag_offsets.y_offset
#else
// XXX we compensate the offsets upfront - should be close to zero.
// 0.001f
_ekf->magData.x = _sensor_combined.magnetometer_ga[0];
_ekf->magBias.x = 0.000001f; // _mag_offsets.x_offset
_ekf->magData.y = _sensor_combined.magnetometer_ga[1];
_ekf->magBias.y = 0.000001f; // _mag_offsets.y_offset
_ekf->magData.z = _sensor_combined.magnetometer_ga[2];
_ekf->magBias.z = 0.000001f; // _mag_offsets.y_offset
#endif
newDataMag = true;
} else {
newDataMag = false;
}
/*
* CHECK IF ITS THE RIGHT TIME TO RUN THINGS ALREADY
*/
if (hrt_elapsed_time(&_filter_start_time) < FILTER_INIT_DELAY) {
continue;
}
/**
* PART TWO: EXECUTE THE FILTER
*
* We run the filter only once all data has been fetched
**/
if (_baro_init && _gyro_valid && _accel_valid && _mag_valid) {
float initVelNED[3];
/* Initialize the filter first */
if (!_gps_initialized && _gps.fix_type > 2 && _gps.eph < _parameters.pos_stddev_threshold && _gps.epv < _parameters.pos_stddev_threshold) {
// GPS is in scaled integers, convert
double lat = _gps.lat / 1.0e7;
double lon = _gps.lon / 1.0e7;
float gps_alt = _gps.alt / 1e3f;
initVelNED[0] = _gps.vel_n_m_s;
initVelNED[1] = _gps.vel_e_m_s;
initVelNED[2] = _gps.vel_d_m_s;
// Set up height correctly
orb_copy(ORB_ID(sensor_baro), _baro_sub, &_baro);
_baro_ref_offset = _ekf->states[9]; // this should become zero in the local frame
_baro_gps_offset = _baro.altitude - gps_alt;
_ekf->baroHgt = _baro.altitude;
_ekf->hgtMea = 1.0f * (_ekf->baroHgt - (_baro_ref));
// Set up position variables correctly
_ekf->GPSstatus = _gps.fix_type;
_ekf->gpsLat = math::radians(lat);
_ekf->gpsLon = math::radians(lon) - M_PI;
_ekf->gpsHgt = gps_alt;
// Look up mag declination based on current position
float declination = math::radians(get_mag_declination(lat, lon));
_ekf->InitialiseFilter(initVelNED, math::radians(lat), math::radians(lon) - M_PI, gps_alt, declination);
// Initialize projection
_local_pos.ref_lat = lat;
_local_pos.ref_lon = lon;
_local_pos.ref_alt = gps_alt;
_local_pos.ref_timestamp = _gps.timestamp_position;
map_projection_init(&_pos_ref, lat, lon);
mavlink_log_info(_mavlink_fd, "[ekf] ref: LA %.4f,LO %.4f,ALT %.2f", lat, lon, (double)gps_alt);
#if 0
warnx("HOME/REF: LA %8.4f,LO %8.4f,ALT %8.2f V: %8.4f %8.4f %8.4f", lat, lon, (double)gps_alt,
(double)_ekf->velNED[0], (double)_ekf->velNED[1], (double)_ekf->velNED[2]);
warnx("BARO: %8.4f m / ref: %8.4f m / gps offs: %8.4f m", (double)_ekf->baroHgt, (double)_baro_ref, (double)_baro_ref_offset);
warnx("GPS: eph: %8.4f, epv: %8.4f, declination: %8.4f", (double)_gps.eph, (double)_gps.epv, (double)math::degrees(declination));
#endif
_gps_initialized = true;
} else if (!_ekf->statesInitialised) {
initVelNED[0] = 0.0f;
initVelNED[1] = 0.0f;
initVelNED[2] = 0.0f;
_ekf->posNE[0] = posNED[0];
_ekf->posNE[1] = posNED[1];
_local_pos.ref_alt = _baro_ref;
_baro_ref_offset = 0.0f;
_baro_gps_offset = 0.0f;
_ekf->InitialiseFilter(initVelNED, 0.0, 0.0, 0.0f, 0.0f);
} else if (_ekf->statesInitialised) {
// We're apparently initialized in this case now
int check = check_filter_state();
if (check) {
// Let the system re-initialize itself
continue;
}
// Run the strapdown INS equations every IMU update
_ekf->UpdateStrapdownEquationsNED();
#if 0
// debug code - could be tunred into a filter mnitoring/watchdog function
float tempQuat[4];
for (uint8_t j = 0; j <= 3; j++) tempQuat[j] = states[j];
quat2eul(eulerEst, tempQuat);
for (uint8_t j = 0; j <= 2; j++) eulerDif[j] = eulerEst[j] - ahrsEul[j];
if (eulerDif[2] > pi) eulerDif[2] -= 2 * pi;
if (eulerDif[2] < -pi) eulerDif[2] += 2 * pi;
#endif
// store the predicted states for subsequent use by measurement fusion
_ekf->StoreStates(IMUmsec);
// Check if on ground - status is used by covariance prediction
_ekf->OnGroundCheck();
// sum delta angles and time used by covariance prediction
_ekf->summedDelAng = _ekf->summedDelAng + _ekf->correctedDelAng;
_ekf->summedDelVel = _ekf->summedDelVel + _ekf->dVelIMU;
dt += _ekf->dtIMU;
// perform a covariance prediction if the total delta angle has exceeded the limit
// or the time limit will be exceeded at the next IMU update
if ((dt >= (_ekf->covTimeStepMax - _ekf->dtIMU)) || (_ekf->summedDelAng.length() > _ekf->covDelAngMax)) {
_ekf->CovariancePrediction(dt);
_ekf->summedDelAng.zero();
_ekf->summedDelVel.zero();
dt = 0.0f;
}
// Fuse GPS Measurements
if (newDataGps && _gps_initialized) {
// Convert GPS measurements to Pos NE, hgt and Vel NED
float gps_dt = (_gps.timestamp_position - last_gps) / 1e6f;
// Calculate acceleration predicted by GPS velocity change
if (((fabsf(_ekf->velNED[0] - _gps.vel_n_m_s) > FLT_EPSILON) ||
(fabsf(_ekf->velNED[1] - _gps.vel_e_m_s) > FLT_EPSILON) ||
(fabsf(_ekf->velNED[2] - _gps.vel_d_m_s) > FLT_EPSILON)) && (gps_dt > 0.00001f)) {
_ekf->accelGPSNED[0] = (_ekf->velNED[0] - _gps.vel_n_m_s) / gps_dt;
_ekf->accelGPSNED[1] = (_ekf->velNED[1] - _gps.vel_e_m_s) / gps_dt;
_ekf->accelGPSNED[2] = (_ekf->velNED[2] - _gps.vel_d_m_s) / gps_dt;
}
_ekf->velNED[0] = _gps.vel_n_m_s;
_ekf->velNED[1] = _gps.vel_e_m_s;
_ekf->velNED[2] = _gps.vel_d_m_s;
_ekf->calcposNED(posNED, _ekf->gpsLat, _ekf->gpsLon, _ekf->gpsHgt, _ekf->latRef, _ekf->lonRef, _ekf->hgtRef);
_ekf->posNE[0] = posNED[0];
_ekf->posNE[1] = posNED[1];
// set fusion flags
_ekf->fuseVelData = true;
_ekf->fusePosData = true;
// recall states stored at time of measurement after adjusting for delays
_ekf->RecallStates(_ekf->statesAtVelTime, (IMUmsec - _parameters.vel_delay_ms));
_ekf->RecallStates(_ekf->statesAtPosTime, (IMUmsec - _parameters.pos_delay_ms));
// run the fusion step
_ekf->FuseVelposNED();
} else if (_ekf->statesInitialised) {
// Convert GPS measurements to Pos NE, hgt and Vel NED
_ekf->velNED[0] = 0.0f;
_ekf->velNED[1] = 0.0f;
_ekf->velNED[2] = 0.0f;
_ekf->posNE[0] = 0.0f;
_ekf->posNE[1] = 0.0f;
// set fusion flags
_ekf->fuseVelData = true;
_ekf->fusePosData = true;
// recall states stored at time of measurement after adjusting for delays
_ekf->RecallStates(_ekf->statesAtVelTime, (IMUmsec - _parameters.vel_delay_ms));
_ekf->RecallStates(_ekf->statesAtPosTime, (IMUmsec - _parameters.pos_delay_ms));
// run the fusion step
_ekf->FuseVelposNED();
} else {
_ekf->fuseVelData = false;
_ekf->fusePosData = false;
}
if (newHgtData && _ekf->statesInitialised) {
// Could use a blend of GPS and baro alt data if desired
_ekf->hgtMea = 1.0f * (_ekf->baroHgt - _baro_ref);
_ekf->fuseHgtData = true;
// recall states stored at time of measurement after adjusting for delays
_ekf->RecallStates(_ekf->statesAtHgtTime, (IMUmsec - _parameters.height_delay_ms));
// run the fusion step
_ekf->FuseVelposNED();
} else {
_ekf->fuseHgtData = false;
}
// Fuse Magnetometer Measurements
if (newDataMag && _ekf->statesInitialised) {
_ekf->fuseMagData = true;
_ekf->RecallStates(_ekf->statesAtMagMeasTime, (IMUmsec - _parameters.mag_delay_ms)); // Assume 50 msec avg delay for magnetometer data
_ekf->magstate.obsIndex = 0;
_ekf->FuseMagnetometer();
_ekf->FuseMagnetometer();
_ekf->FuseMagnetometer();
} else {
_ekf->fuseMagData = false;
}
// Fuse Airspeed Measurements
if (newAdsData && _ekf->statesInitialised && _ekf->VtasMeas > 8.0f) {
_ekf->fuseVtasData = true;
_ekf->RecallStates(_ekf->statesAtVtasMeasTime, (IMUmsec - _parameters.tas_delay_ms)); // assume 100 msec avg delay for airspeed data
_ekf->FuseAirspeed();
} else {
_ekf->fuseVtasData = false;
}
// Output results
math::Quaternion q(_ekf->states[0], _ekf->states[1], _ekf->states[2], _ekf->states[3]);
math::Matrix<3, 3> R = q.to_dcm();
math::Vector<3> euler = R.to_euler();
for (int i = 0; i < 3; i++) for (int j = 0; j < 3; j++)
_att.R[i][j] = R(i, j);
_att.timestamp = _last_sensor_timestamp;
_att.q[0] = _ekf->states[0];
_att.q[1] = _ekf->states[1];
_att.q[2] = _ekf->states[2];
_att.q[3] = _ekf->states[3];
_att.q_valid = true;
_att.R_valid = true;
_att.timestamp = _last_sensor_timestamp;
_att.roll = euler(0);
_att.pitch = euler(1);
_att.yaw = euler(2);
_att.rollspeed = _ekf->angRate.x - _ekf->states[10];
_att.pitchspeed = _ekf->angRate.y - _ekf->states[11];
_att.yawspeed = _ekf->angRate.z - _ekf->states[12];
// gyro offsets
_att.rate_offsets[0] = _ekf->states[10];
_att.rate_offsets[1] = _ekf->states[11];
_att.rate_offsets[2] = _ekf->states[12];
/* lazily publish the attitude only once available */
if (_att_pub > 0) {
/* publish the attitude setpoint */
orb_publish(ORB_ID(vehicle_attitude), _att_pub, &_att);
} else {
/* advertise and publish */
_att_pub = orb_advertise(ORB_ID(vehicle_attitude), &_att);
}
if (_gps_initialized) {
_local_pos.timestamp = _last_sensor_timestamp;
_local_pos.x = _ekf->states[7];
_local_pos.y = _ekf->states[8];
// XXX need to announce change of Z reference somehow elegantly
_local_pos.z = _ekf->states[9] - _baro_ref_offset;
_local_pos.vx = _ekf->states[4];
_local_pos.vy = _ekf->states[5];
_local_pos.vz = _ekf->states[6];
_local_pos.xy_valid = _gps_initialized;
_local_pos.z_valid = true;
_local_pos.v_xy_valid = _gps_initialized;
_local_pos.v_z_valid = true;
_local_pos.xy_global = true;
_velocity_xy_filtered = 0.95f*_velocity_xy_filtered + 0.05f*sqrtf(_local_pos.vx*_local_pos.vx + _local_pos.vy*_local_pos.vy);
_velocity_z_filtered = 0.95f*_velocity_z_filtered + 0.05f*fabsf(_local_pos.vz);
_airspeed_filtered = 0.95f*_airspeed_filtered + + 0.05f*_airspeed.true_airspeed_m_s;
/* crude land detector for fixedwing only,
* TODO: adapt so that it works for both, maybe move to another location
*/
if (_velocity_xy_filtered < 5
&& _velocity_z_filtered < 10
&& _airspeed_filtered < 10) {
_local_pos.landed = true;
} else {
_local_pos.landed = false;
}
_local_pos.z_global = false;
_local_pos.yaw = _att.yaw;
/* lazily publish the local position only once available */
if (_local_pos_pub > 0) {
/* publish the attitude setpoint */
orb_publish(ORB_ID(vehicle_local_position), _local_pos_pub, &_local_pos);
} else {
/* advertise and publish */
_local_pos_pub = orb_advertise(ORB_ID(vehicle_local_position), &_local_pos);
}
_global_pos.timestamp = _local_pos.timestamp;
if (_local_pos.xy_global) {
double est_lat, est_lon;
map_projection_reproject(&_pos_ref, _local_pos.x, _local_pos.y, &est_lat, &est_lon);
_global_pos.lat = est_lat;
_global_pos.lon = est_lon;
_global_pos.time_gps_usec = _gps.time_gps_usec;
_global_pos.eph = _gps.eph;
_global_pos.epv = _gps.epv;
}
if (_local_pos.v_xy_valid) {
_global_pos.vel_n = _local_pos.vx;
_global_pos.vel_e = _local_pos.vy;
} else {
_global_pos.vel_n = 0.0f;
_global_pos.vel_e = 0.0f;
}
/* local pos alt is negative, change sign and add alt offsets */
_global_pos.alt = _baro_ref + (-_local_pos.z) - _baro_gps_offset;
if (_local_pos.v_z_valid) {
_global_pos.vel_d = _local_pos.vz;
}
_global_pos.yaw = _local_pos.yaw;
_global_pos.eph = _gps.eph;
_global_pos.epv = _gps.epv;
_global_pos.timestamp = _local_pos.timestamp;
/* lazily publish the global position only once available */
if (_global_pos_pub > 0) {
/* publish the global position */
orb_publish(ORB_ID(vehicle_global_position), _global_pos_pub, &_global_pos);
} else {
/* advertise and publish */
_global_pos_pub = orb_advertise(ORB_ID(vehicle_global_position), &_global_pos);
}
if (hrt_elapsed_time(&_wind.timestamp) > 99000) {
_wind.timestamp = _global_pos.timestamp;
_wind.windspeed_north = _ekf->states[14];
_wind.windspeed_east = _ekf->states[15];
_wind.covariance_north = 0.0f; // XXX get form filter
_wind.covariance_east = 0.0f;
/* lazily publish the wind estimate only once available */
if (_wind_pub > 0) {
/* publish the wind estimate */
orb_publish(ORB_ID(wind_estimate), _wind_pub, &_wind);
} else {
/* advertise and publish */
_wind_pub = orb_advertise(ORB_ID(wind_estimate), &_wind);
}
}
}
}
if (hrt_elapsed_time(&_wind.timestamp) > 99000) {
_wind.timestamp = _global_pos.timestamp;
_wind.windspeed_north = _ekf->states[14];
_wind.windspeed_east = _ekf->states[15];
_wind.covariance_north = _ekf->P[14][14];
_wind.covariance_east = _ekf->P[15][15];
/* lazily publish the wind estimate only once available */
if (_wind_pub > 0) {
/* publish the wind estimate */
orb_publish(ORB_ID(wind_estimate), _wind_pub, &_wind);
} else {
/* advertise and publish */
_wind_pub = orb_advertise(ORB_ID(wind_estimate), &_wind);
}
}
}
}
perf_end(_loop_perf);
}
warnx("exiting.\n");
_estimator_task = -1;
_exit(0);
}
bool MixerTest::mixerTest()
{
/*
* PWM limit structure
*/
pwm_limit_t pwm_limit;
bool should_arm = false;
uint16_t r_page_servo_disarmed[output_max];
uint16_t r_page_servo_control_min[output_max];
uint16_t r_page_servo_control_max[output_max];
uint16_t r_page_servos[output_max];
uint16_t servo_predicted[output_max];
int16_t reverse_pwm_mask = 0;
bool load_ok = load_mixer(MIXER_PATH(IO_pass.mix), 8);
if (!load_ok) {
return load_ok;
}
/* execute the mixer */
float outputs[output_max];
unsigned mixed;
const int jmax = 5;
pwm_limit_init(&pwm_limit);
/* run through arming phase */
for (unsigned i = 0; i < output_max; i++) {
actuator_controls[i] = 0.1f;
r_page_servo_disarmed[i] = PWM_MOTOR_OFF;
r_page_servo_control_min[i] = PWM_DEFAULT_MIN;
r_page_servo_control_max[i] = PWM_DEFAULT_MAX;
}
//PX4_INFO("PRE-ARM TEST: DISABLING SAFETY");
/* mix */
should_prearm = true;
mixed = mixer_group.mix(&outputs[0], output_max);
pwm_limit_calc(should_arm, should_prearm, mixed, reverse_pwm_mask, r_page_servo_disarmed, r_page_servo_control_min,
r_page_servo_control_max, outputs, r_page_servos, &pwm_limit);
//warnx("mixed %d outputs (max %d), values:", mixed, output_max);
for (unsigned i = 0; i < mixed; i++) {
//fprintf(stderr, "pre-arm:\t %d: out: %8.4f, servo: %d \n", i, (double)outputs[i], (int)r_page_servos[i]);
if (i != actuator_controls_s::INDEX_THROTTLE) {
if (r_page_servos[i] < r_page_servo_control_min[i]) {
warnx("active servo < min");
return false;
}
} else {
if (r_page_servos[i] != r_page_servo_disarmed[i]) {
warnx("throttle output != 0 (this check assumed the IO pass mixer!)");
return false;
}
}
}
should_arm = true;
should_prearm = false;
/* simulate another orb_copy() from actuator controls */
for (unsigned i = 0; i < output_max; i++) {
actuator_controls[i] = 0.1f;
}
//PX4_INFO("ARMING TEST: STARTING RAMP");
unsigned sleep_quantum_us = 10000;
hrt_abstime starttime = hrt_absolute_time();
unsigned sleepcount = 0;
while (hrt_elapsed_time(&starttime) < INIT_TIME_US + RAMP_TIME_US + 2 * sleep_quantum_us) {
/* mix */
mixed = mixer_group.mix(&outputs[0], output_max);
pwm_limit_calc(should_arm, should_prearm, mixed, reverse_pwm_mask, r_page_servo_disarmed, r_page_servo_control_min,
r_page_servo_control_max, outputs, r_page_servos, &pwm_limit);
//warnx("mixed %d outputs (max %d), values:", mixed, output_max);
for (unsigned i = 0; i < mixed; i++) {
//fprintf(stderr, "ramp:\t %d: out: %8.4f, servo: %d \n", i, (double)outputs[i], (int)r_page_servos[i]);
/* check mixed outputs to be zero during init phase */
if (hrt_elapsed_time(&starttime) < INIT_TIME_US &&
r_page_servos[i] != r_page_servo_disarmed[i]) {
PX4_ERR("disarmed servo value mismatch: %d vs %d", r_page_servos[i], r_page_servo_disarmed[i]);
return false;
}
if (hrt_elapsed_time(&starttime) >= INIT_TIME_US &&
r_page_servos[i] + 1 <= r_page_servo_disarmed[i]) {
PX4_ERR("ramp servo value mismatch");
return false;
}
}
usleep(sleep_quantum_us);
sleepcount++;
if (sleepcount % 10 == 0) {
fflush(stdout);
}
}
//PX4_INFO("ARMING TEST: NORMAL OPERATION");
for (int j = -jmax; j <= jmax; j++) {
for (unsigned i = 0; i < output_max; i++) {
actuator_controls[i] = j / 10.0f + 0.1f * i;
r_page_servo_disarmed[i] = PWM_LOWEST_MIN;
r_page_servo_control_min[i] = PWM_DEFAULT_MIN;
r_page_servo_control_max[i] = PWM_DEFAULT_MAX;
}
/* mix */
mixed = mixer_group.mix(&outputs[0], output_max);
pwm_limit_calc(should_arm, should_prearm, mixed, reverse_pwm_mask, r_page_servo_disarmed, r_page_servo_control_min,
r_page_servo_control_max, outputs, r_page_servos, &pwm_limit);
//fprintf(stderr, "mixed %d outputs (max %d)", mixed, output_max);
for (unsigned i = 0; i < mixed; i++) {
servo_predicted[i] = 1500 + outputs[i] * (r_page_servo_control_max[i] - r_page_servo_control_min[i]) / 2.0f;
if (abs(servo_predicted[i] - r_page_servos[i]) > MIXER_DIFFERENCE_THRESHOLD) {
fprintf(stderr, "\t %d: %8.4f predicted: %d, servo: %d\n", i, (double)outputs[i], servo_predicted[i],
(int)r_page_servos[i]);
PX4_ERR("mixer violated predicted value");
return false;
}
}
}
//PX4_INFO("ARMING TEST: DISARMING");
starttime = hrt_absolute_time();
sleepcount = 0;
should_arm = false;
while (hrt_elapsed_time(&starttime) < 600000) {
/* mix */
mixed = mixer_group.mix(&outputs[0], output_max);
pwm_limit_calc(should_arm, should_prearm, mixed, reverse_pwm_mask, r_page_servo_disarmed, r_page_servo_control_min,
r_page_servo_control_max, outputs, r_page_servos, &pwm_limit);
//warnx("mixed %d outputs (max %d), values:", mixed, output_max);
for (unsigned i = 0; i < mixed; i++) {
//fprintf(stderr, "disarmed:\t %d: out: %8.4f, servo: %d \n", i, (double)outputs[i], (int)r_page_servos[i]);
/* check mixed outputs to be zero during init phase */
if (r_page_servos[i] != r_page_servo_disarmed[i]) {
PX4_ERR("disarmed servo value mismatch");
return false;
}
}
usleep(sleep_quantum_us);
sleepcount++;
if (sleepcount % 10 == 0) {
//printf(".");
//fflush(stdout);
}
}
//printf("\n");
//PX4_INFO("ARMING TEST: REARMING: STARTING RAMP");
starttime = hrt_absolute_time();
sleepcount = 0;
should_arm = true;
while (hrt_elapsed_time(&starttime) < 600000 + RAMP_TIME_US) {
/* mix */
mixed = mixer_group.mix(&outputs[0], output_max);
pwm_limit_calc(should_arm, should_prearm, mixed, reverse_pwm_mask, r_page_servo_disarmed, r_page_servo_control_min,
r_page_servo_control_max, outputs, r_page_servos, &pwm_limit);
//warnx("mixed %d outputs (max %d), values:", mixed, output_max);
for (unsigned i = 0; i < mixed; i++) {
/* predict value */
servo_predicted[i] = 1500 + outputs[i] * (r_page_servo_control_max[i] - r_page_servo_control_min[i]) / 2.0f;
/* check ramp */
//fprintf(stderr, "ramp:\t %d: out: %8.4f, servo: %d \n", i, (double)outputs[i], (int)r_page_servos[i]);
if (hrt_elapsed_time(&starttime) < RAMP_TIME_US &&
(r_page_servos[i] + 1 <= r_page_servo_disarmed[i] ||
r_page_servos[i] > servo_predicted[i])) {
PX4_ERR("ramp servo value mismatch");
return false;
}
/* check post ramp phase */
if (hrt_elapsed_time(&starttime) > RAMP_TIME_US &&
abs(servo_predicted[i] - r_page_servos[i]) > 2) {
printf("\t %d: %8.4f predicted: %d, servo: %d\n", i, (double)outputs[i], servo_predicted[i], (int)r_page_servos[i]);
PX4_ERR("mixer violated predicted value");
return false;
}
}
usleep(sleep_quantum_us);
sleepcount++;
if (sleepcount % 10 == 0) {
// printf(".");
// fflush(stdout);
}
}
return true;
}
void Tailsitter::update_transition_state()
{
if (!_flag_was_in_trans_mode) {
// save desired heading for transition and last thrust value
_yaw_transition = _v_att_sp->yaw_body;
_pitch_transition_start = _v_att_sp->pitch_body;
_throttle_transition = _v_att_sp->thrust;
_flag_was_in_trans_mode = true;
}
if (_vtol_schedule.flight_mode == TRANSITION_FRONT_P1) {
/** create time dependant pitch angle set point + 0.2 rad overlap over the switch value*/
_v_att_sp->pitch_body = _pitch_transition_start - (fabsf(PITCH_TRANSITION_FRONT_P1 - _pitch_transition_start) *
(float)hrt_elapsed_time(&_vtol_schedule.transition_start) / (_params_tailsitter.front_trans_dur * 1000000.0f));
_v_att_sp->pitch_body = math::constrain(_v_att_sp->pitch_body , PITCH_TRANSITION_FRONT_P1 - 0.2f ,
_pitch_transition_start);
/** create time dependant throttle signal higher than in MC and growing untill P2 switch speed reached */
if (_airspeed->true_airspeed_m_s <= _params_tailsitter.airspeed_trans) {
_v_att_sp->thrust = _throttle_transition + (fabsf(THROTTLE_TRANSITION_MAX * _throttle_transition) *
(float)hrt_elapsed_time(&_vtol_schedule.transition_start) / (_params_tailsitter.front_trans_dur * 1000000.0f));
_v_att_sp->thrust = math::constrain(_v_att_sp->thrust , _throttle_transition ,
(1.0f + THROTTLE_TRANSITION_MAX) * _throttle_transition);
}
// disable mc yaw control once the plane has picked up speed
if (_airspeed->true_airspeed_m_s > ARSP_YAW_CTRL_DISABLE) {
_mc_yaw_weight = 0.0f;
} else {
_mc_yaw_weight = 1.0f;
}
_mc_roll_weight = 1.0f;
_mc_pitch_weight = 1.0f;
} else if (_vtol_schedule.flight_mode == TRANSITION_FRONT_P2) {
// the plane is ready to go into fixed wing mode, smoothly switch the actuator controls, keep pitching down
/** no motor switching */
if (flag_idle_mc) {
set_idle_fw();
flag_idle_mc = false;
}
/** create time dependant pitch angle set point + 0.2 rad overlap over the switch value*/
if (_v_att_sp->pitch_body >= (PITCH_TRANSITION_FRONT_P2 - 0.2f)) {
_v_att_sp->pitch_body = PITCH_TRANSITION_FRONT_P1 -
(fabsf(PITCH_TRANSITION_FRONT_P2 - PITCH_TRANSITION_FRONT_P1) * (float)hrt_elapsed_time(
&_vtol_schedule.transition_start) / (_params_tailsitter.front_trans_dur_p2 * 1000000.0f));
if (_v_att_sp->pitch_body <= (PITCH_TRANSITION_FRONT_P2 - 0.2f)) {
_v_att_sp->pitch_body = PITCH_TRANSITION_FRONT_P2 - 0.2f;
}
}
/** start blending MC and FW controls from pitch -45 to pitch -70 for smooth control takeover*/
//_mc_roll_weight = 1.0f - 1.0f * ((float)hrt_elapsed_time(&_vtol_schedule.transition_start) / (_params_tailsitter.front_trans_dur_p2 * 1000000.0f));
//_mc_pitch_weight = 1.0f - 1.0f * ((float)hrt_elapsed_time(&_vtol_schedule.transition_start) / (_params_tailsitter.front_trans_dur_p2 * 1000000.0f));
_mc_roll_weight = 0.0f;
_mc_pitch_weight = 0.0f;
/** keep yaw disabled */
_mc_yaw_weight = 0.0f;
} else if (_vtol_schedule.flight_mode == TRANSITION_BACK) {
if (!flag_idle_mc) {
set_idle_mc();
flag_idle_mc = true;
}
/** create time dependant pitch angle set point stating at -pi/2 + 0.2 rad overlap over the switch value*/
_v_att_sp->pitch_body = M_PI_2_F + _pitch_transition_start + fabsf(PITCH_TRANSITION_BACK + 1.57f) *
(float)hrt_elapsed_time(&_vtol_schedule.transition_start) / (_params_tailsitter.back_trans_dur * 1000000.0f);
_v_att_sp->pitch_body = math::constrain(_v_att_sp->pitch_body , -2.0f , PITCH_TRANSITION_BACK + 0.2f);
// throttle value is decreesed
_v_att_sp->thrust = _throttle_transition * 0.9f;
/** keep yaw disabled */
_mc_yaw_weight = 0.0f;
/** smoothly move control weight to MC */
_mc_roll_weight = 1.0f * (float)hrt_elapsed_time(&_vtol_schedule.transition_start) /
(_params_tailsitter.back_trans_dur * 1000000.0f);
_mc_pitch_weight = 1.0f * (float)hrt_elapsed_time(&_vtol_schedule.transition_start) /
(_params_tailsitter.back_trans_dur * 1000000.0f);
}
_mc_roll_weight = math::constrain(_mc_roll_weight, 0.0f, 1.0f);
_mc_yaw_weight = math::constrain(_mc_yaw_weight, 0.0f, 1.0f);
_mc_pitch_weight = math::constrain(_mc_pitch_weight, 0.0f, 1.0f);
// compute desired attitude and thrust setpoint for the transition
_v_att_sp->timestamp = hrt_absolute_time();
_v_att_sp->roll_body = 0.0f;
_v_att_sp->yaw_body = _yaw_transition;
_v_att_sp->R_valid = true;
math::Matrix<3, 3> R_sp;
R_sp.from_euler(_v_att_sp->roll_body, _v_att_sp->pitch_body, _v_att_sp->yaw_body);
memcpy(&_v_att_sp->R_body[0], R_sp.data, sizeof(_v_att_sp->R_body));
math::Quaternion q_sp;
q_sp.from_dcm(R_sp);
memcpy(&_v_att_sp->q_d[0], &q_sp.data[0], sizeof(_v_att_sp->q_d));
}
bool MulticopterLandDetector::_has_altitude_lock()
{
return _vehicleLocalPosition.timestamp != 0 &&
hrt_elapsed_time(&_vehicleLocalPosition.timestamp) < 500_ms &&
_vehicleLocalPosition.z_valid;
}
int test_mixer(int argc, char *argv[])
{
/*
* PWM limit structure
*/
pwm_limit_t pwm_limit;
static bool should_arm = false;
uint16_t r_page_servo_disarmed[output_max];
uint16_t r_page_servo_control_min[output_max];
uint16_t r_page_servo_control_max[output_max];
uint16_t r_page_servos[output_max];
uint16_t servo_predicted[output_max];
warnx("testing mixer");
char *filename = "/etc/mixers/IO_pass.mix";
if (argc > 1)
filename = argv[1];
warnx("loading: %s", filename);
char buf[2048];
load_mixer_file(filename, &buf[0], sizeof(buf));
unsigned loaded = strlen(buf);
warnx("loaded: \n\"%s\"\n (%d chars)", &buf[0], loaded);
/* load the mixer in chunks, like
* in the case of a remote load,
* e.g. on PX4IO.
*/
unsigned nused = 0;
const unsigned chunk_size = 64;
MixerGroup mixer_group(mixer_callback, 0);
/* load at once test */
unsigned xx = loaded;
mixer_group.load_from_buf(&buf[0], xx);
warnx("complete buffer load: loaded %u mixers", mixer_group.count());
if (mixer_group.count() != 8)
return 1;
unsigned empty_load = 2;
char empty_buf[2];
empty_buf[0] = ' ';
empty_buf[1] = '\0';
mixer_group.reset();
mixer_group.load_from_buf(&empty_buf[0], empty_load);
warnx("empty buffer load: loaded %u mixers, used: %u", mixer_group.count(), empty_load);
if (empty_load != 0)
return 1;
/* FIRST mark the mixer as invalid */
bool mixer_ok = false;
/* THEN actually delete it */
mixer_group.reset();
char mixer_text[256]; /* large enough for one mixer */
unsigned mixer_text_length = 0;
unsigned transmitted = 0;
warnx("transmitted: %d, loaded: %d", transmitted, loaded);
while (transmitted < loaded) {
unsigned text_length = (loaded - transmitted > chunk_size) ? chunk_size : loaded - transmitted;
/* check for overflow - this would be really fatal */
if ((mixer_text_length + text_length + 1) > sizeof(mixer_text)) {
bool mixer_ok = false;
return 1;
}
/* append mixer text and nul-terminate */
memcpy(&mixer_text[mixer_text_length], &buf[transmitted], text_length);
mixer_text_length += text_length;
mixer_text[mixer_text_length] = '\0';
warnx("buflen %u, text:\n\"%s\"", mixer_text_length, &mixer_text[0]);
/* process the text buffer, adding new mixers as their descriptions can be parsed */
unsigned resid = mixer_text_length;
mixer_group.load_from_buf(&mixer_text[0], resid);
/* if anything was parsed */
if (resid != mixer_text_length) {
/* only set mixer ok if no residual is left over */
if (resid == 0) {
mixer_ok = true;
} else {
/* not yet reached the end of the mixer, set as not ok */
mixer_ok = false;
}
warnx("used %u", mixer_text_length - resid);
/* copy any leftover text to the base of the buffer for re-use */
if (resid > 0)
memcpy(&mixer_text[0], &mixer_text[mixer_text_length - resid], resid);
mixer_text_length = resid;
}
transmitted += text_length;
}
warnx("chunked load: loaded %u mixers", mixer_group.count());
if (mixer_group.count() != 8)
return 1;
/* execute the mixer */
float outputs[output_max];
unsigned mixed;
const int jmax = 5;
pwm_limit_init(&pwm_limit);
should_arm = true;
/* run through arming phase */
for (int i = 0; i < output_max; i++) {
actuator_controls[i] = 0.1f;
r_page_servo_disarmed[i] = PWM_LOWEST_MIN;
r_page_servo_control_min[i] = PWM_DEFAULT_MIN;
r_page_servo_control_max[i] = PWM_DEFAULT_MAX;
}
warnx("ARMING TEST: STARTING RAMP");
unsigned sleep_quantum_us = 10000;
hrt_abstime starttime = hrt_absolute_time();
unsigned sleepcount = 0;
while (hrt_elapsed_time(&starttime) < INIT_TIME_US + RAMP_TIME_US) {
/* mix */
mixed = mixer_group.mix(&outputs[0], output_max);
pwm_limit_calc(should_arm, mixed, r_page_servo_disarmed, r_page_servo_control_min, r_page_servo_control_max, outputs, r_page_servos, &pwm_limit);
//warnx("mixed %d outputs (max %d), values:", mixed, output_max);
for (int i = 0; i < mixed; i++)
{
/* check mixed outputs to be zero during init phase */
if (hrt_elapsed_time(&starttime) < INIT_TIME_US &&
r_page_servos[i] != r_page_servo_disarmed[i]) {
warnx("disarmed servo value mismatch");
return 1;
}
if (hrt_elapsed_time(&starttime) >= INIT_TIME_US &&
r_page_servos[i] + 1 <= r_page_servo_disarmed[i]) {
warnx("ramp servo value mismatch");
return 1;
}
//printf("\t %d: %8.4f limited: %8.4f, servo: %d\n", i, outputs_unlimited[i], outputs[i], (int)r_page_servos[i]);
}
usleep(sleep_quantum_us);
sleepcount++;
if (sleepcount % 10 == 0) {
printf(".");
fflush(stdout);
}
}
printf("\n");
warnx("ARMING TEST: NORMAL OPERATION");
for (int j = -jmax; j <= jmax; j++) {
for (int i = 0; i < output_max; i++) {
actuator_controls[i] = j/10.0f + 0.1f * i;
r_page_servo_disarmed[i] = PWM_LOWEST_MIN;
r_page_servo_control_min[i] = PWM_DEFAULT_MIN;
r_page_servo_control_max[i] = PWM_DEFAULT_MAX;
}
/* mix */
mixed = mixer_group.mix(&outputs[0], output_max);
pwm_limit_calc(should_arm, mixed, r_page_servo_disarmed, r_page_servo_control_min, r_page_servo_control_max, outputs, r_page_servos, &pwm_limit);
warnx("mixed %d outputs (max %d)", mixed, output_max);
for (int i = 0; i < mixed; i++)
{
servo_predicted[i] = 1500 + outputs[i] * (r_page_servo_control_max[i] - r_page_servo_control_min[i]) / 2.0f;
if (fabsf(servo_predicted[i] - r_page_servos[i]) > 2) {
printf("\t %d: %8.4f predicted: %d, servo: %d\n", i, outputs[i], servo_predicted[i], (int)r_page_servos[i]);
warnx("mixer violated predicted value");
return 1;
}
}
}
warnx("ARMING TEST: DISARMING");
starttime = hrt_absolute_time();
sleepcount = 0;
should_arm = false;
while (hrt_elapsed_time(&starttime) < 600000) {
/* mix */
mixed = mixer_group.mix(&outputs[0], output_max);
pwm_limit_calc(should_arm, mixed, r_page_servo_disarmed, r_page_servo_control_min, r_page_servo_control_max, outputs, r_page_servos, &pwm_limit);
//warnx("mixed %d outputs (max %d), values:", mixed, output_max);
for (int i = 0; i < mixed; i++)
{
/* check mixed outputs to be zero during init phase */
if (r_page_servos[i] != r_page_servo_disarmed[i]) {
warnx("disarmed servo value mismatch");
return 1;
}
//printf("\t %d: %8.4f limited: %8.4f, servo: %d\n", i, outputs_unlimited[i], outputs[i], (int)r_page_servos[i]);
}
usleep(sleep_quantum_us);
sleepcount++;
if (sleepcount % 10 == 0) {
printf(".");
fflush(stdout);
}
}
printf("\n");
warnx("ARMING TEST: REARMING: STARTING RAMP");
starttime = hrt_absolute_time();
sleepcount = 0;
should_arm = true;
while (hrt_elapsed_time(&starttime) < 600000 + RAMP_TIME_US) {
/* mix */
mixed = mixer_group.mix(&outputs[0], output_max);
pwm_limit_calc(should_arm, mixed, r_page_servo_disarmed, r_page_servo_control_min, r_page_servo_control_max, outputs, r_page_servos, &pwm_limit);
//warnx("mixed %d outputs (max %d), values:", mixed, output_max);
for (int i = 0; i < mixed; i++)
{
/* predict value */
servo_predicted[i] = 1500 + outputs[i] * (r_page_servo_control_max[i] - r_page_servo_control_min[i]) / 2.0f;
/* check ramp */
if (hrt_elapsed_time(&starttime) < RAMP_TIME_US &&
(r_page_servos[i] + 1 <= r_page_servo_disarmed[i] ||
r_page_servos[i] > servo_predicted[i])) {
warnx("ramp servo value mismatch");
return 1;
}
/* check post ramp phase */
if (hrt_elapsed_time(&starttime) > RAMP_TIME_US &&
fabsf(servo_predicted[i] - r_page_servos[i]) > 2) {
printf("\t %d: %8.4f predicted: %d, servo: %d\n", i, outputs[i], servo_predicted[i], (int)r_page_servos[i]);
warnx("mixer violated predicted value");
return 1;
}
//printf("\t %d: %8.4f limited: %8.4f, servo: %d\n", i, outputs_unlimited[i], outputs[i], (int)r_page_servos[i]);
}
usleep(sleep_quantum_us);
sleepcount++;
if (sleepcount % 10 == 0) {
printf(".");
fflush(stdout);
}
}
printf("\n");
/* load multirotor at once test */
mixer_group.reset();
if (argc > 2)
filename = argv[2];
else
filename = "/etc/mixers/FMU_quad_w.mix";
load_mixer_file(filename, &buf[0], sizeof(buf));
loaded = strlen(buf);
warnx("loaded: \n\"%s\"\n (%d chars)", &buf[0], loaded);
unsigned mc_loaded = loaded;
mixer_group.load_from_buf(&buf[0], mc_loaded);
warnx("complete buffer load: loaded %u mixers", mixer_group.count());
if (mixer_group.count() != 5) {
warnx("FAIL: Quad W mixer load failed");
return 1;
}
warnx("SUCCESS: No errors in mixer test");
}
void
Navigator::task_main()
{
/* inform about start */
warnx("Initializing..");
_mavlink_fd = open(MAVLINK_LOG_DEVICE, 0);
_geofence.setMavlinkFd(_mavlink_fd);
/* Try to load the geofence:
* if /fs/microsd/etc/geofence.txt load from this file
* else clear geofence data in datamanager */
struct stat buffer;
if (stat(GEOFENCE_FILENAME, &buffer) == 0) {
warnx("Try to load geofence.txt");
_geofence.loadFromFile(GEOFENCE_FILENAME);
} else {
mavlink_log_critical(_mavlink_fd, "#audio: No geofence file");
if (_geofence.clearDm() > 0)
warnx("Geofence cleared");
else
warnx("Could not clear geofence");
}
/* do subscriptions */
_global_pos_sub = orb_subscribe(ORB_ID(vehicle_global_position));
_gps_pos_sub = orb_subscribe(ORB_ID(vehicle_gps_position));
_sensor_combined_sub = orb_subscribe(ORB_ID(sensor_combined));
_capabilities_sub = orb_subscribe(ORB_ID(navigation_capabilities));
_vstatus_sub = orb_subscribe(ORB_ID(vehicle_status));
_control_mode_sub = orb_subscribe(ORB_ID(vehicle_control_mode));
_home_pos_sub = orb_subscribe(ORB_ID(home_position));
_onboard_mission_sub = orb_subscribe(ORB_ID(onboard_mission));
_offboard_mission_sub = orb_subscribe(ORB_ID(offboard_mission));
_param_update_sub = orb_subscribe(ORB_ID(parameter_update));
/* copy all topics first time */
vehicle_status_update();
vehicle_control_mode_update();
global_position_update();
gps_position_update();
sensor_combined_update();
home_position_update();
navigation_capabilities_update();
params_update();
/* rate limit position and sensor updates to 50 Hz */
orb_set_interval(_global_pos_sub, 20);
orb_set_interval(_sensor_combined_sub, 20);
hrt_abstime mavlink_open_time = 0;
const hrt_abstime mavlink_open_interval = 500000;
/* wakeup source(s) */
struct pollfd fds[8];
/* Setup of loop */
fds[0].fd = _global_pos_sub;
fds[0].events = POLLIN;
fds[1].fd = _home_pos_sub;
fds[1].events = POLLIN;
fds[2].fd = _capabilities_sub;
fds[2].events = POLLIN;
fds[3].fd = _vstatus_sub;
fds[3].events = POLLIN;
fds[4].fd = _control_mode_sub;
fds[4].events = POLLIN;
fds[5].fd = _param_update_sub;
fds[5].events = POLLIN;
fds[6].fd = _sensor_combined_sub;
fds[6].events = POLLIN;
fds[7].fd = _gps_pos_sub;
fds[7].events = POLLIN;
while (!_task_should_exit) {
/* wait for up to 100ms for data */
int pret = poll(&fds[0], (sizeof(fds) / sizeof(fds[0])), 100);
if (pret == 0) {
/* timed out - periodic check for _task_should_exit, etc. */
continue;
} else if (pret < 0) {
/* this is undesirable but not much we can do - might want to flag unhappy status */
warn("poll error %d, %d", pret, errno);
continue;
}
perf_begin(_loop_perf);
if (_mavlink_fd < 0 && hrt_absolute_time() > mavlink_open_time) {
/* try to reopen the mavlink log device with specified interval */
mavlink_open_time = hrt_abstime() + mavlink_open_interval;
_mavlink_fd = open(MAVLINK_LOG_DEVICE, 0);
}
static bool have_geofence_position_data = false;
/* gps updated */
if (fds[7].revents & POLLIN) {
gps_position_update();
if (_geofence.getSource() == Geofence::GF_SOURCE_GPS) {
have_geofence_position_data = true;
}
}
/* sensors combined updated */
if (fds[6].revents & POLLIN) {
sensor_combined_update();
}
/* parameters updated */
if (fds[5].revents & POLLIN) {
params_update();
updateParams();
}
/* vehicle control mode updated */
if (fds[4].revents & POLLIN) {
vehicle_control_mode_update();
}
/* vehicle status updated */
if (fds[3].revents & POLLIN) {
vehicle_status_update();
}
/* navigation capabilities updated */
if (fds[2].revents & POLLIN) {
navigation_capabilities_update();
}
/* home position updated */
if (fds[1].revents & POLLIN) {
home_position_update();
}
/* global position updated */
if (fds[0].revents & POLLIN) {
global_position_update();
if (_geofence.getSource() == Geofence::GF_SOURCE_GLOBALPOS) {
have_geofence_position_data = true;
}
}
/* Check geofence violation */
static hrt_abstime last_geofence_check = 0;
if (have_geofence_position_data && hrt_elapsed_time(&last_geofence_check) > GEOFENCE_CHECK_INTERVAL) {
bool inside = _geofence.inside(_global_pos, _gps_pos, _sensor_combined.baro_alt_meter);
last_geofence_check = hrt_absolute_time();
have_geofence_position_data = false;
if (!inside) {
/* inform other apps via the mission result */
_mission_result.geofence_violated = true;
publish_mission_result();
/* Issue a warning about the geofence violation once */
if (!_geofence_violation_warning_sent) {
mavlink_log_critical(_mavlink_fd, "#audio: Geofence violation");
_geofence_violation_warning_sent = true;
}
} else {
/* inform other apps via the mission result */
_mission_result.geofence_violated = false;
publish_mission_result();
/* Reset the _geofence_violation_warning_sent field */
_geofence_violation_warning_sent = false;
}
}
/* Do stuff according to navigation state set by commander */
switch (_vstatus.nav_state) {
case NAVIGATION_STATE_MANUAL:
case NAVIGATION_STATE_ACRO:
case NAVIGATION_STATE_ALTCTL:
case NAVIGATION_STATE_POSCTL:
case NAVIGATION_STATE_LAND:
case NAVIGATION_STATE_TERMINATION:
case NAVIGATION_STATE_OFFBOARD:
_navigation_mode = nullptr;
_can_loiter_at_sp = false;
break;
case NAVIGATION_STATE_AUTO_MISSION:
_navigation_mode = &_mission;
break;
case NAVIGATION_STATE_AUTO_LOITER:
_navigation_mode = &_loiter;
break;
case NAVIGATION_STATE_AUTO_RCRECOVER:
if (_param_rcloss_obc.get() != 0) {
_navigation_mode = &_rcLoss;
} else {
_navigation_mode = &_rtl;
}
break;
case NAVIGATION_STATE_AUTO_RTL:
_navigation_mode = &_rtl;
break;
case NAVIGATION_STATE_AUTO_RTGS:
/* Use complex data link loss mode only when enabled via param
* otherwise use rtl */
if (_param_datalinkloss_obc.get() != 0) {
_navigation_mode = &_dataLinkLoss;
} else {
_navigation_mode = &_rtl;
}
break;
case NAVIGATION_STATE_AUTO_LANDENGFAIL:
_navigation_mode = &_engineFailure;
break;
case NAVIGATION_STATE_AUTO_LANDGPSFAIL:
_navigation_mode = &_gpsFailure;
break;
default:
_navigation_mode = nullptr;
_can_loiter_at_sp = false;
break;
}
/* iterate through navigation modes and set active/inactive for each */
for(unsigned int i = 0; i < NAVIGATOR_MODE_ARRAY_SIZE; i++) {
_navigation_mode_array[i]->run(_navigation_mode == _navigation_mode_array[i]);
}
/* if nothing is running, set position setpoint triplet invalid */
if (_navigation_mode == nullptr) {
// TODO publish empty sp only once
_pos_sp_triplet.previous.valid = false;
_pos_sp_triplet.current.valid = false;
_pos_sp_triplet.next.valid = false;
_pos_sp_triplet_updated = true;
}
if (_pos_sp_triplet_updated) {
publish_position_setpoint_triplet();
_pos_sp_triplet_updated = false;
}
perf_end(_loop_perf);
}
warnx("exiting.");
_navigator_task = -1;
_exit(0);
}
void AttitudePositionEstimatorEKF::task_main()
{
_mavlink_fd = open(MAVLINK_LOG_DEVICE, 0);
_ekf = new AttPosEKF();
_filter_start_time = hrt_absolute_time();
if (!_ekf) {
errx(1, "OUT OF MEM!");
}
/*
* do subscriptions
*/
_distance_sub = orb_subscribe(ORB_ID(sensor_range_finder));
_baro_sub = orb_subscribe_multi(ORB_ID(sensor_baro), 0);
_airspeed_sub = orb_subscribe(ORB_ID(airspeed));
_gps_sub = orb_subscribe(ORB_ID(vehicle_gps_position));
_vstatus_sub = orb_subscribe(ORB_ID(vehicle_status));
_params_sub = orb_subscribe(ORB_ID(parameter_update));
_home_sub = orb_subscribe(ORB_ID(home_position));
_landDetectorSub = orb_subscribe(ORB_ID(vehicle_land_detected));
_armedSub = orb_subscribe(ORB_ID(actuator_armed));
/* rate limit vehicle status updates to 5Hz */
orb_set_interval(_vstatus_sub, 200);
_sensor_combined_sub = orb_subscribe(ORB_ID(sensor_combined));
/* XXX remove this!, BUT increase the data buffer size! */
orb_set_interval(_sensor_combined_sub, 9);
/* sets also parameters in the EKF object */
parameters_update();
/* wakeup source(s) */
struct pollfd fds[2];
/* Setup of loop */
fds[0].fd = _params_sub;
fds[0].events = POLLIN;
fds[1].fd = _sensor_combined_sub;
fds[1].events = POLLIN;
_gps.vel_n_m_s = 0.0f;
_gps.vel_e_m_s = 0.0f;
_gps.vel_d_m_s = 0.0f;
_task_running = true;
while (!_task_should_exit) {
/* wait for up to 100ms for data */
int pret = poll(&fds[0], (sizeof(fds) / sizeof(fds[0])), 100);
/* timed out - periodic check for _task_should_exit, etc. */
if (pret == 0) {
continue;
}
/* this is undesirable but not much we can do - might want to flag unhappy status */
if (pret < 0) {
warn("POLL ERR %d, %d", pret, errno);
continue;
}
perf_begin(_loop_perf);
perf_count(_loop_intvl);
/* only update parameters if they changed */
if (fds[0].revents & POLLIN) {
/* read from param to clear updated flag */
struct parameter_update_s update;
orb_copy(ORB_ID(parameter_update), _params_sub, &update);
/* update parameters from storage */
parameters_update();
}
/* only run estimator if gyro updated */
if (fds[1].revents & POLLIN) {
/* check vehicle status for changes to publication state */
bool prev_hil = (_vstatus.hil_state == vehicle_status_s::HIL_STATE_ON);
vehicle_status_poll();
perf_count(_perf_gyro);
/* Reset baro reference if switching to HIL, reset sensor states */
if (!prev_hil && (_vstatus.hil_state == vehicle_status_s::HIL_STATE_ON)) {
/* system is in HIL now, wait for measurements to come in one last round */
usleep(60000);
/* now read all sensor publications to ensure all real sensor data is purged */
orb_copy(ORB_ID(sensor_combined), _sensor_combined_sub, &_sensor_combined);
/* set sensors to de-initialized state */
_gyro_valid = false;
_accel_valid = false;
_mag_valid = false;
_baro_init = false;
_gps_initialized = false;
_last_sensor_timestamp = hrt_absolute_time();
_last_run = _last_sensor_timestamp;
_ekf->ZeroVariables();
_ekf->dtIMU = 0.01f;
_filter_start_time = _last_sensor_timestamp;
/* now skip this loop and get data on the next one, which will also re-init the filter */
continue;
}
/**
* PART ONE: COLLECT ALL DATA
**/
pollData();
/*
* CHECK IF ITS THE RIGHT TIME TO RUN THINGS ALREADY
*/
if (hrt_elapsed_time(&_filter_start_time) < FILTER_INIT_DELAY) {
continue;
}
/**
* PART TWO: EXECUTE THE FILTER
*
* We run the filter only once all data has been fetched
**/
if (_baro_init && _gyro_valid && _accel_valid && _mag_valid) {
// maintain filtered baro and gps altitudes to calculate weather offset
// baro sample rate is ~70Hz and measurement bandwidth is high
// gps sample rate is 5Hz and altitude is assumed accurate when averaged over 30 seconds
// maintain heavily filtered values for both baro and gps altitude
// Assume the filtered output should be identical for both sensors
_baro_gps_offset = _baro_alt_filt - _gps_alt_filt;
// if (hrt_elapsed_time(&_last_debug_print) >= 5e6) {
// _last_debug_print = hrt_absolute_time();
// perf_print_counter(_perf_baro);
// perf_reset(_perf_baro);
// warnx("gpsoff: %5.1f, baro_alt_filt: %6.1f, gps_alt_filt: %6.1f, gpos.alt: %5.1f, lpos.z: %6.1f",
// (double)_baro_gps_offset,
// (double)_baro_alt_filt,
// (double)_gps_alt_filt,
// (double)_global_pos.alt,
// (double)_local_pos.z);
// }
/* Initialize the filter first */
if (!_gps_initialized && _gpsIsGood) {
initializeGPS();
} else if (!_ekf->statesInitialised) {
// North, East Down position (m)
float initVelNED[3] = {0.0f, 0.0f, 0.0f};
_ekf->posNE[0] = 0.0f;
_ekf->posNE[1] = 0.0f;
_local_pos.ref_alt = _baro_ref;
_baro_ref_offset = 0.0f;
_baro_gps_offset = 0.0f;
_baro_alt_filt = _baro.altitude;
_ekf->InitialiseFilter(initVelNED, 0.0, 0.0, 0.0f, 0.0f);
} else if (_ekf->statesInitialised) {
// Check if on ground - status is used by covariance prediction
_ekf->setOnGround(_landDetector.landed);
// We're apparently initialized in this case now
// check (and reset the filter as needed)
int check = check_filter_state();
if (check) {
// Let the system re-initialize itself
continue;
}
//Run EKF data fusion steps
updateSensorFusion(_newDataGps, _newDataMag, _newRangeData, _newHgtData, _newAdsData);
//Publish attitude estimations
publishAttitude();
//Publish Local Position estimations
publishLocalPosition();
//Publish Global Position, but only if it's any good
if (_gps_initialized && (_gpsIsGood || _global_pos.dead_reckoning)) {
publishGlobalPosition();
}
//Publish wind estimates
if (hrt_elapsed_time(&_wind.timestamp) > 99000) {
publishWindEstimate();
}
}
}
}
perf_end(_loop_perf);
}
_task_running = false;
warnx("exiting.\n");
_estimator_task = -1;
_exit(0);
}
int MavlinkULog::handle_update(mavlink_channel_t channel)
{
static_assert(sizeof(ulog_stream_s::data) == MAVLINK_MSG_LOGGING_DATA_FIELD_DATA_LEN, "Invalid uorb ulog_stream.data length");
static_assert(sizeof(ulog_stream_s::data) == MAVLINK_MSG_LOGGING_DATA_ACKED_FIELD_DATA_LEN, "Invalid uorb ulog_stream.data length");
if (_waiting_for_initial_ack) {
if (hrt_elapsed_time(&_last_sent_time) > 3e5) {
PX4_WARN("no ack from logger (is it running?)");
return -1;
}
return 0;
}
// check if we're waiting for an ACK
if (_last_sent_time) {
bool check_for_updates = false;
if (_ack_received) {
_last_sent_time = 0;
check_for_updates = true;
} else {
if (hrt_elapsed_time(&_last_sent_time) > ulog_stream_ack_s::ACK_TIMEOUT * 1000) {
if (++_sent_tries > ulog_stream_ack_s::ACK_MAX_TRIES) {
return -ETIMEDOUT;
} else {
PX4_DEBUG("re-sending ulog mavlink message (try=%i)", _sent_tries);
_last_sent_time = hrt_absolute_time();
mavlink_logging_data_acked_t msg;
msg.sequence = _ulog_data.sequence;
msg.length = _ulog_data.length;
msg.first_message_offset = _ulog_data.first_message_offset;
msg.target_system = _target_system;
msg.target_component = _target_component;
memcpy(msg.data, _ulog_data.data, sizeof(msg.data));
mavlink_msg_logging_data_acked_send_struct(channel, &msg);
}
}
}
if (!check_for_updates) {
return 0;
}
}
bool updated = false;
int ret = orb_check(_ulog_stream_sub, &updated);
while (updated && !ret && _current_num_msgs < _max_num_messages) {
orb_copy(ORB_ID(ulog_stream), _ulog_stream_sub, &_ulog_data);
if (_ulog_data.flags & ulog_stream_s::FLAGS_NEED_ACK) {
_sent_tries = 1;
_last_sent_time = hrt_absolute_time();
lock();
_wait_for_ack_sequence = _ulog_data.sequence;
_ack_received = false;
unlock();
mavlink_logging_data_acked_t msg;
msg.sequence = _ulog_data.sequence;
msg.length = _ulog_data.length;
msg.first_message_offset = _ulog_data.first_message_offset;
msg.target_system = _target_system;
msg.target_component = _target_component;
memcpy(msg.data, _ulog_data.data, sizeof(msg.data));
mavlink_msg_logging_data_acked_send_struct(channel, &msg);
} else {
mavlink_logging_data_t msg;
msg.sequence = _ulog_data.sequence;
msg.length = _ulog_data.length;
msg.first_message_offset = _ulog_data.first_message_offset;
msg.target_system = _target_system;
msg.target_component = _target_component;
memcpy(msg.data, _ulog_data.data, sizeof(msg.data));
mavlink_msg_logging_data_send_struct(channel, &msg);
}
++_current_num_msgs;
ret = orb_check(_ulog_stream_sub, &updated);
}
//need to update the rate?
hrt_abstime t = hrt_absolute_time();
if (t > _next_rate_check) {
if (_current_num_msgs < _max_num_messages) {
_current_rate_factor = _max_rate_factor * (float)_current_num_msgs / _max_num_messages;
} else {
_current_rate_factor = _max_rate_factor;
}
_current_num_msgs = 0;
_next_rate_check = t + _rate_calculation_delta_t * 1.e6f;
PX4_DEBUG("current rate=%.3f (max=%i msgs in %.3fs)", (double)_current_rate_factor, _max_num_messages,
(double)_rate_calculation_delta_t);
}
return 0;
}
void AttitudePositionEstimatorEKF::publishGlobalPosition()
{
_global_pos.timestamp = _local_pos.timestamp;
if (_local_pos.xy_global) {
double est_lat, est_lon;
map_projection_reproject(&_pos_ref, _local_pos.x, _local_pos.y, &est_lat, &est_lon);
_global_pos.lat = est_lat;
_global_pos.lon = est_lon;
_global_pos.time_utc_usec = _gps.time_utc_usec;
} else {
_global_pos.lat = 0.0;
_global_pos.lon = 0.0;
_global_pos.time_utc_usec = 0;
}
if (_local_pos.v_xy_valid) {
_global_pos.vel_n = _local_pos.vx;
_global_pos.vel_e = _local_pos.vy;
} else {
_global_pos.vel_n = 0.0f;
_global_pos.vel_e = 0.0f;
}
/* local pos alt is negative, change sign and add alt offsets */
_global_pos.alt = (-_local_pos.z) - _filter_ref_offset - _baro_gps_offset;
if (_local_pos.v_z_valid) {
_global_pos.vel_d = _local_pos.vz;
} else {
_global_pos.vel_d = 0.0f;
}
/* terrain altitude */
_global_pos.terrain_alt = _ekf->hgtRef - _ekf->flowStates[1];
_global_pos.terrain_alt_valid = (_distance_last_valid > 0) &&
(hrt_elapsed_time(&_distance_last_valid) < 20 * 1000 * 1000);
_global_pos.yaw = _local_pos.yaw;
const float dtLastGoodGPS = static_cast<float>(hrt_absolute_time() - _previousGPSTimestamp) / 1e6f;
if (_gps.timestamp_position == 0 || (dtLastGoodGPS >= POS_RESET_THRESHOLD)) {
_global_pos.eph = EPH_LARGE_VALUE;
_global_pos.epv = EPV_LARGE_VALUE;
} else {
_global_pos.eph = _gps.eph;
_global_pos.epv = _gps.epv;
}
if (!isfinite(_global_pos.lat) ||
!isfinite(_global_pos.lon) ||
!isfinite(_global_pos.alt) ||
!isfinite(_global_pos.vel_n) ||
!isfinite(_global_pos.vel_e) ||
!isfinite(_global_pos.vel_d))
{
// bad data, abort publication
return;
}
/* lazily publish the global position only once available */
if (_global_pos_pub > 0) {
/* publish the global position */
orb_publish(ORB_ID(vehicle_global_position), _global_pos_pub, &_global_pos);
} else {
/* advertise and publish */
_global_pos_pub = orb_advertise(ORB_ID(vehicle_global_position), &_global_pos);
}
}
void AttitudePositionEstimatorEKF::pollData()
{
//Update arming status
bool armedUpdate;
orb_check(_armedSub, &armedUpdate);
if (armedUpdate) {
orb_copy(ORB_ID(actuator_armed), _armedSub, &_armed);
}
//Update Gyro and Accelerometer
static Vector3f lastAngRate;
static Vector3f lastAccel;
bool accel_updated = false;
orb_copy(ORB_ID(sensor_combined), _sensor_combined_sub, &_sensor_combined);
static hrt_abstime last_accel = 0;
static hrt_abstime last_mag = 0;
if (last_accel != _sensor_combined.accelerometer_timestamp) {
accel_updated = true;
} else {
accel_updated = false;
}
last_accel = _sensor_combined.accelerometer_timestamp;
// Copy gyro and accel
_last_sensor_timestamp = _sensor_combined.timestamp;
IMUmsec = _sensor_combined.timestamp / 1e3;
IMUusec = _sensor_combined.timestamp;
float deltaT = (_sensor_combined.timestamp - _last_run) / 1e6f;
/* guard against too large deltaT's */
if (!isfinite(deltaT) || deltaT > 1.0f || deltaT < 0.000001f) {
deltaT = 0.01f;
}
_last_run = _sensor_combined.timestamp;
// Always store data, independent of init status
/* fill in last data set */
_ekf->dtIMU = deltaT;
int last_gyro_main = _gyro_main;
if (isfinite(_sensor_combined.gyro_rad_s[0]) &&
isfinite(_sensor_combined.gyro_rad_s[1]) &&
isfinite(_sensor_combined.gyro_rad_s[2]) &&
(_sensor_combined.gyro_errcount <= (_sensor_combined.gyro1_errcount + GYRO_SWITCH_HYSTERESIS))) {
_ekf->angRate.x = _sensor_combined.gyro_rad_s[0];
_ekf->angRate.y = _sensor_combined.gyro_rad_s[1];
_ekf->angRate.z = _sensor_combined.gyro_rad_s[2];
_gyro_main = 0;
_gyro_valid = true;
} else if (isfinite(_sensor_combined.gyro1_rad_s[0]) &&
isfinite(_sensor_combined.gyro1_rad_s[1]) &&
isfinite(_sensor_combined.gyro1_rad_s[2])) {
_ekf->angRate.x = _sensor_combined.gyro1_rad_s[0];
_ekf->angRate.y = _sensor_combined.gyro1_rad_s[1];
_ekf->angRate.z = _sensor_combined.gyro1_rad_s[2];
_gyro_main = 1;
_gyro_valid = true;
} else {
_gyro_valid = false;
}
if (last_gyro_main != _gyro_main) {
mavlink_and_console_log_emergency(_mavlink_fd, "GYRO FAILED! Switched from #%d to %d", last_gyro_main, _gyro_main);
}
if (!_gyro_valid) {
/* keep last value if he hit an out of band value */
lastAngRate = _ekf->angRate;
} else {
perf_count(_perf_gyro);
}
if (accel_updated) {
int last_accel_main = _accel_main;
/* fail over to the 2nd accel if we know the first is down */
if (_sensor_combined.accelerometer_errcount <= (_sensor_combined.accelerometer1_errcount + ACCEL_SWITCH_HYSTERESIS)) {
_ekf->accel.x = _sensor_combined.accelerometer_m_s2[0];
_ekf->accel.y = _sensor_combined.accelerometer_m_s2[1];
_ekf->accel.z = _sensor_combined.accelerometer_m_s2[2];
_accel_main = 0;
} else {
_ekf->accel.x = _sensor_combined.accelerometer1_m_s2[0];
_ekf->accel.y = _sensor_combined.accelerometer1_m_s2[1];
_ekf->accel.z = _sensor_combined.accelerometer1_m_s2[2];
_accel_main = 1;
}
if (!_accel_valid) {
lastAccel = _ekf->accel;
}
if (last_accel_main != _accel_main) {
mavlink_and_console_log_emergency(_mavlink_fd, "ACCEL FAILED! Switched from #%d to %d", last_accel_main, _accel_main);
}
_accel_valid = true;
}
_ekf->dAngIMU = 0.5f * (_ekf->angRate + lastAngRate) * _ekf->dtIMU;
lastAngRate = _ekf->angRate;
_ekf->dVelIMU = 0.5f * (_ekf->accel + lastAccel) * _ekf->dtIMU;
lastAccel = _ekf->accel;
if (last_mag != _sensor_combined.magnetometer_timestamp) {
_newDataMag = true;
} else {
_newDataMag = false;
}
last_mag = _sensor_combined.magnetometer_timestamp;
//warnx("dang: %8.4f %8.4f dvel: %8.4f %8.4f", _ekf->dAngIMU.x, _ekf->dAngIMU.z, _ekf->dVelIMU.x, _ekf->dVelIMU.z);
//Update Land Detector
bool newLandData;
orb_check(_landDetectorSub, &newLandData);
if (newLandData) {
orb_copy(ORB_ID(vehicle_land_detected), _landDetectorSub, &_landDetector);
}
//Update AirSpeed
orb_check(_airspeed_sub, &_newAdsData);
if (_newAdsData) {
orb_copy(ORB_ID(airspeed), _airspeed_sub, &_airspeed);
perf_count(_perf_airspeed);
_ekf->VtasMeas = _airspeed.true_airspeed_unfiltered_m_s;
}
bool gps_update;
orb_check(_gps_sub, &gps_update);
if (gps_update) {
orb_copy(ORB_ID(vehicle_gps_position), _gps_sub, &_gps);
perf_count(_perf_gps);
//We are more strict for our first fix
float requiredAccuracy = _parameters.pos_stddev_threshold;
if (_gpsIsGood) {
requiredAccuracy = _parameters.pos_stddev_threshold * 2.0f;
}
//Check if the GPS fix is good enough for us to use
if (_gps.fix_type >= 3 && _gps.eph < requiredAccuracy && _gps.epv < requiredAccuracy) {
_gpsIsGood = true;
} else {
_gpsIsGood = false;
}
if (_gpsIsGood) {
//Calculate time since last good GPS fix
const float dtLastGoodGPS = static_cast<float>(_gps.timestamp_position - _previousGPSTimestamp) / 1e6f;
//Stop dead-reckoning mode
if (_global_pos.dead_reckoning) {
mavlink_log_info(_mavlink_fd, "[ekf] stop dead-reckoning");
}
_global_pos.dead_reckoning = false;
//Fetch new GPS data
_ekf->GPSstatus = _gps.fix_type;
_ekf->velNED[0] = _gps.vel_n_m_s;
_ekf->velNED[1] = _gps.vel_e_m_s;
_ekf->velNED[2] = _gps.vel_d_m_s;
_ekf->gpsLat = math::radians(_gps.lat / (double)1e7);
_ekf->gpsLon = math::radians(_gps.lon / (double)1e7) - M_PI;
_ekf->gpsHgt = _gps.alt / 1e3f;
if (_previousGPSTimestamp != 0) {
//Calculate average time between GPS updates
_ekf->updateDtGpsFilt(math::constrain(dtLastGoodGPS, 0.01f, POS_RESET_THRESHOLD));
// update LPF
float filter_step = (dtLastGoodGPS / (rc + dtLastGoodGPS)) * (_ekf->gpsHgt - _gps_alt_filt);
if (isfinite(filter_step)) {
_gps_alt_filt += filter_step;
}
}
//check if we had a GPS outage for a long time
if (_gps_initialized) {
//Convert from global frame to local frame
map_projection_project(&_pos_ref, (_gps.lat / 1.0e7), (_gps.lon / 1.0e7), &_ekf->posNE[0], &_ekf->posNE[1]);
if (dtLastGoodGPS > POS_RESET_THRESHOLD) {
_ekf->ResetPosition();
_ekf->ResetVelocity();
}
}
//warnx("gps alt: %6.1f, interval: %6.3f", (double)_ekf->gpsHgt, (double)dtGoodGPS);
// if (_gps.s_variance_m_s > 0.25f && _gps.s_variance_m_s < 100.0f * 100.0f) {
// _ekf->vneSigma = sqrtf(_gps.s_variance_m_s);
// } else {
// _ekf->vneSigma = _parameters.velne_noise;
// }
// if (_gps.p_variance_m > 0.25f && _gps.p_variance_m < 100.0f * 100.0f) {
// _ekf->posNeSigma = sqrtf(_gps.p_variance_m);
// } else {
// _ekf->posNeSigma = _parameters.posne_noise;
// }
// warnx("vel: %8.4f pos: %8.4f", _gps.s_variance_m_s, _gps.p_variance_m);
_previousGPSTimestamp = _gps.timestamp_position;
}
}
// If it has gone more than POS_RESET_THRESHOLD amount of seconds since we received a GPS update,
// then something is very wrong with the GPS (possibly a hardware failure or comlink error)
const float dtLastGoodGPS = static_cast<float>(hrt_absolute_time() - _previousGPSTimestamp) / 1e6f;
if (dtLastGoodGPS >= POS_RESET_THRESHOLD) {
if (_global_pos.dead_reckoning) {
mavlink_log_info(_mavlink_fd, "[ekf] gave up dead-reckoning after long timeout");
}
_gpsIsGood = false;
_global_pos.dead_reckoning = false;
}
//If we have no good GPS fix for half a second, then enable dead-reckoning mode while armed (for up to POS_RESET_THRESHOLD seconds)
else if (dtLastGoodGPS >= 0.5f) {
if (_armed.armed) {
if (!_global_pos.dead_reckoning) {
mavlink_log_info(_mavlink_fd, "[ekf] dead-reckoning enabled");
}
_global_pos.dead_reckoning = true;
} else {
_global_pos.dead_reckoning = false;
}
}
//Update barometer
orb_check(_baro_sub, &_newHgtData);
if (_newHgtData) {
static hrt_abstime baro_last = 0;
orb_copy(ORB_ID(sensor_baro), _baro_sub, &_baro);
// init lowpass filters for baro and gps altitude
float baro_elapsed;
if (baro_last == 0) {
baro_elapsed = 0.0f;
} else {
baro_elapsed = (_baro.timestamp - baro_last) / 1e6f;
}
baro_last = _baro.timestamp;
if (!_baro_init) {
_baro_init = true;
_baro_alt_filt = _baro.altitude;
}
_ekf->updateDtHgtFilt(math::constrain(baro_elapsed, 0.001f, 0.1f));
_ekf->baroHgt = _baro.altitude;
float filter_step = (baro_elapsed / (rc + baro_elapsed)) * (_baro.altitude - _baro_alt_filt);
if (isfinite(filter_step)) {
_baro_alt_filt += filter_step;
}
perf_count(_perf_baro);
}
//Update Magnetometer
if (_newDataMag) {
_mag_valid = true;
perf_count(_perf_mag);
int last_mag_main = _mag_main;
Vector3f mag0(_sensor_combined.magnetometer_ga[0], _sensor_combined.magnetometer_ga[1],
_sensor_combined.magnetometer_ga[2]);
Vector3f mag1(_sensor_combined.magnetometer1_ga[0], _sensor_combined.magnetometer1_ga[1],
_sensor_combined.magnetometer1_ga[2]);
const unsigned mag_timeout_us = 200000;
/* fail over to the 2nd mag if we know the first is down */
if (hrt_elapsed_time(&_sensor_combined.magnetometer_timestamp) < mag_timeout_us &&
_sensor_combined.magnetometer_errcount <= (_sensor_combined.magnetometer1_errcount + MAG_SWITCH_HYSTERESIS) &&
mag0.length() > 0.1f) {
_ekf->magData.x = mag0.x;
_ekf->magBias.x = 0.000001f; // _mag_offsets.x_offset
_ekf->magData.y = mag0.y;
_ekf->magBias.y = 0.000001f; // _mag_offsets.y_offset
_ekf->magData.z = mag0.z;
_ekf->magBias.z = 0.000001f; // _mag_offsets.y_offset
_mag_main = 0;
} else if (hrt_elapsed_time(&_sensor_combined.magnetometer1_timestamp) < mag_timeout_us &&
mag1.length() > 0.1f) {
_ekf->magData.x = mag1.x;
_ekf->magBias.x = 0.000001f; // _mag_offsets.x_offset
_ekf->magData.y = mag1.y;
_ekf->magBias.y = 0.000001f; // _mag_offsets.y_offset
_ekf->magData.z = mag1.z;
_ekf->magBias.z = 0.000001f; // _mag_offsets.y_offset
_mag_main = 1;
} else {
_mag_valid = false;
}
if (last_mag_main != _mag_main) {
mavlink_and_console_log_emergency(_mavlink_fd, "MAG FAILED! Failover from unit %d to unit %d", last_mag_main, _mag_main);
}
}
//Update range data
orb_check(_distance_sub, &_newRangeData);
if (_newRangeData) {
orb_copy(ORB_ID(sensor_range_finder), _distance_sub, &_distance);
if (_distance.valid) {
_ekf->rngMea = _distance.distance;
_distance_last_valid = _distance.timestamp;
} else {
_newRangeData = false;
}
}
}
int uORBTest::UnitTest::pubsublatency_main(void)
{
/* poll on test topic and output latency */
float latency_integral = 0.0f;
/* wakeup source(s) */
px4_pollfd_struct_t fds[3];
int test_multi_sub = orb_subscribe_multi(ORB_ID(orb_test), 0);
int test_multi_sub_medium = orb_subscribe_multi(ORB_ID(orb_test_medium), 0);
int test_multi_sub_large = orb_subscribe_multi(ORB_ID(orb_test_large), 0);
struct orb_test_large t;
/* clear all ready flags */
orb_copy(ORB_ID(orb_test), test_multi_sub, &t);
orb_copy(ORB_ID(orb_test_medium), test_multi_sub_medium, &t);
orb_copy(ORB_ID(orb_test_large), test_multi_sub_large, &t);
fds[0].fd = test_multi_sub;
fds[0].events = POLLIN;
fds[1].fd = test_multi_sub_medium;
fds[1].events = POLLIN;
fds[2].fd = test_multi_sub_large;
fds[2].events = POLLIN;
const unsigned maxruns = 1000;
unsigned timingsgroup = 0;
unsigned *timings = new unsigned[maxruns];
for (unsigned i = 0; i < maxruns; i++) {
/* wait for up to 500ms for data */
int pret = px4_poll(&fds[0], (sizeof(fds) / sizeof(fds[0])), 500);
if (fds[0].revents & POLLIN) {
orb_copy(ORB_ID(orb_test), test_multi_sub, &t);
timingsgroup = 0;
} else if (fds[1].revents & POLLIN) {
orb_copy(ORB_ID(orb_test_medium), test_multi_sub_medium, &t);
timingsgroup = 1;
} else if (fds[2].revents & POLLIN) {
orb_copy(ORB_ID(orb_test_large), test_multi_sub_large, &t);
timingsgroup = 2;
}
if (pret < 0) {
warn("poll error %d, %d", pret, errno);
continue;
}
hrt_abstime elt = hrt_elapsed_time(&t.time);
latency_integral += elt;
timings[i] = elt;
}
orb_unsubscribe(test_multi_sub);
orb_unsubscribe(test_multi_sub_medium);
orb_unsubscribe(test_multi_sub_large);
if (pubsubtest_print) {
char fname[32];
sprintf(fname, PX4_ROOTFSDIR"/fs/microsd/timings%u.txt", timingsgroup);
FILE *f = fopen(fname, "w");
if (f == NULL) {
warnx("Error opening file!\n");
return uORB::ERROR;
}
for (unsigned i = 0; i < maxruns; i++) {
fprintf(f, "%u\n", timings[i]);
}
fclose(f);
}
delete[] timings;
warnx("mean: %8.4f us", static_cast<double>(latency_integral / maxruns));
pubsubtest_passed = true;
if (static_cast<float>(latency_integral / maxruns) > 30.0f) {
pubsubtest_res = uORB::ERROR;
} else {
pubsubtest_res = PX4_OK;
}
return pubsubtest_res;
}
void Standard::update_vtol_state()
{
parameters_update();
/* After flipping the switch the vehicle will start the pusher (or tractor) motor, picking up
* forward speed. After the vehicle has picked up enough speed the rotors shutdown.
* For the back transition the pusher motor is immediately stopped and rotors reactivated.
*/
if (!_attc->is_fixed_wing_requested()) {
// the transition to fw mode switch is off
if (_vtol_schedule.flight_mode == MC_MODE) {
// in mc mode
_vtol_schedule.flight_mode = MC_MODE;
_mc_roll_weight = 1.0f;
_mc_pitch_weight = 1.0f;
_mc_yaw_weight = 1.0f;
_mc_throttle_weight = 1.0f;
} else if (_vtol_schedule.flight_mode == FW_MODE) {
// transition to mc mode
_vtol_schedule.flight_mode = TRANSITION_TO_MC;
_flag_enable_mc_motors = true;
_vtol_schedule.transition_start = hrt_absolute_time();
} else if (_vtol_schedule.flight_mode == TRANSITION_TO_FW) {
// failsafe back to mc mode
_vtol_schedule.flight_mode = MC_MODE;
_mc_roll_weight = 1.0f;
_mc_pitch_weight = 1.0f;
_mc_yaw_weight = 1.0f;
_mc_throttle_weight = 1.0f;
} else if (_vtol_schedule.flight_mode == TRANSITION_TO_MC) {
// transition to MC mode if transition time has passed
if (hrt_elapsed_time(&_vtol_schedule.transition_start) >
(_params_standard.back_trans_dur * 1000000.0f)) {
_vtol_schedule.flight_mode = MC_MODE;
}
}
// the pusher motor should never be powered when in or transitioning to mc mode
_pusher_throttle = 0.0f;
} else {
// the transition to fw mode switch is on
if (_vtol_schedule.flight_mode == MC_MODE) {
// start transition to fw mode
_vtol_schedule.flight_mode = TRANSITION_TO_FW;
_vtol_schedule.transition_start = hrt_absolute_time();
} else if (_vtol_schedule.flight_mode == FW_MODE) {
// in fw mode
_vtol_schedule.flight_mode = FW_MODE;
_mc_roll_weight = 0.0f;
_mc_pitch_weight = 0.0f;
_mc_yaw_weight = 0.0f;
_mc_throttle_weight = 0.0f;
} else if (_vtol_schedule.flight_mode == TRANSITION_TO_FW) {
// continue the transition to fw mode while monitoring airspeed for a final switch to fw mode
if (_airspeed->true_airspeed_m_s >= _params_standard.airspeed_trans || !_armed->armed) {
_vtol_schedule.flight_mode = FW_MODE;
// we can turn off the multirotor motors now
_flag_enable_mc_motors = false;
// don't set pusher throttle here as it's being ramped up elsewhere
}
} else if (_vtol_schedule.flight_mode == TRANSITION_TO_MC) {
// transitioning to mc mode & transition switch on - failsafe back into fw mode
_vtol_schedule.flight_mode = FW_MODE;
}
}
// map specific control phases to simple control modes
switch (_vtol_schedule.flight_mode) {
case MC_MODE:
_vtol_mode = ROTARY_WING;
break;
case FW_MODE:
_vtol_mode = FIXED_WING;
break;
case TRANSITION_TO_FW:
case TRANSITION_TO_MC:
_vtol_mode = TRANSITION;
break;
}
}
void
mixer_tick(void)
{
/* check that we are receiving fresh data from the FMU */
if (hrt_elapsed_time(&system_state.fmu_data_received_time) > FMU_INPUT_DROP_LIMIT_US) {
/* too long without FMU input, time to go to failsafe */
if (r_status_flags & PX4IO_P_STATUS_FLAGS_FMU_OK) {
isr_debug(1, "AP RX timeout");
}
r_status_flags &= ~(PX4IO_P_STATUS_FLAGS_FMU_OK | PX4IO_P_STATUS_FLAGS_RAW_PWM);
r_status_alarms |= PX4IO_P_STATUS_ALARMS_FMU_LOST;
} else {
r_status_flags |= PX4IO_P_STATUS_FLAGS_FMU_OK;
r_status_alarms &= ~PX4IO_P_STATUS_ALARMS_FMU_LOST;
}
source = MIX_FAILSAFE;
/*
* Decide which set of controls we're using.
*/
if ((r_status_flags & PX4IO_P_STATUS_FLAGS_RAW_PWM) ||
!(r_status_flags & PX4IO_P_STATUS_FLAGS_MIXER_OK)) {
/* don't actually mix anything - we already have raw PWM values or
not a valid mixer. */
source = MIX_NONE;
} else {
if (!(r_status_flags & PX4IO_P_STATUS_FLAGS_OVERRIDE) &&
(r_status_flags & PX4IO_P_STATUS_FLAGS_MIXER_OK)) {
/* mix from FMU controls */
source = MIX_FMU;
}
if ( (r_status_flags & PX4IO_P_STATUS_FLAGS_OVERRIDE) &&
(r_status_flags & PX4IO_P_STATUS_FLAGS_RC_OK) &&
(r_status_flags & PX4IO_P_STATUS_FLAGS_MIXER_OK)) {
/* if allowed, mix from RC inputs directly */
source = MIX_OVERRIDE;
}
}
/*
* Run the mixers.
*/
if (source == MIX_FAILSAFE) {
/* copy failsafe values to the servo outputs */
for (unsigned i = 0; i < IO_SERVO_COUNT; i++)
r_page_servos[i] = r_page_servo_failsafe[i];
} else if (source != MIX_NONE) {
float outputs[IO_SERVO_COUNT];
unsigned mixed;
/* mix */
mixed = mixer_group.mix(&outputs[0], IO_SERVO_COUNT);
/* scale to PWM and update the servo outputs as required */
for (unsigned i = 0; i < mixed; i++) {
/* save actuator values for FMU readback */
r_page_actuators[i] = FLOAT_TO_REG(outputs[i]);
/* scale to servo output */
r_page_servos[i] = (outputs[i] * 500.0f) + 1500;
}
for (unsigned i = mixed; i < IO_SERVO_COUNT; i++)
r_page_servos[i] = 0;
}
/*
* Decide whether the servos should be armed right now.
*
* We must be armed, and we must have a PWM source; either raw from
* FMU or from the mixer.
*
* XXX correct behaviour for failsafe may require an additional case
* here.
*/
bool should_arm = (
/* FMU is armed */ (r_setup_arming & PX4IO_P_SETUP_ARMING_FMU_ARMED) &&
/* IO is armed */ (r_status_flags & PX4IO_P_STATUS_FLAGS_ARMED) &&
/* there is valid input */ (r_status_flags & (PX4IO_P_STATUS_FLAGS_RAW_PWM | PX4IO_P_STATUS_FLAGS_MIXER_OK)) &&
/* IO initialised without error */ (r_status_flags & PX4IO_P_STATUS_FLAGS_INIT_OK) &&
/* FMU is available or FMU is not available but override is an option */
((r_status_flags & PX4IO_P_STATUS_FLAGS_FMU_OK) || (!(r_status_flags & PX4IO_P_STATUS_FLAGS_FMU_OK) && (r_setup_arming & PX4IO_P_SETUP_ARMING_MANUAL_OVERRIDE_OK) ))
);
if (should_arm && !mixer_servos_armed) {
/* need to arm, but not armed */
up_pwm_servo_arm(true);
mixer_servos_armed = true;
} else if (!should_arm && mixer_servos_armed) {
/* armed but need to disarm */
up_pwm_servo_arm(false);
mixer_servos_armed = false;
}
if (mixer_servos_armed) {
/* update the servo outputs. */
for (unsigned i = 0; i < IO_SERVO_COUNT; i++)
up_pwm_servo_set(i, r_page_servos[i]);
}
}
void Standard::update_transition_state()
{
// copy virtual attitude setpoint to real attitude setpoint
memcpy(_v_att_sp, _mc_virtual_att_sp, sizeof(vehicle_attitude_setpoint_s));
if (_vtol_schedule.flight_mode == TRANSITION_TO_FW) {
if (_params_standard.front_trans_dur <= 0.0f) {
// just set the final target throttle value
_pusher_throttle = _params_standard.pusher_trans;
} else if (_pusher_throttle <= _params_standard.pusher_trans) {
// ramp up throttle to the target throttle value
_pusher_throttle = _params_standard.pusher_trans *
(float)hrt_elapsed_time(&_vtol_schedule.transition_start) / (_params_standard.front_trans_dur * 1000000.0f);
}
// do blending of mc and fw controls if a blending airspeed has been provided
if (_airspeed_trans_blend_margin > 0.0f && _airspeed->true_airspeed_m_s >= _params_standard.airspeed_blend) {
float weight = 1.0f - fabsf(_airspeed->true_airspeed_m_s - _params_standard.airspeed_blend) /
_airspeed_trans_blend_margin;
_mc_roll_weight = weight;
_mc_pitch_weight = weight;
_mc_yaw_weight = weight;
_mc_throttle_weight = weight;
} else {
// at low speeds give full weight to mc
_mc_roll_weight = 1.0f;
_mc_pitch_weight = 1.0f;
_mc_yaw_weight = 1.0f;
_mc_throttle_weight = 1.0f;
}
// check front transition timeout
if (_params_standard.front_trans_timeout > FLT_EPSILON) {
if ( (float)hrt_elapsed_time(&_vtol_schedule.transition_start) > (_params_standard.front_trans_timeout * 1000000.0f)) {
// transition timeout occured, abort transition
_attc->abort_front_transition();
}
}
} else if (_vtol_schedule.flight_mode == TRANSITION_TO_MC) {
// continually increase mc attitude control as we transition back to mc mode
if (_params_standard.back_trans_dur > 0.0f) {
float weight = (float)hrt_elapsed_time(&_vtol_schedule.transition_start) / (_params_standard.back_trans_dur *
1000000.0f);
_mc_roll_weight = weight;
_mc_pitch_weight = weight;
_mc_yaw_weight = weight;
_mc_throttle_weight = weight;
} else {
_mc_roll_weight = 1.0f;
_mc_pitch_weight = 1.0f;
_mc_yaw_weight = 1.0f;
_mc_throttle_weight = 1.0f;
}
// in fw mode we need the multirotor motors to stop spinning, in backtransition mode we let them spin up again
if (_flag_enable_mc_motors) {
set_max_mc(2000);
set_idle_mc();
_flag_enable_mc_motors = false;
}
}
_mc_roll_weight = math::constrain(_mc_roll_weight, 0.0f, 1.0f);
_mc_pitch_weight = math::constrain(_mc_pitch_weight, 0.0f, 1.0f);
_mc_yaw_weight = math::constrain(_mc_yaw_weight, 0.0f, 1.0f);
_mc_throttle_weight = math::constrain(_mc_throttle_weight, 0.0f, 1.0f);
}
void
MavlinkMissionManager::send(const hrt_abstime now)
{
bool updated = false;
orb_check(_mission_result_sub, &updated);
if (updated) {
mission_result_s mission_result;
orb_copy(ORB_ID(mission_result), _mission_result_sub, &mission_result);
_current_seq = mission_result.seq_current;
if (_verbose) { warnx("WPM: got mission result, new current_seq: %d", _current_seq); }
if (mission_result.reached) {
_last_reached = mission_result.seq_reached;
send_mission_item_reached((uint16_t)mission_result.seq_reached);
} else {
_last_reached = -1;
}
send_mission_current(_current_seq);
if (mission_result.item_do_jump_changed) {
/* send a mission item again if the remaining DO_JUMPs has changed */
send_mission_item(_transfer_partner_sysid, _transfer_partner_compid,
(uint16_t)mission_result.item_changed_index);
}
} else {
if (_slow_rate_limiter.check(now)) {
send_mission_current(_current_seq);
if (_last_reached >= 0) {
send_mission_item_reached((uint16_t)_last_reached);
}
}
}
/* check for timed-out operations */
if (_state != MAVLINK_WPM_STATE_IDLE && hrt_elapsed_time(&_time_last_recv) > _action_timeout) {
_mavlink->send_statustext_critical("Operation timeout");
if (_verbose) { warnx("WPM: Last operation (state=%u) timed out, changing state to MAVLINK_WPM_STATE_IDLE", _state); }
_state = MAVLINK_WPM_STATE_IDLE;
// since we are giving up, reset this state also, so another request can be started.
_transfer_in_progress = false;
} else if (_state == MAVLINK_WPM_STATE_GETLIST && hrt_elapsed_time(&_time_last_sent) > _retry_timeout) {
/* try to request item again after timeout,
* toggle int32 or float protocol variant to try both */
_int_mode = !_int_mode;
send_mission_request(_transfer_partner_sysid, _transfer_partner_compid, _transfer_seq);
} else if (_state == MAVLINK_WPM_STATE_SENDLIST && hrt_elapsed_time(&_time_last_sent) > _retry_timeout) {
if (_transfer_seq == 0) {
/* try to send items count again after timeout */
send_mission_count(_transfer_partner_sysid, _transfer_partner_compid, _transfer_count);
} else {
/* try to send item again after timeout */
send_mission_item(_transfer_partner_sysid, _transfer_partner_compid, _transfer_seq - 1);
}
}
}
void
Navigator::task_main()
{
bool have_geofence_position_data = false;
/* Try to load the geofence:
* if /fs/microsd/etc/geofence.txt load from this file */
struct stat buffer;
if (stat(GEOFENCE_FILENAME, &buffer) == 0) {
PX4_INFO("Loading geofence from %s", GEOFENCE_FILENAME);
_geofence.loadFromFile(GEOFENCE_FILENAME);
}
/* do subscriptions */
_global_pos_sub = orb_subscribe(ORB_ID(vehicle_global_position));
_local_pos_sub = orb_subscribe(ORB_ID(vehicle_local_position));
_gps_pos_sub = orb_subscribe(ORB_ID(vehicle_gps_position));
_sensor_combined_sub = orb_subscribe(ORB_ID(sensor_combined));
_fw_pos_ctrl_status_sub = orb_subscribe(ORB_ID(fw_pos_ctrl_status));
_vstatus_sub = orb_subscribe(ORB_ID(vehicle_status));
_land_detected_sub = orb_subscribe(ORB_ID(vehicle_land_detected));
_home_pos_sub = orb_subscribe(ORB_ID(home_position));
_onboard_mission_sub = orb_subscribe(ORB_ID(onboard_mission));
_offboard_mission_sub = orb_subscribe(ORB_ID(offboard_mission));
_param_update_sub = orb_subscribe(ORB_ID(parameter_update));
_vehicle_command_sub = orb_subscribe(ORB_ID(vehicle_command));
_traffic_sub = orb_subscribe(ORB_ID(transponder_report));
/* copy all topics first time */
vehicle_status_update();
vehicle_land_detected_update();
global_position_update();
local_position_update();
gps_position_update();
sensor_combined_update();
home_position_update(true);
fw_pos_ctrl_status_update(true);
params_update();
/* wakeup source(s) */
px4_pollfd_struct_t fds[1] = {};
/* Setup of loop */
fds[0].fd = _local_pos_sub;
fds[0].events = POLLIN;
/* rate-limit position subscription to 20 Hz / 50 ms */
orb_set_interval(_local_pos_sub, 50);
while (!_task_should_exit) {
/* wait for up to 1000ms for data */
int pret = px4_poll(&fds[0], (sizeof(fds) / sizeof(fds[0])), 1000);
if (pret == 0) {
/* Let the loop run anyway, don't do `continue` here. */
} else if (pret < 0) {
/* this is undesirable but not much we can do - might want to flag unhappy status */
PX4_ERR("poll error %d, %d", pret, errno);
usleep(10000);
continue;
} else {
if (fds[0].revents & POLLIN) {
/* success, local pos is available */
local_position_update();
}
}
perf_begin(_loop_perf);
bool updated;
/* gps updated */
orb_check(_gps_pos_sub, &updated);
if (updated) {
gps_position_update();
if (_geofence.getSource() == Geofence::GF_SOURCE_GPS) {
have_geofence_position_data = true;
}
}
/* global position updated */
orb_check(_global_pos_sub, &updated);
if (updated) {
global_position_update();
if (_geofence.getSource() == Geofence::GF_SOURCE_GLOBALPOS) {
have_geofence_position_data = true;
}
}
/* sensors combined updated */
orb_check(_sensor_combined_sub, &updated);
if (updated) {
sensor_combined_update();
}
/* parameters updated */
orb_check(_param_update_sub, &updated);
if (updated) {
params_update();
}
/* vehicle status updated */
orb_check(_vstatus_sub, &updated);
if (updated) {
vehicle_status_update();
}
/* vehicle land detected updated */
orb_check(_land_detected_sub, &updated);
if (updated) {
vehicle_land_detected_update();
}
/* navigation capabilities updated */
orb_check(_fw_pos_ctrl_status_sub, &updated);
if (updated) {
fw_pos_ctrl_status_update();
}
/* home position updated */
orb_check(_home_pos_sub, &updated);
if (updated) {
home_position_update();
}
/* vehicle_command updated */
orb_check(_vehicle_command_sub, &updated);
if (updated) {
vehicle_command_s cmd;
orb_copy(ORB_ID(vehicle_command), _vehicle_command_sub, &cmd);
if (cmd.command == vehicle_command_s::VEHICLE_CMD_DO_GO_AROUND) {
// DO_GO_AROUND is currently handled by the position controller (unacknowledged)
// TODO: move DO_GO_AROUND handling to navigator
publish_vehicle_command_ack(cmd, vehicle_command_s::VEHICLE_CMD_RESULT_ACCEPTED);
} else if (cmd.command == vehicle_command_s::VEHICLE_CMD_DO_REPOSITION) {
position_setpoint_triplet_s *rep = get_reposition_triplet();
position_setpoint_triplet_s *curr = get_position_setpoint_triplet();
// store current position as previous position and goal as next
rep->previous.yaw = get_global_position()->yaw;
rep->previous.lat = get_global_position()->lat;
rep->previous.lon = get_global_position()->lon;
rep->previous.alt = get_global_position()->alt;
rep->current.loiter_radius = get_loiter_radius();
rep->current.loiter_direction = 1;
rep->current.type = position_setpoint_s::SETPOINT_TYPE_LOITER;
rep->current.cruising_speed = get_cruising_speed();
rep->current.cruising_throttle = get_cruising_throttle();
// Go on and check which changes had been requested
if (PX4_ISFINITE(cmd.param4)) {
rep->current.yaw = cmd.param4;
} else {
rep->current.yaw = NAN;
}
if (PX4_ISFINITE(cmd.param5) && PX4_ISFINITE(cmd.param6)) {
// Position change with optional altitude change
rep->current.lat = (cmd.param5 < 1000) ? cmd.param5 : cmd.param5 / (double)1e7;
rep->current.lon = (cmd.param6 < 1000) ? cmd.param6 : cmd.param6 / (double)1e7;
if (PX4_ISFINITE(cmd.param7)) {
rep->current.alt = cmd.param7;
} else {
rep->current.alt = get_global_position()->alt;
}
} else if (PX4_ISFINITE(cmd.param7) && curr->current.valid
&& PX4_ISFINITE(curr->current.lat)
&& PX4_ISFINITE(curr->current.lon)) {
// Altitude without position change
rep->current.lat = curr->current.lat;
rep->current.lon = curr->current.lon;
rep->current.alt = cmd.param7;
} else {
// All three set to NaN - hold in current position
rep->current.lat = get_global_position()->lat;
rep->current.lon = get_global_position()->lon;
rep->current.alt = get_global_position()->alt;
}
rep->previous.valid = true;
rep->current.valid = true;
rep->next.valid = false;
// CMD_DO_REPOSITION is acknowledged by commander
} else if (cmd.command == vehicle_command_s::VEHICLE_CMD_NAV_TAKEOFF) {
position_setpoint_triplet_s *rep = get_takeoff_triplet();
// store current position as previous position and goal as next
rep->previous.yaw = get_global_position()->yaw;
rep->previous.lat = get_global_position()->lat;
rep->previous.lon = get_global_position()->lon;
rep->previous.alt = get_global_position()->alt;
rep->current.loiter_radius = get_loiter_radius();
rep->current.loiter_direction = 1;
rep->current.type = position_setpoint_s::SETPOINT_TYPE_TAKEOFF;
if (home_position_valid()) {
rep->current.yaw = cmd.param4;
rep->previous.valid = true;
} else {
rep->current.yaw = get_local_position()->yaw;
rep->previous.valid = false;
}
if (PX4_ISFINITE(cmd.param5) && PX4_ISFINITE(cmd.param6)) {
rep->current.lat = (cmd.param5 < 1000) ? cmd.param5 : cmd.param5 / (double)1e7;
rep->current.lon = (cmd.param6 < 1000) ? cmd.param6 : cmd.param6 / (double)1e7;
} else {
// If one of them is non-finite, reset both
rep->current.lat = NAN;
rep->current.lon = NAN;
}
rep->current.alt = cmd.param7;
rep->current.valid = true;
rep->next.valid = false;
// CMD_NAV_TAKEOFF is acknowledged by commander
} else if (cmd.command == vehicle_command_s::VEHICLE_CMD_DO_LAND_START) {
/* find NAV_CMD_DO_LAND_START in the mission and
* use MAV_CMD_MISSION_START to start the mission there
*/
int land_start = _mission.find_offboard_land_start();
if (land_start != -1) {
vehicle_command_s vcmd = {};
vcmd.command = vehicle_command_s::VEHICLE_CMD_MISSION_START;
vcmd.param1 = land_start;
publish_vehicle_cmd(&vcmd);
} else {
PX4_WARN("planned landing not available");
}
publish_vehicle_command_ack(cmd, vehicle_command_s::VEHICLE_CMD_RESULT_ACCEPTED);
} else if (cmd.command == vehicle_command_s::VEHICLE_CMD_MISSION_START) {
if (get_mission_result()->valid &&
PX4_ISFINITE(cmd.param1) && (cmd.param1 >= 0) && (cmd.param1 < _mission_result.seq_total)) {
_mission.set_current_offboard_mission_index(cmd.param1);
}
// CMD_MISSION_START is acknowledged by commander
} else if (cmd.command == vehicle_command_s::VEHICLE_CMD_DO_CHANGE_SPEED) {
if (cmd.param2 > FLT_EPSILON) {
// XXX not differentiating ground and airspeed yet
set_cruising_speed(cmd.param2);
} else {
set_cruising_speed();
/* if no speed target was given try to set throttle */
if (cmd.param3 > FLT_EPSILON) {
set_cruising_throttle(cmd.param3 / 100);
} else {
set_cruising_throttle();
}
}
// TODO: handle responses for supported DO_CHANGE_SPEED options?
publish_vehicle_command_ack(cmd, vehicle_command_s::VEHICLE_CMD_RESULT_ACCEPTED);
} else if (cmd.command == vehicle_command_s::VEHICLE_CMD_DO_SET_ROI
|| cmd.command == vehicle_command_s::VEHICLE_CMD_NAV_ROI) {
_vroi = {};
_vroi.mode = cmd.param1;
switch (_vroi.mode) {
case vehicle_command_s::VEHICLE_ROI_NONE:
break;
case vehicle_command_s::VEHICLE_ROI_WPNEXT:
// TODO: implement point toward next MISSION
break;
case vehicle_command_s::VEHICLE_ROI_WPINDEX:
_vroi.mission_seq = cmd.param2;
break;
case vehicle_command_s::VEHICLE_ROI_LOCATION:
_vroi.lat = cmd.param5;
_vroi.lon = cmd.param6;
_vroi.alt = cmd.param7;
break;
case vehicle_command_s::VEHICLE_ROI_TARGET:
_vroi.target_seq = cmd.param2;
break;
default:
_vroi.mode = vehicle_command_s::VEHICLE_ROI_NONE;
break;
}
_vroi.timestamp = hrt_absolute_time();
if (_vehicle_roi_pub != nullptr) {
orb_publish(ORB_ID(vehicle_roi), _vehicle_roi_pub, &_vroi);
} else {
_vehicle_roi_pub = orb_advertise(ORB_ID(vehicle_roi), &_vroi);
}
publish_vehicle_command_ack(cmd, vehicle_command_s::VEHICLE_CMD_RESULT_ACCEPTED);
}
}
/* Check for traffic */
check_traffic();
/* Check geofence violation */
static hrt_abstime last_geofence_check = 0;
if (have_geofence_position_data &&
(_geofence.getGeofenceAction() != geofence_result_s::GF_ACTION_NONE) &&
(hrt_elapsed_time(&last_geofence_check) > GEOFENCE_CHECK_INTERVAL)) {
bool inside = _geofence.check(_global_pos, _gps_pos, _sensor_combined.baro_alt_meter, _home_pos,
home_position_valid());
last_geofence_check = hrt_absolute_time();
have_geofence_position_data = false;
_geofence_result.timestamp = hrt_absolute_time();
_geofence_result.geofence_action = _geofence.getGeofenceAction();
_geofence_result.home_required = _geofence.isHomeRequired();
if (!inside) {
/* inform other apps via the mission result */
_geofence_result.geofence_violated = true;
/* Issue a warning about the geofence violation once */
if (!_geofence_violation_warning_sent) {
mavlink_log_critical(&_mavlink_log_pub, "Geofence violation");
_geofence_violation_warning_sent = true;
}
} else {
/* inform other apps via the mission result */
_geofence_result.geofence_violated = false;
/* Reset the _geofence_violation_warning_sent field */
_geofence_violation_warning_sent = false;
}
publish_geofence_result();
}
/* Do stuff according to navigation state set by commander */
NavigatorMode *navigation_mode_new{nullptr};
switch (_vstatus.nav_state) {
case vehicle_status_s::NAVIGATION_STATE_AUTO_MISSION:
_pos_sp_triplet_published_invalid_once = false;
navigation_mode_new = &_mission;
break;
case vehicle_status_s::NAVIGATION_STATE_AUTO_LOITER:
_pos_sp_triplet_published_invalid_once = false;
navigation_mode_new = &_loiter;
break;
case vehicle_status_s::NAVIGATION_STATE_AUTO_RCRECOVER:
_pos_sp_triplet_published_invalid_once = false;
navigation_mode_new = &_rcLoss;
break;
case vehicle_status_s::NAVIGATION_STATE_AUTO_RTL:
_pos_sp_triplet_published_invalid_once = false;
navigation_mode_new = &_rtl;
break;
case vehicle_status_s::NAVIGATION_STATE_AUTO_TAKEOFF:
_pos_sp_triplet_published_invalid_once = false;
navigation_mode_new = &_takeoff;
break;
case vehicle_status_s::NAVIGATION_STATE_AUTO_LAND:
_pos_sp_triplet_published_invalid_once = false;
navigation_mode_new = &_land;
break;
case vehicle_status_s::NAVIGATION_STATE_DESCEND:
_pos_sp_triplet_published_invalid_once = false;
navigation_mode_new = &_land;
break;
case vehicle_status_s::NAVIGATION_STATE_AUTO_RTGS:
_pos_sp_triplet_published_invalid_once = false;
navigation_mode_new = &_dataLinkLoss;
break;
case vehicle_status_s::NAVIGATION_STATE_AUTO_LANDENGFAIL:
_pos_sp_triplet_published_invalid_once = false;
navigation_mode_new = &_engineFailure;
break;
case vehicle_status_s::NAVIGATION_STATE_AUTO_LANDGPSFAIL:
_pos_sp_triplet_published_invalid_once = false;
navigation_mode_new = &_gpsFailure;
break;
case vehicle_status_s::NAVIGATION_STATE_AUTO_FOLLOW_TARGET:
_pos_sp_triplet_published_invalid_once = false;
navigation_mode_new = &_follow_target;
break;
case vehicle_status_s::NAVIGATION_STATE_MANUAL:
case vehicle_status_s::NAVIGATION_STATE_ACRO:
case vehicle_status_s::NAVIGATION_STATE_ALTCTL:
case vehicle_status_s::NAVIGATION_STATE_POSCTL:
case vehicle_status_s::NAVIGATION_STATE_TERMINATION:
case vehicle_status_s::NAVIGATION_STATE_OFFBOARD:
case vehicle_status_s::NAVIGATION_STATE_STAB:
default:
_pos_sp_triplet_published_invalid_once = false;
navigation_mode_new = nullptr;
_can_loiter_at_sp = false;
break;
}
/* we have a new navigation mode: reset triplet */
if (_navigation_mode != navigation_mode_new) {
reset_triplets();
}
_navigation_mode = navigation_mode_new;
/* iterate through navigation modes and set active/inactive for each */
for (unsigned int i = 0; i < NAVIGATOR_MODE_ARRAY_SIZE; i++) {
_navigation_mode_array[i]->run(_navigation_mode == _navigation_mode_array[i]);
}
/* if we landed and have not received takeoff setpoint then stay in idle */
if (_land_detected.landed &&
!((_vstatus.nav_state == vehicle_status_s::NAVIGATION_STATE_AUTO_TAKEOFF)
|| (_vstatus.nav_state == vehicle_status_s::NAVIGATION_STATE_AUTO_MISSION))) {
_pos_sp_triplet.current.type = position_setpoint_s::SETPOINT_TYPE_IDLE;
_pos_sp_triplet.current.valid = true;
_pos_sp_triplet.previous.valid = false;
_pos_sp_triplet.next.valid = false;
}
/* if nothing is running, set position setpoint triplet invalid once */
if (_navigation_mode == nullptr && !_pos_sp_triplet_published_invalid_once) {
_pos_sp_triplet_published_invalid_once = true;
reset_triplets();
}
if (_pos_sp_triplet_updated) {
_pos_sp_triplet.timestamp = hrt_absolute_time();
publish_position_setpoint_triplet();
_pos_sp_triplet_updated = false;
}
if (_mission_result_updated) {
publish_mission_result();
_mission_result_updated = false;
}
perf_end(_loop_perf);
}
orb_unsubscribe(_global_pos_sub);
orb_unsubscribe(_local_pos_sub);
orb_unsubscribe(_gps_pos_sub);
orb_unsubscribe(_sensor_combined_sub);
orb_unsubscribe(_fw_pos_ctrl_status_sub);
orb_unsubscribe(_vstatus_sub);
orb_unsubscribe(_land_detected_sub);
orb_unsubscribe(_home_pos_sub);
orb_unsubscribe(_onboard_mission_sub);
orb_unsubscribe(_offboard_mission_sub);
orb_unsubscribe(_param_update_sub);
orb_unsubscribe(_vehicle_command_sub);
PX4_INFO("exiting");
_navigator_task = -1;
}
void pwm_limit_calc(const bool armed, const unsigned num_channels, const uint16_t *disarmed_pwm, const uint16_t *min_pwm, const uint16_t *max_pwm, const float *output, uint16_t *effective_pwm, pwm_limit_t *limit)
{
/* first evaluate state changes */
switch (limit->state) {
case PWM_LIMIT_STATE_INIT:
if (armed) {
/* set arming time for the first call */
if (limit->time_armed == 0) {
limit->time_armed = hrt_absolute_time();
}
if (hrt_elapsed_time(&limit->time_armed) >= INIT_TIME_US) {
limit->state = PWM_LIMIT_STATE_OFF;
}
}
break;
case PWM_LIMIT_STATE_OFF:
if (armed) {
limit->state = PWM_LIMIT_STATE_RAMP;
/* reset arming time, used for ramp timing */
limit->time_armed = hrt_absolute_time();
}
break;
case PWM_LIMIT_STATE_RAMP:
if (!armed) {
limit->state = PWM_LIMIT_STATE_OFF;
} else if (hrt_elapsed_time(&limit->time_armed) >= RAMP_TIME_US) {
limit->state = PWM_LIMIT_STATE_ON;
}
break;
case PWM_LIMIT_STATE_ON:
if (!armed) {
limit->state = PWM_LIMIT_STATE_OFF;
}
break;
default:
break;
}
unsigned progress;
/* then set effective_pwm based on state */
switch (limit->state) {
case PWM_LIMIT_STATE_OFF:
case PWM_LIMIT_STATE_INIT:
for (unsigned i=0; i<num_channels; i++) {
effective_pwm[i] = disarmed_pwm[i];
}
break;
case PWM_LIMIT_STATE_RAMP:
{
hrt_abstime diff = hrt_elapsed_time(&limit->time_armed);
progress = diff * 10000 / RAMP_TIME_US;
for (unsigned i=0; i<num_channels; i++) {
uint16_t ramp_min_pwm;
/* if a disarmed pwm value was set, blend between disarmed and min */
if (disarmed_pwm[i] > 0) {
/* safeguard against overflows */
unsigned disarmed = disarmed_pwm[i];
if (disarmed > min_pwm[i]) {
disarmed = min_pwm[i];
}
unsigned disarmed_min_diff = min_pwm[i] - disarmed;
ramp_min_pwm = disarmed + (disarmed_min_diff * progress) / 10000;
} else {
/* no disarmed pwm value set, choose min pwm */
ramp_min_pwm = min_pwm[i];
}
effective_pwm[i] = output[i] * (max_pwm[i] - ramp_min_pwm)/2 + (max_pwm[i] + ramp_min_pwm)/2;
/* last line of defense against invalid inputs */
if (effective_pwm[i] < ramp_min_pwm) {
effective_pwm[i] = ramp_min_pwm;
} else if (effective_pwm[i] > max_pwm[i]) {
effective_pwm[i] = max_pwm[i];
}
}
}
break;
case PWM_LIMIT_STATE_ON:
for (unsigned i=0; i<num_channels; i++) {
effective_pwm[i] = output[i] * (max_pwm[i] - min_pwm[i])/2 + (max_pwm[i] + min_pwm[i])/2;
/* last line of defense against invalid inputs */
if (effective_pwm[i] < min_pwm[i]) {
effective_pwm[i] = min_pwm[i];
} else if (effective_pwm[i] > max_pwm[i]) {
effective_pwm[i] = max_pwm[i];
}
}
break;
default:
break;
}
return;
}
int test_mixer(int argc, char *argv[])
{
/*
* PWM limit structure
*/
pwm_limit_t pwm_limit;
bool should_arm = false;
uint16_t r_page_servo_disarmed[output_max];
uint16_t r_page_servo_control_min[output_max];
uint16_t r_page_servo_control_max[output_max];
uint16_t r_page_servos[output_max];
uint16_t servo_predicted[output_max];
int16_t reverse_pwm_mask = 0;
//PX4_INFO("testing mixer");
#if !defined(CONFIG_ARCH_BOARD_SITL)
const char *filename = "/etc/mixers/IO_pass.mix";
#else
const char *filename = "../../../../ROMFS/px4fmu_test/mixers/IO_pass.mix";
#endif
//PX4_INFO("loading: %s", filename);
char buf[2048];
load_mixer_file(filename, &buf[0], sizeof(buf));
unsigned loaded = strlen(buf);
//fprintf(stderr, "loaded: \n\"%s\"\n (%d chars)", &buf[0], loaded);
/* load the mixer in chunks, like
* in the case of a remote load,
* e.g. on PX4IO.
*/
const unsigned chunk_size = 64;
MixerGroup mixer_group(mixer_callback, 0);
/* load at once test */
unsigned xx = loaded;
mixer_group.load_from_buf(&buf[0], xx);
//ASSERT_EQ(mixer_group.count(), 8);
unsigned empty_load = 2;
char empty_buf[2];
empty_buf[0] = ' ';
empty_buf[1] = '\0';
mixer_group.reset();
mixer_group.load_from_buf(&empty_buf[0], empty_load);
//PX4_INFO("empty buffer load: loaded %u mixers, used: %u", mixer_group.count(), empty_load);
//ASSERT_NE(empty_load, 0);
if (empty_load != 0) {
return 1;
}
/* FIRST mark the mixer as invalid */
/* THEN actually delete it */
mixer_group.reset();
char mixer_text[256]; /* large enough for one mixer */
unsigned mixer_text_length = 0;
unsigned transmitted = 0;
//PX4_INFO("transmitted: %d, loaded: %d", transmitted, loaded);
while (transmitted < loaded) {
unsigned text_length = (loaded - transmitted > chunk_size) ? chunk_size : loaded - transmitted;
/* check for overflow - this would be really fatal */
if ((mixer_text_length + text_length + 1) > sizeof(mixer_text)) {
return 1;
}
/* append mixer text and nul-terminate */
memcpy(&mixer_text[mixer_text_length], &buf[transmitted], text_length);
mixer_text_length += text_length;
mixer_text[mixer_text_length] = '\0';
//fprintf(stderr, "buflen %u, text:\n\"%s\"", mixer_text_length, &mixer_text[0]);
/* process the text buffer, adding new mixers as their descriptions can be parsed */
unsigned resid = mixer_text_length;
mixer_group.load_from_buf(&mixer_text[0], resid);
/* if anything was parsed */
if (resid != mixer_text_length) {
//fprintf(stderr, "used %u", mixer_text_length - resid);
/* copy any leftover text to the base of the buffer for re-use */
if (resid > 0) {
memcpy(&mixer_text[0], &mixer_text[mixer_text_length - resid], resid);
}
mixer_text_length = resid;
}
transmitted += text_length;
}
//PX4_INFO("chunked load: loaded %u mixers", mixer_group.count());
if (mixer_group.count() != 8) {
return 1;
}
/* execute the mixer */
float outputs[output_max];
unsigned mixed;
const int jmax = 5;
pwm_limit_init(&pwm_limit);
/* run through arming phase */
for (unsigned i = 0; i < output_max; i++) {
actuator_controls[i] = 0.1f;
r_page_servo_disarmed[i] = PWM_MOTOR_OFF;
r_page_servo_control_min[i] = PWM_DEFAULT_MIN;
r_page_servo_control_max[i] = PWM_DEFAULT_MAX;
}
//PX4_INFO("PRE-ARM TEST: DISABLING SAFETY");
/* mix */
should_prearm = true;
mixed = mixer_group.mix(&outputs[0], output_max, NULL);
pwm_limit_calc(should_arm, should_prearm, mixed, reverse_pwm_mask, r_page_servo_disarmed, r_page_servo_control_min,
r_page_servo_control_max, outputs, r_page_servos, &pwm_limit);
//warnx("mixed %d outputs (max %d), values:", mixed, output_max);
for (unsigned i = 0; i < mixed; i++) {
//fprintf(stderr, "pre-arm:\t %d: out: %8.4f, servo: %d \n", i, (double)outputs[i], (int)r_page_servos[i]);
if (i != actuator_controls_s::INDEX_THROTTLE) {
if (r_page_servos[i] < r_page_servo_control_min[i]) {
warnx("active servo < min");
return 1;
}
} else {
if (r_page_servos[i] != r_page_servo_disarmed[i]) {
warnx("throttle output != 0 (this check assumed the IO pass mixer!)");
return 1;
}
}
}
should_arm = true;
should_prearm = false;
/* simulate another orb_copy() from actuator controls */
for (unsigned i = 0; i < output_max; i++) {
actuator_controls[i] = 0.1f;
}
//PX4_INFO("ARMING TEST: STARTING RAMP");
unsigned sleep_quantum_us = 10000;
hrt_abstime starttime = hrt_absolute_time();
unsigned sleepcount = 0;
while (hrt_elapsed_time(&starttime) < INIT_TIME_US + RAMP_TIME_US + 2 * sleep_quantum_us) {
/* mix */
mixed = mixer_group.mix(&outputs[0], output_max, NULL);
pwm_limit_calc(should_arm, should_prearm, mixed, reverse_pwm_mask, r_page_servo_disarmed, r_page_servo_control_min,
r_page_servo_control_max, outputs, r_page_servos, &pwm_limit);
//warnx("mixed %d outputs (max %d), values:", mixed, output_max);
for (unsigned i = 0; i < mixed; i++) {
//fprintf(stderr, "ramp:\t %d: out: %8.4f, servo: %d \n", i, (double)outputs[i], (int)r_page_servos[i]);
/* check mixed outputs to be zero during init phase */
if (hrt_elapsed_time(&starttime) < INIT_TIME_US &&
r_page_servos[i] != r_page_servo_disarmed[i]) {
PX4_ERR("disarmed servo value mismatch: %d vs %d", r_page_servos[i], r_page_servo_disarmed[i]);
return 1;
}
if (hrt_elapsed_time(&starttime) >= INIT_TIME_US &&
r_page_servos[i] + 1 <= r_page_servo_disarmed[i]) {
PX4_ERR("ramp servo value mismatch");
return 1;
}
}
usleep(sleep_quantum_us);
sleepcount++;
if (sleepcount % 10 == 0) {
fflush(stdout);
}
}
//PX4_INFO("ARMING TEST: NORMAL OPERATION");
for (int j = -jmax; j <= jmax; j++) {
for (unsigned i = 0; i < output_max; i++) {
actuator_controls[i] = j / 10.0f + 0.1f * i;
r_page_servo_disarmed[i] = PWM_LOWEST_MIN;
r_page_servo_control_min[i] = PWM_DEFAULT_MIN;
r_page_servo_control_max[i] = PWM_DEFAULT_MAX;
}
/* mix */
mixed = mixer_group.mix(&outputs[0], output_max, NULL);
pwm_limit_calc(should_arm, should_prearm, mixed, reverse_pwm_mask, r_page_servo_disarmed, r_page_servo_control_min,
r_page_servo_control_max, outputs,
r_page_servos, &pwm_limit);
//fprintf(stderr, "mixed %d outputs (max %d)", mixed, output_max);
for (unsigned i = 0; i < mixed; i++) {
servo_predicted[i] = 1500 + outputs[i] * (r_page_servo_control_max[i] - r_page_servo_control_min[i]) / 2.0f;
if (abs(servo_predicted[i] - r_page_servos[i]) > MIXER_DIFFERENCE_THRESHOLD) {
fprintf(stderr, "\t %d: %8.4f predicted: %d, servo: %d\n", i, (double)outputs[i], servo_predicted[i],
(int)r_page_servos[i]);
PX4_ERR("mixer violated predicted value");
return 1;
}
}
}
//PX4_INFO("ARMING TEST: DISARMING");
starttime = hrt_absolute_time();
sleepcount = 0;
should_arm = false;
while (hrt_elapsed_time(&starttime) < 600000) {
/* mix */
mixed = mixer_group.mix(&outputs[0], output_max, NULL);
pwm_limit_calc(should_arm, should_prearm, mixed, reverse_pwm_mask, r_page_servo_disarmed, r_page_servo_control_min,
r_page_servo_control_max, outputs,
r_page_servos, &pwm_limit);
//warnx("mixed %d outputs (max %d), values:", mixed, output_max);
for (unsigned i = 0; i < mixed; i++) {
//fprintf(stderr, "disarmed:\t %d: out: %8.4f, servo: %d \n", i, (double)outputs[i], (int)r_page_servos[i]);
/* check mixed outputs to be zero during init phase */
if (r_page_servos[i] != r_page_servo_disarmed[i]) {
PX4_ERR("disarmed servo value mismatch");
return 1;
}
}
usleep(sleep_quantum_us);
sleepcount++;
if (sleepcount % 10 == 0) {
//printf(".");
//fflush(stdout);
}
}
//printf("\n");
//PX4_INFO("ARMING TEST: REARMING: STARTING RAMP");
starttime = hrt_absolute_time();
sleepcount = 0;
should_arm = true;
while (hrt_elapsed_time(&starttime) < 600000 + RAMP_TIME_US) {
/* mix */
mixed = mixer_group.mix(&outputs[0], output_max, NULL);
pwm_limit_calc(should_arm, should_prearm, mixed, reverse_pwm_mask, r_page_servo_disarmed, r_page_servo_control_min,
r_page_servo_control_max, outputs,
r_page_servos, &pwm_limit);
//warnx("mixed %d outputs (max %d), values:", mixed, output_max);
for (unsigned i = 0; i < mixed; i++) {
/* predict value */
servo_predicted[i] = 1500 + outputs[i] * (r_page_servo_control_max[i] - r_page_servo_control_min[i]) / 2.0f;
/* check ramp */
//fprintf(stderr, "ramp:\t %d: out: %8.4f, servo: %d \n", i, (double)outputs[i], (int)r_page_servos[i]);
if (hrt_elapsed_time(&starttime) < RAMP_TIME_US &&
(r_page_servos[i] + 1 <= r_page_servo_disarmed[i] ||
r_page_servos[i] > servo_predicted[i])) {
PX4_ERR("ramp servo value mismatch");
return 1;
}
/* check post ramp phase */
if (hrt_elapsed_time(&starttime) > RAMP_TIME_US &&
abs(servo_predicted[i] - r_page_servos[i]) > 2) {
printf("\t %d: %8.4f predicted: %d, servo: %d\n", i, (double)outputs[i], servo_predicted[i], (int)r_page_servos[i]);
PX4_ERR("mixer violated predicted value");
return 1;
}
}
usleep(sleep_quantum_us);
sleepcount++;
if (sleepcount % 10 == 0) {
// printf(".");
// fflush(stdout);
}
}
//printf("\n");
/* load multirotor at once test */
mixer_group.reset();
#if !defined(CONFIG_ARCH_BOARD_SITL)
filename = "/etc/mixers/quad_test.mix";
#else
filename = "../../../../ROMFS/px4fmu_test/mixers/quad_test.mix";
#endif
load_mixer_file(filename, &buf[0], sizeof(buf));
loaded = strlen(buf);
//fprintf(stderr, "loaded: \n\"%s\"\n (%d chars)", &buf[0], loaded);
unsigned mc_loaded = loaded;
mixer_group.load_from_buf(&buf[0], mc_loaded);
//PX4_INFO("complete buffer load: loaded %u mixers", mixer_group.count());
if (mixer_group.count() != 5) {
PX4_ERR("FAIL: Quad test mixer load failed");
return 1;
}
//PX4_INFO("SUCCESS: No errors in mixer test");
return 0;
}
void
Navigator::task_main()
{
bool have_geofence_position_data = false;
/* Try to load the geofence:
* if /fs/microsd/etc/geofence.txt load from this file
* else clear geofence data in datamanager */
struct stat buffer;
if (stat(GEOFENCE_FILENAME, &buffer) == 0) {
warnx("Try to load geofence.txt");
_geofence.loadFromFile(GEOFENCE_FILENAME);
} else {
if (_geofence.clearDm() != OK) {
mavlink_log_critical(&_mavlink_log_pub, "failed clearing geofence");
}
}
/* do subscriptions */
_global_pos_sub = orb_subscribe(ORB_ID(vehicle_global_position));
_gps_pos_sub = orb_subscribe(ORB_ID(vehicle_gps_position));
_sensor_combined_sub = orb_subscribe(ORB_ID(sensor_combined));
_capabilities_sub = orb_subscribe(ORB_ID(navigation_capabilities));
_vstatus_sub = orb_subscribe(ORB_ID(vehicle_status));
_land_detected_sub = orb_subscribe(ORB_ID(vehicle_land_detected));
_control_mode_sub = orb_subscribe(ORB_ID(vehicle_control_mode));
_home_pos_sub = orb_subscribe(ORB_ID(home_position));
_onboard_mission_sub = orb_subscribe(ORB_ID(onboard_mission));
_offboard_mission_sub = orb_subscribe(ORB_ID(offboard_mission));
_param_update_sub = orb_subscribe(ORB_ID(parameter_update));
_vehicle_command_sub = orb_subscribe(ORB_ID(vehicle_command));
/* copy all topics first time */
vehicle_status_update();
vehicle_land_detected_update();
vehicle_control_mode_update();
global_position_update();
gps_position_update();
sensor_combined_update();
home_position_update(true);
navigation_capabilities_update();
params_update();
/* wakeup source(s) */
px4_pollfd_struct_t fds[1] = {};
/* Setup of loop */
fds[0].fd = _global_pos_sub;
fds[0].events = POLLIN;
bool global_pos_available_once = false;
while (!_task_should_exit) {
/* wait for up to 200ms for data */
int pret = px4_poll(&fds[0], (sizeof(fds) / sizeof(fds[0])), 1000);
if (pret == 0) {
/* timed out - periodic check for _task_should_exit, etc. */
if (global_pos_available_once) {
PX4_WARN("navigator timed out");
}
continue;
} else if (pret < 0) {
/* this is undesirable but not much we can do - might want to flag unhappy status */
PX4_WARN("nav: poll error %d, %d", pret, errno);
continue;
}
global_pos_available_once = true;
perf_begin(_loop_perf);
bool updated;
/* gps updated */
orb_check(_gps_pos_sub, &updated);
if (updated) {
gps_position_update();
if (_geofence.getSource() == Geofence::GF_SOURCE_GPS) {
have_geofence_position_data = true;
}
}
/* sensors combined updated */
orb_check(_sensor_combined_sub, &updated);
if (updated) {
sensor_combined_update();
}
/* parameters updated */
orb_check(_param_update_sub, &updated);
if (updated) {
params_update();
updateParams();
}
/* vehicle control mode updated */
orb_check(_control_mode_sub, &updated);
if (updated) {
vehicle_control_mode_update();
}
/* vehicle status updated */
orb_check(_vstatus_sub, &updated);
if (updated) {
vehicle_status_update();
}
/* vehicle land detected updated */
orb_check(_land_detected_sub, &updated);
if (updated) {
vehicle_land_detected_update();
}
/* navigation capabilities updated */
orb_check(_capabilities_sub, &updated);
if (updated) {
navigation_capabilities_update();
}
/* home position updated */
orb_check(_home_pos_sub, &updated);
if (updated) {
home_position_update();
}
orb_check(_vehicle_command_sub, &updated);
if (updated) {
vehicle_command_s cmd;
orb_copy(ORB_ID(vehicle_command), _vehicle_command_sub, &cmd);
if (cmd.command == vehicle_command_s::VEHICLE_CMD_DO_REPOSITION) {
warnx("navigator: got reposition command");
}
if (cmd.command == vehicle_command_s::VEHICLE_CMD_DO_PAUSE_CONTINUE) {
warnx("navigator: got pause/continue command");
}
}
/* global position updated */
if (fds[0].revents & POLLIN) {
global_position_update();
if (_geofence.getSource() == Geofence::GF_SOURCE_GLOBALPOS) {
have_geofence_position_data = true;
}
}
/* Check geofence violation */
static hrt_abstime last_geofence_check = 0;
if (have_geofence_position_data &&
(_geofence.getGeofenceAction() != geofence_result_s::GF_ACTION_NONE) &&
(hrt_elapsed_time(&last_geofence_check) > GEOFENCE_CHECK_INTERVAL)) {
bool inside = _geofence.inside(_global_pos, _gps_pos, _sensor_combined.baro_alt_meter[0], _home_pos, home_position_valid());
last_geofence_check = hrt_absolute_time();
have_geofence_position_data = false;
_geofence_result.geofence_action = _geofence.getGeofenceAction();
if (!inside) {
/* inform other apps via the mission result */
_geofence_result.geofence_violated = true;
publish_geofence_result();
/* Issue a warning about the geofence violation once */
if (!_geofence_violation_warning_sent) {
mavlink_log_critical(&_mavlink_log_pub, "Geofence violation");
_geofence_violation_warning_sent = true;
}
} else {
/* inform other apps via the mission result */
_geofence_result.geofence_violated = false;
publish_geofence_result();
/* Reset the _geofence_violation_warning_sent field */
_geofence_violation_warning_sent = false;
}
}
/* Do stuff according to navigation state set by commander */
switch (_vstatus.nav_state) {
case vehicle_status_s::NAVIGATION_STATE_MANUAL:
case vehicle_status_s::NAVIGATION_STATE_ACRO:
case vehicle_status_s::NAVIGATION_STATE_ALTCTL:
case vehicle_status_s::NAVIGATION_STATE_POSCTL:
case vehicle_status_s::NAVIGATION_STATE_TERMINATION:
case vehicle_status_s::NAVIGATION_STATE_OFFBOARD:
_navigation_mode = nullptr;
_can_loiter_at_sp = false;
break;
case vehicle_status_s::NAVIGATION_STATE_AUTO_MISSION:
if (_nav_caps.abort_landing) {
// pos controller aborted landing, requests loiter
// above landing waypoint
_navigation_mode = &_loiter;
_pos_sp_triplet_published_invalid_once = false;
} else {
_pos_sp_triplet_published_invalid_once = false;
_navigation_mode = &_mission;
}
break;
case vehicle_status_s::NAVIGATION_STATE_AUTO_LOITER:
_pos_sp_triplet_published_invalid_once = false;
_navigation_mode = &_loiter;
break;
case vehicle_status_s::NAVIGATION_STATE_AUTO_RCRECOVER:
_pos_sp_triplet_published_invalid_once = false;
if (_param_rcloss_act.get() == 0) {
_navigation_mode = &_loiter;
} else if (_param_rcloss_act.get() == 2) {
_navigation_mode = &_land;
} else if (_param_rcloss_act.get() == 3) {
_navigation_mode = &_rcLoss;
} else { /* if == 1 or unknown, RTL */
_navigation_mode = &_rtl;
}
break;
case vehicle_status_s::NAVIGATION_STATE_AUTO_RTL:
_pos_sp_triplet_published_invalid_once = false;
_navigation_mode = &_rtl;
break;
case vehicle_status_s::NAVIGATION_STATE_AUTO_TAKEOFF:
_pos_sp_triplet_published_invalid_once = false;
_navigation_mode = &_takeoff;
break;
case vehicle_status_s::NAVIGATION_STATE_AUTO_LAND:
_pos_sp_triplet_published_invalid_once = false;
_navigation_mode = &_land;
break;
case vehicle_status_s::NAVIGATION_STATE_DESCEND:
_pos_sp_triplet_published_invalid_once = false;
_navigation_mode = &_land;
break;
case vehicle_status_s::NAVIGATION_STATE_AUTO_RTGS:
/* Use complex data link loss mode only when enabled via param
* otherwise use rtl */
_pos_sp_triplet_published_invalid_once = false;
if (_param_datalinkloss_act.get() == 0) {
_navigation_mode = &_loiter;
} else if (_param_datalinkloss_act.get() == 2) {
_navigation_mode = &_land;
} else if (_param_datalinkloss_act.get() == 3) {
_navigation_mode = &_dataLinkLoss;
} else { /* if == 1 or unknown, RTL */
_navigation_mode = &_rtl;
}
break;
case vehicle_status_s::NAVIGATION_STATE_AUTO_LANDENGFAIL:
_pos_sp_triplet_published_invalid_once = false;
_navigation_mode = &_engineFailure;
break;
case vehicle_status_s::NAVIGATION_STATE_AUTO_LANDGPSFAIL:
_pos_sp_triplet_published_invalid_once = false;
_navigation_mode = &_gpsFailure;
break;
case vehicle_status_s::NAVIGATION_STATE_AUTO_FOLLOW_TARGET:
_pos_sp_triplet_published_invalid_once = false;
_navigation_mode = &_follow_target;
break;
default:
_navigation_mode = nullptr;
_can_loiter_at_sp = false;
break;
}
/* iterate through navigation modes and set active/inactive for each */
for (unsigned int i = 0; i < NAVIGATOR_MODE_ARRAY_SIZE; i++) {
_navigation_mode_array[i]->run(_navigation_mode == _navigation_mode_array[i]);
}
/* if nothing is running, set position setpoint triplet invalid once */
if (_navigation_mode == nullptr && !_pos_sp_triplet_published_invalid_once) {
_pos_sp_triplet_published_invalid_once = true;
_pos_sp_triplet.previous.valid = false;
_pos_sp_triplet.current.valid = false;
_pos_sp_triplet.next.valid = false;
_pos_sp_triplet_updated = true;
}
if (_pos_sp_triplet_updated) {
publish_position_setpoint_triplet();
_pos_sp_triplet_updated = false;
}
if (_mission_result_updated) {
publish_mission_result();
_mission_result_updated = false;
}
perf_end(_loop_perf);
}
warnx("exiting.");
_navigator_task = -1;
return;
}
int
TFMINI::collect()
{
perf_begin(_sample_perf);
/* clear buffer if last read was too long ago */
int64_t read_elapsed = hrt_elapsed_time(&_last_read);
/* the buffer for read chars is buflen minus null termination */
char readbuf[sizeof(_linebuf)];
unsigned readlen = sizeof(readbuf) - 1;
int ret = 0;
float distance_m = -1.0f;
/* Check the number of bytes available in the buffer*/
int bytes_available = 0;
::ioctl(_fd, FIONREAD, (unsigned long)&bytes_available);
if (!bytes_available) {
return -EAGAIN;
}
/* parse entire buffer */
do {
/* read from the sensor (uart buffer) */
ret = ::read(_fd, &readbuf[0], readlen);
if (ret < 0) {
PX4_ERR("read err: %d", ret);
perf_count(_comms_errors);
perf_end(_sample_perf);
/* only throw an error if we time out */
if (read_elapsed > (_conversion_interval * 2)) {
/* flush anything in RX buffer */
tcflush(_fd, TCIFLUSH);
return ret;
} else {
return -EAGAIN;
}
}
_last_read = hrt_absolute_time();
/* parse buffer */
for (int i = 0; i < ret; i++) {
tfmini_parse(readbuf[i], _linebuf, &_linebuf_index, &_parse_state, &distance_m);
}
/* bytes left to parse */
bytes_available -= ret;
} while (bytes_available > 0);
/* no valid measurement after parsing buffer */
if (distance_m < 0.0f) {
return -EAGAIN;
}
/* publish most recent valid measurement from buffer */
distance_sensor_s report{};
report.timestamp = hrt_absolute_time();
report.type = distance_sensor_s::MAV_DISTANCE_SENSOR_LASER;
report.orientation = _rotation;
report.current_distance = distance_m;
report.min_distance = get_minimum_distance();
report.max_distance = get_maximum_distance();
report.covariance = 0.0f;
report.signal_quality = -1;
/* TODO: set proper ID */
report.id = 0;
/* publish it */
orb_publish(ORB_ID(distance_sensor), _distance_sensor_topic, &report);
_reports->force(&report);
/* notify anyone waiting for data */
poll_notify(POLLIN);
ret = OK;
perf_end(_sample_perf);
return ret;
}
void
mixer_tick(void)
{
/* check that we are receiving fresh data from the FMU */
if (hrt_elapsed_time(&system_state.fmu_data_received_time) > FMU_INPUT_DROP_LIMIT_US) {
/* too long without FMU input, time to go to failsafe */
if (r_status_flags & PX4IO_P_STATUS_FLAGS_FMU_OK) {
isr_debug(1, "AP RX timeout");
}
r_status_flags &= ~(PX4IO_P_STATUS_FLAGS_FMU_OK);
r_status_alarms |= PX4IO_P_STATUS_ALARMS_FMU_LOST;
} else {
r_status_flags |= PX4IO_P_STATUS_FLAGS_FMU_OK;
}
/* default to failsafe mixing */
source = MIX_FAILSAFE;
/*
* Decide which set of controls we're using.
*/
/* do not mix if RAW_PWM mode is on and FMU is good */
if ((r_status_flags & PX4IO_P_STATUS_FLAGS_RAW_PWM) &&
(r_status_flags & PX4IO_P_STATUS_FLAGS_FMU_OK)) {
/* don't actually mix anything - we already have raw PWM values */
source = MIX_NONE;
} else {
if (!(r_status_flags & PX4IO_P_STATUS_FLAGS_OVERRIDE) &&
(r_status_flags & PX4IO_P_STATUS_FLAGS_FMU_OK) &&
(r_status_flags & PX4IO_P_STATUS_FLAGS_MIXER_OK)) {
/* mix from FMU controls */
source = MIX_FMU;
}
if ( (r_status_flags & PX4IO_P_STATUS_FLAGS_OVERRIDE) &&
(r_status_flags & PX4IO_P_STATUS_FLAGS_RC_OK) &&
(r_status_flags & PX4IO_P_STATUS_FLAGS_MIXER_OK) &&
!(r_setup_arming & PX4IO_P_SETUP_ARMING_RC_HANDLING_DISABLED) &&
!(r_status_flags & PX4IO_P_STATUS_FLAGS_FMU_OK)) {
/* if allowed, mix from RC inputs directly */
source = MIX_OVERRIDE;
} else if ( (r_status_flags & PX4IO_P_STATUS_FLAGS_OVERRIDE) &&
(r_status_flags & PX4IO_P_STATUS_FLAGS_RC_OK) &&
(r_status_flags & PX4IO_P_STATUS_FLAGS_MIXER_OK) &&
!(r_setup_arming & PX4IO_P_SETUP_ARMING_RC_HANDLING_DISABLED) &&
(r_status_flags & PX4IO_P_STATUS_FLAGS_FMU_OK)) {
/* if allowed, mix from RC inputs directly up to available rc channels */
source = MIX_OVERRIDE_FMU_OK;
}
}
/*
* Set failsafe status flag depending on mixing source
*/
if (source == MIX_FAILSAFE) {
r_status_flags |= PX4IO_P_STATUS_FLAGS_FAILSAFE;
} else {
r_status_flags &= ~(PX4IO_P_STATUS_FLAGS_FAILSAFE);
}
/*
* Decide whether the servos should be armed right now.
*
* We must be armed, and we must have a PWM source; either raw from
* FMU or from the mixer.
*
* XXX correct behaviour for failsafe may require an additional case
* here.
*/
should_arm = (
/* IO initialised without error */ (r_status_flags & PX4IO_P_STATUS_FLAGS_INIT_OK)
/* and IO is armed */ && (r_status_flags & PX4IO_P_STATUS_FLAGS_SAFETY_OFF)
/* and FMU is armed */ && (
((r_setup_arming & PX4IO_P_SETUP_ARMING_FMU_ARMED)
/* and there is valid input via or mixer */ && (r_status_flags & PX4IO_P_STATUS_FLAGS_MIXER_OK) )
/* or direct PWM is set */ || (r_status_flags & PX4IO_P_STATUS_FLAGS_RAW_PWM)
/* or failsafe was set manually */ || (r_setup_arming & PX4IO_P_SETUP_ARMING_FAILSAFE_CUSTOM)
)
);
should_always_enable_pwm = (r_setup_arming & PX4IO_P_SETUP_ARMING_ALWAYS_PWM_ENABLE)
&& (r_status_flags & PX4IO_P_STATUS_FLAGS_INIT_OK)
&& (r_status_flags & PX4IO_P_STATUS_FLAGS_FMU_OK);
/*
* Run the mixers.
*/
if (source == MIX_FAILSAFE) {
/* copy failsafe values to the servo outputs */
for (unsigned i = 0; i < PX4IO_SERVO_COUNT; i++) {
r_page_servos[i] = r_page_servo_failsafe[i];
/* safe actuators for FMU feedback */
r_page_actuators[i] = FLOAT_TO_REG((r_page_servos[i] - 1500) / 600.0f);
}
} else if (source != MIX_NONE && (r_status_flags & PX4IO_P_STATUS_FLAGS_MIXER_OK)) {
float outputs[PX4IO_SERVO_COUNT];
unsigned mixed;
/* mix */
/* poor mans mutex */
in_mixer = true;
mixed = mixer_group.mix(&outputs[0], PX4IO_SERVO_COUNT);
in_mixer = false;
pwm_limit_calc(should_arm, mixed, r_page_servo_disarmed, r_page_servo_control_min, r_page_servo_control_max, outputs, r_page_servos, &pwm_limit);
for (unsigned i = mixed; i < PX4IO_SERVO_COUNT; i++)
r_page_servos[i] = 0;
for (unsigned i = 0; i < PX4IO_SERVO_COUNT; i++) {
r_page_actuators[i] = FLOAT_TO_REG(outputs[i]);
}
}
if ((should_arm || should_always_enable_pwm) && !mixer_servos_armed) {
/* need to arm, but not armed */
up_pwm_servo_arm(true);
mixer_servos_armed = true;
r_status_flags |= PX4IO_P_STATUS_FLAGS_OUTPUTS_ARMED;
isr_debug(5, "> PWM enabled");
} else if ((!should_arm && !should_always_enable_pwm) && mixer_servos_armed) {
/* armed but need to disarm */
up_pwm_servo_arm(false);
mixer_servos_armed = false;
r_status_flags &= ~(PX4IO_P_STATUS_FLAGS_OUTPUTS_ARMED);
isr_debug(5, "> PWM disabled");
}
if (mixer_servos_armed && should_arm) {
/* update the servo outputs. */
for (unsigned i = 0; i < PX4IO_SERVO_COUNT; i++)
up_pwm_servo_set(i, r_page_servos[i]);
} else if (mixer_servos_armed && should_always_enable_pwm) {
/* set the disarmed servo outputs. */
for (unsigned i = 0; i < PX4IO_SERVO_COUNT; i++)
up_pwm_servo_set(i, r_page_servo_disarmed[i]);
}
}
void
mixer_tick(void)
{
/* check that we are receiving fresh data from the FMU */
if ((system_state.fmu_data_received_time == 0) ||
hrt_elapsed_time(&system_state.fmu_data_received_time) > FMU_INPUT_DROP_LIMIT_US) {
/* too long without FMU input, time to go to failsafe */
if (r_status_flags & PX4IO_P_STATUS_FLAGS_FMU_OK) {
isr_debug(1, "AP RX timeout");
}
r_status_flags &= ~(PX4IO_P_STATUS_FLAGS_FMU_OK);
r_status_alarms |= PX4IO_P_STATUS_ALARMS_FMU_LOST;
} else {
r_status_flags |= PX4IO_P_STATUS_FLAGS_FMU_OK;
/* this flag is never cleared once OK */
r_status_flags |= PX4IO_P_STATUS_FLAGS_FMU_INITIALIZED;
}
/* default to failsafe mixing - it will be forced below if flag is set */
source = MIX_FAILSAFE;
/*
* Decide which set of controls we're using.
*/
/* do not mix if RAW_PWM mode is on and FMU is good */
if ((r_status_flags & PX4IO_P_STATUS_FLAGS_RAW_PWM) &&
(r_status_flags & PX4IO_P_STATUS_FLAGS_FMU_OK)) {
/* don't actually mix anything - we already have raw PWM values */
source = MIX_NONE;
} else {
if (!(r_status_flags & PX4IO_P_STATUS_FLAGS_OVERRIDE) &&
(r_status_flags & PX4IO_P_STATUS_FLAGS_FMU_OK) &&
(r_status_flags & PX4IO_P_STATUS_FLAGS_MIXER_OK)) {
/* mix from FMU controls */
source = MIX_FMU;
}
if ( (r_status_flags & PX4IO_P_STATUS_FLAGS_OVERRIDE) &&
(r_status_flags & PX4IO_P_STATUS_FLAGS_RC_OK) &&
(r_status_flags & PX4IO_P_STATUS_FLAGS_MIXER_OK) &&
!(r_setup_arming & PX4IO_P_SETUP_ARMING_RC_HANDLING_DISABLED) &&
!(r_status_flags & PX4IO_P_STATUS_FLAGS_FMU_OK) &&
/* do not enter manual override if we asked for termination failsafe and FMU is lost */
!(r_setup_arming & PX4IO_P_SETUP_ARMING_TERMINATION_FAILSAFE)) {
/* if allowed, mix from RC inputs directly */
source = MIX_OVERRIDE;
} else if ( (r_status_flags & PX4IO_P_STATUS_FLAGS_OVERRIDE) &&
(r_status_flags & PX4IO_P_STATUS_FLAGS_RC_OK) &&
(r_status_flags & PX4IO_P_STATUS_FLAGS_MIXER_OK) &&
!(r_setup_arming & PX4IO_P_SETUP_ARMING_RC_HANDLING_DISABLED) &&
(r_status_flags & PX4IO_P_STATUS_FLAGS_FMU_OK)) {
/* if allowed, mix from RC inputs directly up to available rc channels */
source = MIX_OVERRIDE_FMU_OK;
}
}
/*
* Decide whether the servos should be armed right now.
*
* We must be armed, and we must have a PWM source; either raw from
* FMU or from the mixer.
*
*/
should_arm = (
/* IO initialised without error */ (r_status_flags & PX4IO_P_STATUS_FLAGS_INIT_OK)
/* and IO is armed */ && (r_status_flags & PX4IO_P_STATUS_FLAGS_SAFETY_OFF)
/* and FMU is armed */ && (
((r_setup_arming & PX4IO_P_SETUP_ARMING_FMU_ARMED)
/* and there is valid input via or mixer */ && (r_status_flags & PX4IO_P_STATUS_FLAGS_MIXER_OK) )
/* or direct PWM is set */ || (r_status_flags & PX4IO_P_STATUS_FLAGS_RAW_PWM)
/* or failsafe was set manually */ || ((r_setup_arming & PX4IO_P_SETUP_ARMING_FAILSAFE_CUSTOM) && !(r_status_flags & PX4IO_P_STATUS_FLAGS_FMU_OK))
)
);
should_always_enable_pwm = (r_setup_arming & PX4IO_P_SETUP_ARMING_ALWAYS_PWM_ENABLE)
&& (r_status_flags & PX4IO_P_STATUS_FLAGS_INIT_OK)
&& (r_status_flags & PX4IO_P_STATUS_FLAGS_FMU_OK);
/*
* Check if failsafe termination is set - if yes,
* set the force failsafe flag once entering the first
* failsafe condition.
*/
if ( /* if we have requested flight termination style failsafe (noreturn) */
(r_setup_arming & PX4IO_P_SETUP_ARMING_TERMINATION_FAILSAFE) &&
/* and we ended up in a failsafe condition */
(source == MIX_FAILSAFE) &&
/* and we should be armed, so we intended to provide outputs */
should_arm &&
/* and FMU is initialized */
(r_status_flags & PX4IO_P_STATUS_FLAGS_FMU_INITIALIZED)) {
r_setup_arming |= PX4IO_P_SETUP_ARMING_FORCE_FAILSAFE;
}
/*
* Check if we should force failsafe - and do it if we have to
*/
if (r_setup_arming & PX4IO_P_SETUP_ARMING_FORCE_FAILSAFE) {
source = MIX_FAILSAFE;
}
/*
* Set failsafe status flag depending on mixing source
*/
if (source == MIX_FAILSAFE) {
r_status_flags |= PX4IO_P_STATUS_FLAGS_FAILSAFE;
} else {
r_status_flags &= ~(PX4IO_P_STATUS_FLAGS_FAILSAFE);
}
/*
* Run the mixers.
*/
if (source == MIX_FAILSAFE) {
/* copy failsafe values to the servo outputs */
for (unsigned i = 0; i < PX4IO_SERVO_COUNT; i++) {
r_page_servos[i] = r_page_servo_failsafe[i];
/* safe actuators for FMU feedback */
r_page_actuators[i] = FLOAT_TO_REG((r_page_servos[i] - 1500) / 600.0f);
}
} else if (source != MIX_NONE && (r_status_flags & PX4IO_P_STATUS_FLAGS_MIXER_OK)) {
float outputs[PX4IO_SERVO_COUNT];
unsigned mixed;
/* mix */
/* poor mans mutex */
in_mixer = true;
mixed = mixer_group.mix(&outputs[0], PX4IO_SERVO_COUNT);
in_mixer = false;
/* the pwm limit call takes care of out of band errors */
pwm_limit_calc(should_arm, mixed, r_page_servo_disarmed, r_page_servo_control_min, r_page_servo_control_max, outputs, r_page_servos, &pwm_limit);
for (unsigned i = mixed; i < PX4IO_SERVO_COUNT; i++)
r_page_servos[i] = 0;
for (unsigned i = 0; i < PX4IO_SERVO_COUNT; i++) {
r_page_actuators[i] = FLOAT_TO_REG(outputs[i]);
}
}
/* set arming */
bool needs_to_arm = (should_arm || should_always_enable_pwm);
/* check any conditions that prevent arming */
if (r_setup_arming & PX4IO_P_SETUP_ARMING_LOCKDOWN) {
needs_to_arm = false;
}
if (!should_arm && !should_always_enable_pwm) {
needs_to_arm = false;
}
if (needs_to_arm && !mixer_servos_armed) {
/* need to arm, but not armed */
up_pwm_servo_arm(true);
mixer_servos_armed = true;
r_status_flags |= PX4IO_P_STATUS_FLAGS_OUTPUTS_ARMED;
isr_debug(5, "> PWM enabled");
} else if (!needs_to_arm && mixer_servos_armed) {
/* armed but need to disarm */
up_pwm_servo_arm(false);
mixer_servos_armed = false;
r_status_flags &= ~(PX4IO_P_STATUS_FLAGS_OUTPUTS_ARMED);
isr_debug(5, "> PWM disabled");
}
if (mixer_servos_armed && should_arm) {
/* update the servo outputs. */
for (unsigned i = 0; i < PX4IO_SERVO_COUNT; i++)
up_pwm_servo_set(i, r_page_servos[i]);
/* set S.BUS1 or S.BUS2 outputs */
if (r_setup_features & PX4IO_P_SETUP_FEATURES_SBUS2_OUT) {
sbus2_output(r_page_servos, PX4IO_SERVO_COUNT);
} else if (r_setup_features & PX4IO_P_SETUP_FEATURES_SBUS1_OUT) {
sbus1_output(r_page_servos, PX4IO_SERVO_COUNT);
}
} else if (mixer_servos_armed && should_always_enable_pwm) {
/* set the disarmed servo outputs. */
for (unsigned i = 0; i < PX4IO_SERVO_COUNT; i++)
up_pwm_servo_set(i, r_page_servo_disarmed[i]);
/* set S.BUS1 or S.BUS2 outputs */
if (r_setup_features & PX4IO_P_SETUP_FEATURES_SBUS1_OUT)
sbus1_output(r_page_servos, PX4IO_SERVO_COUNT);
if (r_setup_features & PX4IO_P_SETUP_FEATURES_SBUS2_OUT)
sbus2_output(r_page_servos, PX4IO_SERVO_COUNT);
}
}
void
Navigator::task_main()
{
bool have_geofence_position_data = false;
/* Try to load the geofence:
* if /fs/microsd/etc/geofence.txt load from this file
* else clear geofence data in datamanager */
struct stat buffer;
if (stat(GEOFENCE_FILENAME, &buffer) == 0) {
PX4_INFO("Try to load geofence.txt");
_geofence.loadFromFile(GEOFENCE_FILENAME);
} else {
if (_geofence.clearDm() != OK) {
mavlink_log_critical(&_mavlink_log_pub, "failed clearing geofence");
}
}
/* do subscriptions */
_global_pos_sub = orb_subscribe(ORB_ID(vehicle_global_position));
_local_pos_sub = orb_subscribe(ORB_ID(vehicle_local_position));
_gps_pos_sub = orb_subscribe(ORB_ID(vehicle_gps_position));
_sensor_combined_sub = orb_subscribe(ORB_ID(sensor_combined));
_fw_pos_ctrl_status_sub = orb_subscribe(ORB_ID(fw_pos_ctrl_status));
_vstatus_sub = orb_subscribe(ORB_ID(vehicle_status));
_land_detected_sub = orb_subscribe(ORB_ID(vehicle_land_detected));
_home_pos_sub = orb_subscribe(ORB_ID(home_position));
_onboard_mission_sub = orb_subscribe(ORB_ID(onboard_mission));
_offboard_mission_sub = orb_subscribe(ORB_ID(offboard_mission));
_param_update_sub = orb_subscribe(ORB_ID(parameter_update));
_vehicle_command_sub = orb_subscribe(ORB_ID(vehicle_command));
/* copy all topics first time */
vehicle_status_update();
vehicle_land_detected_update();
global_position_update();
local_position_update();
gps_position_update();
sensor_combined_update();
home_position_update(true);
fw_pos_ctrl_status_update(true);
params_update();
/* wakeup source(s) */
px4_pollfd_struct_t fds[1] = {};
/* Setup of loop */
fds[0].fd = _global_pos_sub;
fds[0].events = POLLIN;
bool global_pos_available_once = false;
/* rate-limit global pos subscription to 20 Hz / 50 ms */
orb_set_interval(_global_pos_sub, 49);
while (!_task_should_exit) {
/* wait for up to 1000ms for data */
int pret = px4_poll(&fds[0], (sizeof(fds) / sizeof(fds[0])), 1000);
if (pret == 0) {
/* timed out - periodic check for _task_should_exit, etc. */
if (global_pos_available_once) {
global_pos_available_once = false;
PX4_WARN("global position timeout");
}
/* Let the loop run anyway, don't do `continue` here. */
} else if (pret < 0) {
/* this is undesirable but not much we can do - might want to flag unhappy status */
PX4_ERR("nav: poll error %d, %d", pret, errno);
usleep(10000);
continue;
} else {
if (fds[0].revents & POLLIN) {
/* success, global pos is available */
global_position_update();
if (_geofence.getSource() == Geofence::GF_SOURCE_GLOBALPOS) {
have_geofence_position_data = true;
}
global_pos_available_once = true;
}
}
perf_begin(_loop_perf);
bool updated;
/* gps updated */
orb_check(_gps_pos_sub, &updated);
if (updated) {
gps_position_update();
if (_geofence.getSource() == Geofence::GF_SOURCE_GPS) {
have_geofence_position_data = true;
}
}
/* local position updated */
orb_check(_local_pos_sub, &updated);
if (updated) {
local_position_update();
}
/* sensors combined updated */
orb_check(_sensor_combined_sub, &updated);
if (updated) {
sensor_combined_update();
}
/* parameters updated */
orb_check(_param_update_sub, &updated);
if (updated) {
params_update();
}
/* vehicle status updated */
orb_check(_vstatus_sub, &updated);
if (updated) {
vehicle_status_update();
}
/* vehicle land detected updated */
orb_check(_land_detected_sub, &updated);
if (updated) {
vehicle_land_detected_update();
}
/* navigation capabilities updated */
orb_check(_fw_pos_ctrl_status_sub, &updated);
if (updated) {
fw_pos_ctrl_status_update();
}
/* home position updated */
orb_check(_home_pos_sub, &updated);
if (updated) {
home_position_update();
}
orb_check(_vehicle_command_sub, &updated);
if (updated) {
vehicle_command_s cmd = {};
orb_copy(ORB_ID(vehicle_command), _vehicle_command_sub, &cmd);
if (cmd.command == vehicle_command_s::VEHICLE_CMD_DO_REPOSITION) {
struct position_setpoint_triplet_s *rep = get_reposition_triplet();
// store current position as previous position and goal as next
rep->previous.yaw = get_global_position()->yaw;
rep->previous.lat = get_global_position()->lat;
rep->previous.lon = get_global_position()->lon;
rep->previous.alt = get_global_position()->alt;
rep->current.loiter_radius = get_loiter_radius();
rep->current.loiter_direction = 1;
rep->current.type = position_setpoint_s::SETPOINT_TYPE_LOITER;
// Go on and check which changes had been requested
if (PX4_ISFINITE(cmd.param4)) {
rep->current.yaw = cmd.param4;
} else {
rep->current.yaw = NAN;
}
if (PX4_ISFINITE(cmd.param5) && PX4_ISFINITE(cmd.param6)) {
rep->current.lat = (cmd.param5 < 1000) ? cmd.param5 : cmd.param5 / (double)1e7;
rep->current.lon = (cmd.param6 < 1000) ? cmd.param6 : cmd.param6 / (double)1e7;
} else {
rep->current.lat = get_global_position()->lat;
rep->current.lon = get_global_position()->lon;
}
if (PX4_ISFINITE(cmd.param7)) {
rep->current.alt = cmd.param7;
} else {
rep->current.alt = get_global_position()->alt;
}
rep->previous.valid = true;
rep->current.valid = true;
rep->next.valid = false;
} else if (cmd.command == vehicle_command_s::VEHICLE_CMD_NAV_TAKEOFF) {
struct position_setpoint_triplet_s *rep = get_takeoff_triplet();
// store current position as previous position and goal as next
rep->previous.yaw = get_global_position()->yaw;
rep->previous.lat = get_global_position()->lat;
rep->previous.lon = get_global_position()->lon;
rep->previous.alt = get_global_position()->alt;
rep->current.loiter_radius = get_loiter_radius();
rep->current.loiter_direction = 1;
rep->current.type = position_setpoint_s::SETPOINT_TYPE_TAKEOFF;
if (home_position_valid()) {
rep->current.yaw = cmd.param4;
rep->previous.valid = true;
} else {
rep->current.yaw = get_local_position()->yaw;
rep->previous.valid = false;
}
if (PX4_ISFINITE(cmd.param5) && PX4_ISFINITE(cmd.param6)) {
rep->current.lat = (cmd.param5 < 1000) ? cmd.param5 : cmd.param5 / (double)1e7;
rep->current.lon = (cmd.param6 < 1000) ? cmd.param6 : cmd.param6 / (double)1e7;
} else {
// If one of them is non-finite, reset both
rep->current.lat = NAN;
rep->current.lon = NAN;
}
rep->current.alt = cmd.param7;
rep->current.valid = true;
rep->next.valid = false;
} else if (cmd.command == vehicle_command_s::VEHICLE_CMD_DO_LAND_START) {
/* find NAV_CMD_DO_LAND_START in the mission and
* use MAV_CMD_MISSION_START to start the mission there
*/
int land_start = _mission.find_offboard_land_start();
if (land_start != -1) {
vehicle_command_s vcmd = {};
vcmd.target_system = get_vstatus()->system_id;
vcmd.target_component = get_vstatus()->component_id;
vcmd.command = vehicle_command_s::VEHICLE_CMD_MISSION_START;
vcmd.param1 = land_start;
vcmd.param2 = 0;
publish_vehicle_cmd(vcmd);
} else {
PX4_WARN("planned landing not available");
}
} else if (cmd.command == vehicle_command_s::VEHICLE_CMD_NAV_RETURN_TO_LAUNCH) {
vehicle_command_s vcmd = {};
vcmd.target_system = get_vstatus()->system_id;
vcmd.target_component = get_vstatus()->component_id;
vcmd.command = vehicle_command_s::VEHICLE_CMD_NAV_RETURN_TO_LAUNCH;
orb_advert_t pub = orb_advertise_queue(ORB_ID(vehicle_command), &vcmd, vehicle_command_s::ORB_QUEUE_LENGTH);
(void)orb_unadvertise(pub);
} else if (cmd.command == vehicle_command_s::VEHICLE_CMD_MISSION_START) {
if (get_mission_result()->valid &&
PX4_ISFINITE(cmd.param1) && (cmd.param1 >= 0) && (cmd.param1 < _mission_result.seq_total)) {
_mission.set_current_offboard_mission_index(cmd.param1);
}
} else if (cmd.command == vehicle_command_s::VEHICLE_CMD_DO_PAUSE_CONTINUE) {
warnx("navigator: got pause/continue command");
} else if (cmd.command == vehicle_command_s::VEHICLE_CMD_DO_CHANGE_SPEED) {
if (cmd.param2 > FLT_EPSILON) {
// XXX not differentiating ground and airspeed yet
set_cruising_speed(cmd.param2);
} else {
set_cruising_speed();
/* if no speed target was given try to set throttle */
if (cmd.param3 > FLT_EPSILON) {
set_cruising_throttle(cmd.param3 / 100);
} else {
set_cruising_throttle();
}
}
}
}
/* Check geofence violation */
static hrt_abstime last_geofence_check = 0;
if (have_geofence_position_data &&
(_geofence.getGeofenceAction() != geofence_result_s::GF_ACTION_NONE) &&
(hrt_elapsed_time(&last_geofence_check) > GEOFENCE_CHECK_INTERVAL)) {
bool inside = _geofence.inside(_global_pos, _gps_pos, _sensor_combined.baro_alt_meter);
last_geofence_check = hrt_absolute_time();
have_geofence_position_data = false;
_geofence_result.timestamp = hrt_absolute_time();
_geofence_result.geofence_action = _geofence.getGeofenceAction();
_geofence_result.home_required = _geofence.isHomeRequired();
if (!inside) {
/* inform other apps via the mission result */
_geofence_result.geofence_violated = true;
/* Issue a warning about the geofence violation once */
if (!_geofence_violation_warning_sent) {
mavlink_log_critical(&_mavlink_log_pub, "Geofence violation");
_geofence_violation_warning_sent = true;
}
} else {
/* inform other apps via the mission result */
_geofence_result.geofence_violated = false;
/* Reset the _geofence_violation_warning_sent field */
_geofence_violation_warning_sent = false;
}
publish_geofence_result();
}
/* Do stuff according to navigation state set by commander */
switch (_vstatus.nav_state) {
case vehicle_status_s::NAVIGATION_STATE_AUTO_MISSION:
_pos_sp_triplet_published_invalid_once = false;
_navigation_mode = &_mission;
break;
case vehicle_status_s::NAVIGATION_STATE_AUTO_LOITER:
_pos_sp_triplet_published_invalid_once = false;
_navigation_mode = &_loiter;
break;
case vehicle_status_s::NAVIGATION_STATE_AUTO_RCRECOVER:
_pos_sp_triplet_published_invalid_once = false;
_navigation_mode = &_rcLoss;
break;
case vehicle_status_s::NAVIGATION_STATE_AUTO_RTL:
_pos_sp_triplet_published_invalid_once = false;
_navigation_mode = &_rtl;
break;
case vehicle_status_s::NAVIGATION_STATE_AUTO_TAKEOFF:
_pos_sp_triplet_published_invalid_once = false;
_navigation_mode = &_takeoff;
break;
case vehicle_status_s::NAVIGATION_STATE_AUTO_LAND:
_pos_sp_triplet_published_invalid_once = false;
_navigation_mode = &_land;
break;
case vehicle_status_s::NAVIGATION_STATE_DESCEND:
_pos_sp_triplet_published_invalid_once = false;
_navigation_mode = &_land;
break;
case vehicle_status_s::NAVIGATION_STATE_AUTO_RTGS:
_pos_sp_triplet_published_invalid_once = false;
_navigation_mode = &_dataLinkLoss;
break;
case vehicle_status_s::NAVIGATION_STATE_AUTO_LANDENGFAIL:
_pos_sp_triplet_published_invalid_once = false;
_navigation_mode = &_engineFailure;
break;
case vehicle_status_s::NAVIGATION_STATE_AUTO_LANDGPSFAIL:
_pos_sp_triplet_published_invalid_once = false;
_navigation_mode = &_gpsFailure;
break;
case vehicle_status_s::NAVIGATION_STATE_AUTO_FOLLOW_TARGET:
_pos_sp_triplet_published_invalid_once = false;
_navigation_mode = &_follow_target;
break;
case vehicle_status_s::NAVIGATION_STATE_MANUAL:
case vehicle_status_s::NAVIGATION_STATE_ACRO:
case vehicle_status_s::NAVIGATION_STATE_ALTCTL:
case vehicle_status_s::NAVIGATION_STATE_POSCTL:
case vehicle_status_s::NAVIGATION_STATE_TERMINATION:
case vehicle_status_s::NAVIGATION_STATE_OFFBOARD:
case vehicle_status_s::NAVIGATION_STATE_STAB:
default:
_pos_sp_triplet_published_invalid_once = false;
_navigation_mode = nullptr;
_can_loiter_at_sp = false;
break;
}
/* iterate through navigation modes and set active/inactive for each */
for (unsigned int i = 0; i < NAVIGATOR_MODE_ARRAY_SIZE; i++) {
_navigation_mode_array[i]->run(_navigation_mode == _navigation_mode_array[i]);
}
/* if nothing is running, set position setpoint triplet invalid once */
if (_navigation_mode == nullptr && !_pos_sp_triplet_published_invalid_once) {
_pos_sp_triplet_published_invalid_once = true;
_pos_sp_triplet.previous.valid = false;
_pos_sp_triplet.current.valid = false;
_pos_sp_triplet.next.valid = false;
_pos_sp_triplet_updated = true;
}
if (_pos_sp_triplet_updated) {
_pos_sp_triplet.timestamp = hrt_absolute_time();
publish_position_setpoint_triplet();
_pos_sp_triplet_updated = false;
}
if (_mission_result_updated) {
publish_mission_result();
_mission_result_updated = false;
}
perf_end(_loop_perf);
}
PX4_INFO("exiting");
_navigator_task = -1;
}
void
controls_tick() {
/*
* Gather R/C control inputs from supported sources.
*
* Note that if you're silly enough to connect more than
* one control input source, they're going to fight each
* other. Don't do that.
*/
/* receive signal strenght indicator (RSSI). 0 = no connection, 255: perfect connection */
uint16_t rssi = 0;
#ifdef ADC_RSSI
if (r_setup_features & PX4IO_P_SETUP_FEATURES_ADC_RSSI) {
unsigned counts = adc_measure(ADC_RSSI);
if (counts != 0xffff) {
/* use 1:1 scaling on 3.3V ADC input */
unsigned mV = counts * 3300 / 4096;
/* scale to 0..253 */
rssi = mV / 13;
}
}
#endif
// perf_begin(c_gather_dsm);
// uint16_t temp_count = r_raw_rc_count;
// bool dsm_updated = dsm_input(r_raw_rc_values, &temp_count);
// if (dsm_updated) {
// r_raw_rc_flags |= PX4IO_P_STATUS_FLAGS_RC_DSM;
// r_raw_rc_count = temp_count & 0x7fff;
// if (temp_count & 0x8000)
// r_raw_rc_flags |= PX4IO_P_RAW_RC_FLAGS_RC_DSM11;
// else
// r_raw_rc_flags &= ~PX4IO_P_RAW_RC_FLAGS_RC_DSM11;
//
// r_raw_rc_flags &= ~(PX4IO_P_RAW_RC_FLAGS_FRAME_DROP);
// r_raw_rc_flags &= ~(PX4IO_P_RAW_RC_FLAGS_FAILSAFE);
//
// }
// perf_end(c_gather_dsm);
perf_begin(c_gather_sbus);
bool sbus_status = (r_status_flags & PX4IO_P_STATUS_FLAGS_RC_SBUS);
bool sbus_failsafe, sbus_frame_drop;
bool sbus_updated = sbus_input(r_raw_rc_values, &r_raw_rc_count, &sbus_failsafe, &sbus_frame_drop, PX4IO_RC_INPUT_CHANNELS);
if (sbus_updated) {
r_status_flags |= PX4IO_P_STATUS_FLAGS_RC_SBUS;
rssi = 255;
if (sbus_frame_drop) {
r_raw_rc_flags |= PX4IO_P_RAW_RC_FLAGS_FRAME_DROP;
rssi = 100;
} else {
r_raw_rc_flags &= ~(PX4IO_P_RAW_RC_FLAGS_FRAME_DROP);
}
if (sbus_failsafe) {
r_raw_rc_flags |= PX4IO_P_RAW_RC_FLAGS_FAILSAFE;
rssi = 0;
} else {
r_raw_rc_flags &= ~(PX4IO_P_RAW_RC_FLAGS_FAILSAFE);
}
}
perf_end(c_gather_sbus);
/*
* XXX each S.bus frame will cause a PPM decoder interrupt
* storm (lots of edges). It might be sensible to actually
* disable the PPM decoder completely if we have S.bus signal.
*/
perf_begin(c_gather_ppm);
bool ppm_updated = ppm_input(r_raw_rc_values, &r_raw_rc_count, &r_page_raw_rc_input[PX4IO_P_RAW_RC_DATA]);
if (ppm_updated) {
r_status_flags |= PX4IO_P_STATUS_FLAGS_RC_PPM;
r_raw_rc_flags &= ~(PX4IO_P_RAW_RC_FLAGS_FRAME_DROP);
r_raw_rc_flags &= ~(PX4IO_P_RAW_RC_FLAGS_FAILSAFE);
}
perf_end(c_gather_ppm);
/* limit number of channels to allowable data size */
if (r_raw_rc_count > PX4IO_RC_INPUT_CHANNELS)
r_raw_rc_count = PX4IO_RC_INPUT_CHANNELS;
/* store RSSI */
r_page_raw_rc_input[PX4IO_P_RAW_RC_NRSSI] = rssi;
/*
* In some cases we may have received a frame, but input has still
* been lost.
*/
bool rc_input_lost = false;
/*
* If we received a new frame from any of the RC sources, process it.
*/
// if (dsm_updated || sbus_updated || ppm_updated) {
if (sbus_updated || ppm_updated) {
/* record a bitmask of channels assigned */
unsigned assigned_channels = 0;
/* update RC-received timestamp */
system_state.rc_channels_timestamp_received = hrt_absolute_time();
/* do not command anything in failsafe, kick in the RC loss counter */
if (!(r_raw_rc_flags & PX4IO_P_RAW_RC_FLAGS_FAILSAFE)) {
/* update RC-received timestamp */
system_state.rc_channels_timestamp_valid = system_state.rc_channels_timestamp_received;
/* map raw inputs to mapped inputs */
/* XXX mapping should be atomic relative to protocol */
for (unsigned i = 0; i < r_raw_rc_count; i++) {
/* map the input channel */
uint16_t *conf = &r_page_rc_input_config[i * PX4IO_P_RC_CONFIG_STRIDE];
if (conf[PX4IO_P_RC_CONFIG_OPTIONS] & PX4IO_P_RC_CONFIG_OPTIONS_ENABLED) {
uint16_t raw = r_raw_rc_values[i];
int16_t scaled;
/*
* 1) Constrain to min/max values, as later processing depends on bounds.
*/
if (raw < conf[PX4IO_P_RC_CONFIG_MIN])
raw = conf[PX4IO_P_RC_CONFIG_MIN];
if (raw > conf[PX4IO_P_RC_CONFIG_MAX])
raw = conf[PX4IO_P_RC_CONFIG_MAX];
/*
* 2) Scale around the mid point differently for lower and upper range.
*
* This is necessary as they don't share the same endpoints and slope.
*
* First normalize to 0..1 range with correct sign (below or above center),
* then scale to 20000 range (if center is an actual center, -10000..10000,
* if parameters only support half range, scale to 10000 range, e.g. if
* center == min 0..10000, if center == max -10000..0).
*
* As the min and max bounds were enforced in step 1), division by zero
* cannot occur, as for the case of center == min or center == max the if
* statement is mutually exclusive with the arithmetic NaN case.
*
* DO NOT REMOVE OR ALTER STEP 1!
*/
if (raw > (conf[PX4IO_P_RC_CONFIG_CENTER] + conf[PX4IO_P_RC_CONFIG_DEADZONE])) {
scaled = 10000.0f * ((raw - conf[PX4IO_P_RC_CONFIG_CENTER] - conf[PX4IO_P_RC_CONFIG_DEADZONE]) / (float)(conf[PX4IO_P_RC_CONFIG_MAX] - conf[PX4IO_P_RC_CONFIG_CENTER] - conf[PX4IO_P_RC_CONFIG_DEADZONE]));
} else if (raw < (conf[PX4IO_P_RC_CONFIG_CENTER] - conf[PX4IO_P_RC_CONFIG_DEADZONE])) {
scaled = 10000.0f * ((raw - conf[PX4IO_P_RC_CONFIG_CENTER] + conf[PX4IO_P_RC_CONFIG_DEADZONE]) / (float)(conf[PX4IO_P_RC_CONFIG_CENTER] - conf[PX4IO_P_RC_CONFIG_DEADZONE] - conf[PX4IO_P_RC_CONFIG_MIN]));
} else {
/* in the configured dead zone, output zero */
scaled = 0;
}
/* invert channel if requested */
if (conf[PX4IO_P_RC_CONFIG_OPTIONS] & PX4IO_P_RC_CONFIG_OPTIONS_REVERSE)
scaled = -scaled;
/* and update the scaled/mapped version */
unsigned mapped = conf[PX4IO_P_RC_CONFIG_ASSIGNMENT];
if (mapped < PX4IO_CONTROL_CHANNELS) {
/* invert channel if pitch - pulling the lever down means pitching up by convention */
if (mapped == 1) /* roll, pitch, yaw, throttle, override is the standard order */
scaled = -scaled;
r_rc_values[mapped] = SIGNED_TO_REG(scaled);
assigned_channels |= (1 << mapped);
}
}
}
/* set un-assigned controls to zero */
for (unsigned i = 0; i < PX4IO_CONTROL_CHANNELS; i++) {
if (!(assigned_channels & (1 << i)))
r_rc_values[i] = 0;
}
/* set RC OK flag, as we got an update */
r_status_flags |= PX4IO_P_STATUS_FLAGS_RC_OK;
/* if we have enough channels (5) to control the vehicle, the mapping is ok */
if (assigned_channels > 4) {
r_raw_rc_flags |= PX4IO_P_RAW_RC_FLAGS_MAPPING_OK;
} else {
r_raw_rc_flags &= ~(PX4IO_P_RAW_RC_FLAGS_MAPPING_OK);
}
}
/*
* Export the valid channel bitmap
*/
r_rc_valid = assigned_channels;
}
/*
* If we haven't seen any new control data in 200ms, assume we
* have lost input.
*/
if (hrt_elapsed_time(&system_state.rc_channels_timestamp_received) > 200000) {
rc_input_lost = true;
/* clear the input-kind flags here */
r_status_flags &= ~(
PX4IO_P_STATUS_FLAGS_RC_PPM |
PX4IO_P_STATUS_FLAGS_RC_DSM |
PX4IO_P_STATUS_FLAGS_RC_SBUS);
}
/*
* Handle losing RC input
*/
/* this kicks in if the receiver is gone or the system went to failsafe */
if (rc_input_lost || (r_raw_rc_flags & PX4IO_P_RAW_RC_FLAGS_FAILSAFE)) {
/* Clear the RC input status flag, clear manual override flag */
r_status_flags &= ~(
PX4IO_P_STATUS_FLAGS_OVERRIDE |
PX4IO_P_STATUS_FLAGS_RC_OK);
/* Mark all channels as invalid, as we just lost the RX */
r_rc_valid = 0;
/* Set the RC_LOST alarm */
r_status_alarms |= PX4IO_P_STATUS_ALARMS_RC_LOST;
}
/* this kicks in if the receiver is completely gone */
if (rc_input_lost) {
/* Set channel count to zero */
r_raw_rc_count = 0;
}
/*
* Check for manual override.
*
* The PX4IO_P_SETUP_ARMING_MANUAL_OVERRIDE_OK flag must be set, and we
* must have R/C input.
* Override is enabled if either the hardcoded channel / value combination
* is selected, or the AP has requested it.
*/
if ((r_setup_arming & PX4IO_P_SETUP_ARMING_MANUAL_OVERRIDE_OK) &&
(r_status_flags & PX4IO_P_STATUS_FLAGS_RC_OK)) {
bool override = false;
/*
* Check mapped channel 5 (can be any remote channel,
* depends on RC_MAP_OVER parameter);
* If the value is 'high' then the pilot has
* requested override.
*
*/
if ((r_status_flags & PX4IO_P_STATUS_FLAGS_RC_OK) && (REG_TO_SIGNED(r_rc_values[4]) < RC_CHANNEL_LOW_THRESH))
override = true;
if (override) {
r_status_flags |= PX4IO_P_STATUS_FLAGS_OVERRIDE;
/* mix new RC input control values to servos */
// if (dsm_updated || sbus_updated || ppm_updated)
// mixer_tick();
} else {
int
SF0X::collect()
{
int ret;
perf_begin(_sample_perf);
/* clear buffer if last read was too long ago */
uint64_t read_elapsed = hrt_elapsed_time(&_last_read);
/* the buffer for read chars is buflen minus null termination */
char readbuf[sizeof(_linebuf)];
unsigned readlen = sizeof(readbuf) - 1;
/* read from the sensor (uart buffer) */
ret = ::read(_fd, &readbuf[0], readlen);
if (ret < 0) {
DEVICE_DEBUG("read err: %d", ret);
perf_count(_comms_errors);
perf_end(_sample_perf);
/* only throw an error if we time out */
if (read_elapsed > (_conversion_interval * 2)) {
return ret;
} else {
return -EAGAIN;
}
} else if (ret == 0) {
return -EAGAIN;
}
_last_read = hrt_absolute_time();
float distance_m = -1.0f;
bool valid = false;
for (int i = 0; i < ret; i++) {
if (OK == sf0x_parser(readbuf[i], _linebuf, &_linebuf_index, &_parse_state, &distance_m)) {
valid = true;
}
}
if (!valid) {
return -EAGAIN;
}
DEVICE_DEBUG("val (float): %8.4f, raw: %s, valid: %s", (double)distance_m, _linebuf, ((valid) ? "OK" : "NO"));
struct distance_sensor_s report;
report.timestamp = hrt_absolute_time();
report.type = distance_sensor_s::MAV_DISTANCE_SENSOR_LASER;
report.orientation = _rotation;
report.current_distance = distance_m;
report.min_distance = get_minimum_distance();
report.max_distance = get_maximum_distance();
report.covariance = 0.0f;
/* TODO: set proper ID */
report.id = 0;
/* publish it */
orb_publish(ORB_ID(distance_sensor), _distance_sensor_topic, &report);
_reports->force(&report);
/* notify anyone waiting for data */
poll_notify(POLLIN);
ret = OK;
perf_end(_sample_perf);
return ret;
}
void
FixedwingAttitudeControl::task_main()
{
/*
* do subscriptions
*/
_att_sp_sub = orb_subscribe(ORB_ID(vehicle_attitude_setpoint));
_att_sub = orb_subscribe(ORB_ID(vehicle_attitude));
_accel_sub = orb_subscribe_multi(ORB_ID(sensor_accel), 0);
_airspeed_sub = orb_subscribe(ORB_ID(airspeed));
_vcontrol_mode_sub = orb_subscribe(ORB_ID(vehicle_control_mode));
_params_sub = orb_subscribe(ORB_ID(parameter_update));
_manual_sub = orb_subscribe(ORB_ID(manual_control_setpoint));
_global_pos_sub = orb_subscribe(ORB_ID(vehicle_global_position));
_vehicle_status_sub = orb_subscribe(ORB_ID(vehicle_status));
/* rate limit vehicle status updates to 5Hz */
orb_set_interval(_vcontrol_mode_sub, 200);
/* do not limit the attitude updates in order to minimize latency.
* actuator outputs are still limited by the individual drivers
* properly to not saturate IO or physical limitations */
parameters_update();
/* get an initial update for all sensor and status data */
vehicle_airspeed_poll();
vehicle_setpoint_poll();
vehicle_accel_poll();
vehicle_control_mode_poll();
vehicle_manual_poll();
vehicle_status_poll();
/* wakeup source(s) */
struct pollfd fds[2];
/* Setup of loop */
fds[0].fd = _params_sub;
fds[0].events = POLLIN;
fds[1].fd = _att_sub;
fds[1].events = POLLIN;
_task_running = true;
while (!_task_should_exit) {
static int loop_counter = 0;
/* wait for up to 500ms for data */
int pret = poll(&fds[0], (sizeof(fds) / sizeof(fds[0])), 100);
/* timed out - periodic check for _task_should_exit, etc. */
if (pret == 0)
continue;
/* this is undesirable but not much we can do - might want to flag unhappy status */
if (pret < 0) {
warn("poll error %d, %d", pret, errno);
continue;
}
perf_begin(_loop_perf);
/* only update parameters if they changed */
if (fds[0].revents & POLLIN) {
/* read from param to clear updated flag */
struct parameter_update_s update;
orb_copy(ORB_ID(parameter_update), _params_sub, &update);
/* update parameters from storage */
parameters_update();
}
/* only run controller if attitude changed */
if (fds[1].revents & POLLIN) {
static uint64_t last_run = 0;
float deltaT = (hrt_absolute_time() - last_run) / 1000000.0f;
last_run = hrt_absolute_time();
/* guard against too large deltaT's */
if (deltaT > 1.0f)
deltaT = 0.01f;
/* load local copies */
orb_copy(ORB_ID(vehicle_attitude), _att_sub, &_att);
if (_vehicle_status.is_vtol && _parameters.vtol_type == 0) {
/* vehicle is a tailsitter, we need to modify the estimated attitude for fw mode
*
* Since the VTOL airframe is initialized as a multicopter we need to
* modify the estimated attitude for the fixed wing operation.
* Since the neutral position of the vehicle in fixed wing mode is -90 degrees rotated around
* the pitch axis compared to the neutral position of the vehicle in multicopter mode
* we need to swap the roll and the yaw axis (1st and 3rd column) in the rotation matrix.
* Additionally, in order to get the correct sign of the pitch, we need to multiply
* the new x axis of the rotation matrix with -1
*
* original: modified:
*
* Rxx Ryx Rzx -Rzx Ryx Rxx
* Rxy Ryy Rzy -Rzy Ryy Rxy
* Rxz Ryz Rzz -Rzz Ryz Rxz
* */
math::Matrix<3, 3> R; //original rotation matrix
math::Matrix<3, 3> R_adapted; //modified rotation matrix
R.set(_att.R);
R_adapted.set(_att.R);
/* move z to x */
R_adapted(0, 0) = R(0, 2);
R_adapted(1, 0) = R(1, 2);
R_adapted(2, 0) = R(2, 2);
/* move x to z */
R_adapted(0, 2) = R(0, 0);
R_adapted(1, 2) = R(1, 0);
R_adapted(2, 2) = R(2, 0);
/* change direction of pitch (convert to right handed system) */
R_adapted(0, 0) = -R_adapted(0, 0);
R_adapted(1, 0) = -R_adapted(1, 0);
R_adapted(2, 0) = -R_adapted(2, 0);
math::Vector<3> euler_angles; //adapted euler angles for fixed wing operation
euler_angles = R_adapted.to_euler();
/* fill in new attitude data */
_att.roll = euler_angles(0);
_att.pitch = euler_angles(1);
_att.yaw = euler_angles(2);
PX4_R(_att.R, 0, 0) = R_adapted(0, 0);
PX4_R(_att.R, 0, 1) = R_adapted(0, 1);
PX4_R(_att.R, 0, 2) = R_adapted(0, 2);
PX4_R(_att.R, 1, 0) = R_adapted(1, 0);
PX4_R(_att.R, 1, 1) = R_adapted(1, 1);
PX4_R(_att.R, 1, 2) = R_adapted(1, 2);
PX4_R(_att.R, 2, 0) = R_adapted(2, 0);
PX4_R(_att.R, 2, 1) = R_adapted(2, 1);
PX4_R(_att.R, 2, 2) = R_adapted(2, 2);
/* lastly, roll- and yawspeed have to be swaped */
float helper = _att.rollspeed;
_att.rollspeed = -_att.yawspeed;
_att.yawspeed = helper;
}
vehicle_airspeed_poll();
vehicle_setpoint_poll();
vehicle_accel_poll();
vehicle_control_mode_poll();
vehicle_manual_poll();
global_pos_poll();
vehicle_status_poll();
/* lock integrator until control is started */
bool lock_integrator;
if (_vcontrol_mode.flag_control_attitude_enabled && !_vehicle_status.is_rotary_wing) {
lock_integrator = false;
} else {
lock_integrator = true;
}
/* Simple handling of failsafe: deploy parachute if failsafe is on */
if (_vcontrol_mode.flag_control_termination_enabled) {
_actuators_airframe.control[7] = 1.0f;
//warnx("_actuators_airframe.control[1] = 1.0f;");
} else {
_actuators_airframe.control[7] = 0.0f;
//warnx("_actuators_airframe.control[1] = -1.0f;");
}
/* if we are in rotary wing mode, do nothing */
if (_vehicle_status.is_rotary_wing) {
continue;
}
/* default flaps to center */
float flaps_control = 0.0f;
/* map flaps by default to manual if valid */
if (isfinite(_manual.flaps)) {
flaps_control = _manual.flaps;
}
/* decide if in stabilized or full manual control */
if (_vcontrol_mode.flag_control_attitude_enabled) {
/* scale around tuning airspeed */
float airspeed;
/* if airspeed is not updating, we assume the normal average speed */
if (bool nonfinite = !isfinite(_airspeed.true_airspeed_m_s) ||
hrt_elapsed_time(&_airspeed.timestamp) > 1e6) {
airspeed = _parameters.airspeed_trim;
if (nonfinite) {
perf_count(_nonfinite_input_perf);
}
} else {
/* prevent numerical drama by requiring 0.5 m/s minimal speed */
airspeed = math::max(0.5f, _airspeed.true_airspeed_m_s);
}
/*
* For scaling our actuators using anything less than the min (close to stall)
* speed doesn't make any sense - its the strongest reasonable deflection we
* want to do in flight and its the baseline a human pilot would choose.
*
* Forcing the scaling to this value allows reasonable handheld tests.
*/
float airspeed_scaling = _parameters.airspeed_trim / ((airspeed < _parameters.airspeed_min) ? _parameters.airspeed_min : airspeed);
float roll_sp = _parameters.rollsp_offset_rad;
float pitch_sp = _parameters.pitchsp_offset_rad;
float yaw_manual = 0.0f;
float throttle_sp = 0.0f;
/* Read attitude setpoint from uorb if
* - velocity control or position control is enabled (pos controller is running)
* - manual control is disabled (another app may send the setpoint, but it should
* for sure not be set from the remote control values)
*/
if (_vcontrol_mode.flag_control_auto_enabled ||
!_vcontrol_mode.flag_control_manual_enabled) {
/* read in attitude setpoint from attitude setpoint uorb topic */
roll_sp = _att_sp.roll_body + _parameters.rollsp_offset_rad;
pitch_sp = _att_sp.pitch_body + _parameters.pitchsp_offset_rad;
throttle_sp = _att_sp.thrust;
/* reset integrals where needed */
if (_att_sp.roll_reset_integral) {
_roll_ctrl.reset_integrator();
}
if (_att_sp.pitch_reset_integral) {
_pitch_ctrl.reset_integrator();
}
if (_att_sp.yaw_reset_integral) {
_yaw_ctrl.reset_integrator();
}
} else if (_vcontrol_mode.flag_control_velocity_enabled) {
/* the pilot does not want to change direction,
* take straight attitude setpoint from position controller
*/
if (fabsf(_manual.y) < 0.01f && fabsf(_att.roll) < 0.2f) {
roll_sp = _att_sp.roll_body + _parameters.rollsp_offset_rad;
} else {
roll_sp = (_manual.y * _parameters.man_roll_max)
+ _parameters.rollsp_offset_rad;
}
pitch_sp = _att_sp.pitch_body + _parameters.pitchsp_offset_rad;
throttle_sp = _att_sp.thrust;
/* reset integrals where needed */
if (_att_sp.roll_reset_integral) {
_roll_ctrl.reset_integrator();
}
if (_att_sp.pitch_reset_integral) {
_pitch_ctrl.reset_integrator();
}
if (_att_sp.yaw_reset_integral) {
_yaw_ctrl.reset_integrator();
}
} else if (_vcontrol_mode.flag_control_altitude_enabled) {
/*
* Velocity should be controlled and manual is enabled.
*/
roll_sp = (_manual.y * _parameters.man_roll_max) + _parameters.rollsp_offset_rad;
pitch_sp = _att_sp.pitch_body + _parameters.pitchsp_offset_rad;
throttle_sp = _att_sp.thrust;
/* reset integrals where needed */
if (_att_sp.roll_reset_integral) {
_roll_ctrl.reset_integrator();
}
if (_att_sp.pitch_reset_integral) {
_pitch_ctrl.reset_integrator();
}
if (_att_sp.yaw_reset_integral) {
_yaw_ctrl.reset_integrator();
}
} else {
/*
* Scale down roll and pitch as the setpoints are radians
* and a typical remote can only do around 45 degrees, the mapping is
* -1..+1 to -man_roll_max rad..+man_roll_max rad (equivalent for pitch)
*
* With this mapping the stick angle is a 1:1 representation of
* the commanded attitude.
*
* The trim gets subtracted here from the manual setpoint to get
* the intended attitude setpoint. Later, after the rate control step the
* trim is added again to the control signal.
*/
roll_sp = (_manual.y * _parameters.man_roll_max) + _parameters.rollsp_offset_rad;
pitch_sp = -(_manual.x * _parameters.man_pitch_max) + _parameters.pitchsp_offset_rad;
/* allow manual control of rudder deflection */
yaw_manual = _manual.r;
throttle_sp = _manual.z;
/*
* in manual mode no external source should / does emit attitude setpoints.
* emit the manual setpoint here to allow attitude controller tuning
* in attitude control mode.
*/
struct vehicle_attitude_setpoint_s att_sp;
att_sp.timestamp = hrt_absolute_time();
att_sp.roll_body = roll_sp;
att_sp.pitch_body = pitch_sp;
att_sp.yaw_body = 0.0f - _parameters.trim_yaw;
att_sp.thrust = throttle_sp;
/* lazily publish the setpoint only once available */
if (!_vehicle_status.is_rotary_wing) {
if (_attitude_sp_pub != nullptr) {
/* publish the attitude setpoint */
orb_publish(ORB_ID(vehicle_attitude_setpoint), _attitude_sp_pub, &att_sp);
} else {
/* advertise and publish */
_attitude_sp_pub = orb_advertise(ORB_ID(vehicle_attitude_setpoint), &att_sp);
}
}
}
/* If the aircraft is on ground reset the integrators */
if (_vehicle_status.condition_landed || _vehicle_status.is_rotary_wing) {
_roll_ctrl.reset_integrator();
_pitch_ctrl.reset_integrator();
_yaw_ctrl.reset_integrator();
}
/* Prepare speed_body_u and speed_body_w */
float speed_body_u = 0.0f;
float speed_body_v = 0.0f;
float speed_body_w = 0.0f;
if(_att.R_valid) {
speed_body_u = PX4_R(_att.R, 0, 0) * _global_pos.vel_n + PX4_R(_att.R, 1, 0) * _global_pos.vel_e + PX4_R(_att.R, 2, 0) * _global_pos.vel_d;
speed_body_v = PX4_R(_att.R, 0, 1) * _global_pos.vel_n + PX4_R(_att.R, 1, 1) * _global_pos.vel_e + PX4_R(_att.R, 2, 1) * _global_pos.vel_d;
speed_body_w = PX4_R(_att.R, 0, 2) * _global_pos.vel_n + PX4_R(_att.R, 1, 2) * _global_pos.vel_e + PX4_R(_att.R, 2, 2) * _global_pos.vel_d;
} else {
if (_debug && loop_counter % 10 == 0) {
warnx("Did not get a valid R\n");
}
}
/* Prepare data for attitude controllers */
struct ECL_ControlData control_input = {};
control_input.roll = _att.roll;
control_input.pitch = _att.pitch;
control_input.yaw = _att.yaw;
control_input.roll_rate = _att.rollspeed;
control_input.pitch_rate = _att.pitchspeed;
control_input.yaw_rate = _att.yawspeed;
control_input.speed_body_u = speed_body_u;
control_input.speed_body_v = speed_body_v;
control_input.speed_body_w = speed_body_w;
control_input.acc_body_x = _accel.x;
control_input.acc_body_y = _accel.y;
control_input.acc_body_z = _accel.z;
control_input.roll_setpoint = roll_sp;
control_input.pitch_setpoint = pitch_sp;
control_input.airspeed_min = _parameters.airspeed_min;
control_input.airspeed_max = _parameters.airspeed_max;
control_input.airspeed = airspeed;
control_input.scaler = airspeed_scaling;
control_input.lock_integrator = lock_integrator;
/* Run attitude controllers */
if (isfinite(roll_sp) && isfinite(pitch_sp)) {
_roll_ctrl.control_attitude(control_input);
_pitch_ctrl.control_attitude(control_input);
_yaw_ctrl.control_attitude(control_input); //runs last, because is depending on output of roll and pitch attitude
/* Update input data for rate controllers */
control_input.roll_rate_setpoint = _roll_ctrl.get_desired_rate();
control_input.pitch_rate_setpoint = _pitch_ctrl.get_desired_rate();
control_input.yaw_rate_setpoint = _yaw_ctrl.get_desired_rate();
/* Run attitude RATE controllers which need the desired attitudes from above, add trim */
float roll_u = _roll_ctrl.control_bodyrate(control_input);
_actuators.control[0] = (isfinite(roll_u)) ? roll_u + _parameters.trim_roll : _parameters.trim_roll;
if (!isfinite(roll_u)) {
_roll_ctrl.reset_integrator();
perf_count(_nonfinite_output_perf);
if (_debug && loop_counter % 10 == 0) {
warnx("roll_u %.4f", (double)roll_u);
}
}
float pitch_u = _pitch_ctrl.control_bodyrate(control_input);
_actuators.control[1] = (isfinite(pitch_u)) ? pitch_u + _parameters.trim_pitch : _parameters.trim_pitch;
if (!isfinite(pitch_u)) {
_pitch_ctrl.reset_integrator();
perf_count(_nonfinite_output_perf);
if (_debug && loop_counter % 10 == 0) {
warnx("pitch_u %.4f, _yaw_ctrl.get_desired_rate() %.4f,"
" airspeed %.4f, airspeed_scaling %.4f,"
" roll_sp %.4f, pitch_sp %.4f,"
" _roll_ctrl.get_desired_rate() %.4f,"
" _pitch_ctrl.get_desired_rate() %.4f"
" att_sp.roll_body %.4f",
(double)pitch_u, (double)_yaw_ctrl.get_desired_rate(),
(double)airspeed, (double)airspeed_scaling,
(double)roll_sp, (double)pitch_sp,
(double)_roll_ctrl.get_desired_rate(),
(double)_pitch_ctrl.get_desired_rate(),
(double)_att_sp.roll_body);
}
}
float yaw_u = _yaw_ctrl.control_bodyrate(control_input);
_actuators.control[2] = (isfinite(yaw_u)) ? yaw_u + _parameters.trim_yaw : _parameters.trim_yaw;
/* add in manual rudder control */
_actuators.control[2] += yaw_manual;
if (!isfinite(yaw_u)) {
_yaw_ctrl.reset_integrator();
perf_count(_nonfinite_output_perf);
if (_debug && loop_counter % 10 == 0) {
warnx("yaw_u %.4f", (double)yaw_u);
}
}
/* throttle passed through if it is finite and if no engine failure was
* detected */
_actuators.control[3] = (isfinite(throttle_sp) &&
!(_vehicle_status.engine_failure ||
_vehicle_status.engine_failure_cmd)) ?
throttle_sp : 0.0f;
if (!isfinite(throttle_sp)) {
if (_debug && loop_counter % 10 == 0) {
warnx("throttle_sp %.4f", (double)throttle_sp);
}
}
} else {
perf_count(_nonfinite_input_perf);
if (_debug && loop_counter % 10 == 0) {
warnx("Non-finite setpoint roll_sp: %.4f, pitch_sp %.4f", (double)roll_sp, (double)pitch_sp);
}
}
/*
* Lazily publish the rate setpoint (for analysis, the actuators are published below)
* only once available
*/
_rates_sp.roll = _roll_ctrl.get_desired_rate();
_rates_sp.pitch = _pitch_ctrl.get_desired_rate();
_rates_sp.yaw = _yaw_ctrl.get_desired_rate();
_rates_sp.timestamp = hrt_absolute_time();
if (_rate_sp_pub != nullptr) {
/* publish the attitude rates setpoint */
orb_publish(_rates_sp_id, _rate_sp_pub, &_rates_sp);
} else if (_rates_sp_id) {
/* advertise the attitude rates setpoint */
_rate_sp_pub = orb_advertise(_rates_sp_id, &_rates_sp);
}
} else {
/* manual/direct control */
_actuators.control[actuator_controls_s::INDEX_ROLL] = _manual.y + _parameters.trim_roll;
_actuators.control[actuator_controls_s::INDEX_PITCH] = -_manual.x + _parameters.trim_pitch;
_actuators.control[actuator_controls_s::INDEX_YAW] = _manual.r + _parameters.trim_yaw;
_actuators.control[actuator_controls_s::INDEX_THROTTLE] = _manual.z;
}
_actuators.control[actuator_controls_s::INDEX_FLAPS] = flaps_control;
_actuators.control[5] = _manual.aux1;
_actuators.control[6] = _manual.aux2;
_actuators.control[7] = _manual.aux3;
/* lazily publish the setpoint only once available */
_actuators.timestamp = hrt_absolute_time();
_actuators.timestamp_sample = _att.timestamp;
_actuators_airframe.timestamp = hrt_absolute_time();
_actuators_airframe.timestamp_sample = _att.timestamp;
/* Only publish if any of the proper modes are enabled */
if(_vcontrol_mode.flag_control_rates_enabled ||
_vcontrol_mode.flag_control_attitude_enabled ||
_vcontrol_mode.flag_control_manual_enabled)
{
/* publish the actuator controls */
if (_actuators_0_pub != nullptr) {
orb_publish(_actuators_id, _actuators_0_pub, &_actuators);
} else if (_actuators_id) {
_actuators_0_pub= orb_advertise(_actuators_id, &_actuators);
}
if (_actuators_2_pub != nullptr) {
/* publish the actuator controls*/
orb_publish(ORB_ID(actuator_controls_2), _actuators_2_pub, &_actuators_airframe);
} else {
/* advertise and publish */
_actuators_2_pub = orb_advertise(ORB_ID(actuator_controls_2), &_actuators_airframe);
}
}
}
loop_counter++;
perf_end(_loop_perf);
}
warnx("exiting.\n");
_control_task = -1;
_task_running = false;
_exit(0);
}
int
SF0X::collect()
{
int ret;
perf_begin(_sample_perf);
/* clear buffer if last read was too long ago */
uint64_t read_elapsed = hrt_elapsed_time(&_last_read);
/* the buffer for read chars is buflen minus null termination */
char readbuf[sizeof(_linebuf)];
unsigned readlen = sizeof(readbuf) - 1;
/* read from the sensor (uart buffer) */
ret = ::read(_fd, &readbuf[0], readlen);
if (ret < 0) {
debug("read err: %d", ret);
perf_count(_comms_errors);
perf_end(_sample_perf);
/* only throw an error if we time out */
if (read_elapsed > (SF0X_CONVERSION_INTERVAL * 2)) {
return ret;
} else {
return -EAGAIN;
}
} else if (ret == 0) {
return -EAGAIN;
}
_last_read = hrt_absolute_time();
float si_units;
bool valid = false;
for (int i = 0; i < ret; i++) {
if (OK == sf0x_parser(readbuf[i], _linebuf, &_linebuf_index, &_parse_state, &si_units)) {
valid = true;
}
}
if (!valid) {
return -EAGAIN;
}
debug("val (float): %8.4f, raw: %s, valid: %s", (double)si_units, _linebuf, ((valid) ? "OK" : "NO"));
struct range_finder_report report;
/* this should be fairly close to the end of the measurement, so the best approximation of the time */
report.timestamp = hrt_absolute_time();
report.error_count = perf_event_count(_comms_errors);
report.distance = si_units;
report.minimum_distance = get_minimum_distance();
report.maximum_distance = get_maximum_distance();
report.valid = valid && (si_units > get_minimum_distance() && si_units < get_maximum_distance() ? 1 : 0);
/* publish it */
orb_publish(ORB_ID(sensor_range_finder), _range_finder_topic, &report);
if (_reports->force(&report)) {
perf_count(_buffer_overflows);
}
/* notify anyone waiting for data */
poll_notify(POLLIN);
ret = OK;
perf_end(_sample_perf);
return ret;
}
