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@ -559,61 +559,26 @@ FixedwingEstimator::check_filter_state()
@@ -559,61 +559,26 @@ FixedwingEstimator::check_filter_state()
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int check = _ekf->CheckAndBound(&ekf_report); |
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const char* ekfname = "att pos estimator: "; |
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switch (check) { |
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case 0: |
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/* all ok */ |
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break; |
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case 1: |
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{ |
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const char* str = "NaN in states, resetting"; |
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warnx("%s", str); |
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mavlink_log_critical(_mavlink_fd, "%s%s", ekfname, str); |
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break; |
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} |
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case 2: |
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{ |
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const char* str = "stale IMU data, resetting"; |
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warnx("%s", str); |
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mavlink_log_critical(_mavlink_fd, "%s%s", ekfname, str); |
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break; |
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} |
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case 3: |
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{ |
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const char* str = "switching to dynamic state"; |
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warnx("%s", str); |
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mavlink_log_info(_mavlink_fd, "%s%s", ekfname, str); |
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break; |
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} |
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case 4: |
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{ |
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const char* str = "excessive gyro offsets"; |
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warnx("%s", str); |
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mavlink_log_info(_mavlink_fd, "%s%s", ekfname, str); |
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break; |
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} |
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case 5: |
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{ |
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const char* str = "GPS velocity divergence"; |
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warnx("%s", str); |
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mavlink_log_info(_mavlink_fd, "%s%s", ekfname, str); |
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break; |
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} |
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case 6: |
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{ |
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const char* str = "excessive covariances"; |
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warnx("%s", str); |
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mavlink_log_info(_mavlink_fd, "%s%s", ekfname, str); |
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break; |
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const char* const feedback[] = { 0, |
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"NaN in states, resetting", |
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"stale IMU data, resetting", |
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"got initial position lock", |
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"excessive gyro offsets", |
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"GPS velocity divergence", |
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"excessive covariances", |
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"unknown condition"}; |
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// Print out error condition
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if (check) { |
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unsigned warn_index = static_cast<unsigned>(check); |
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unsigned max_warn_index = (sizeof(feedback) / sizeof(feedback[0])); |
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if (max_warn_index < warn_index) { |
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warn_index = max_warn_index; |
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} |
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default: |
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{ |
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const char* str = "unknown reset condition"; |
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warnx("%s", str); |
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mavlink_log_critical(_mavlink_fd, "%s%s", ekfname, str); |
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} |
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warnx("reset: %s", feedback[warn_index]); |
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mavlink_log_critical(_mavlink_fd, "[ekf] re-init: %s", feedback[warn_index]); |
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} |
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struct estimator_status_report rep; |
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@ -1140,20 +1105,6 @@ FixedwingEstimator::task_main()
@@ -1140,20 +1105,6 @@ FixedwingEstimator::task_main()
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float initVelNED[3]; |
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// Guard before running any parts of the filter
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// of NaN / invalid values
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if (_ekf->statesInitialised) { |
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// We're apparently initialized in this case now
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int check = check_filter_state(); |
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if (check) { |
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// Let the system re-initialize itself
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continue; |
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} |
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} |
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/* Initialize the filter first */ |
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if (!_gps_initialized && _gps.fix_type > 2 && _gps.eph < _parameters.pos_stddev_threshold && _gps.epv < _parameters.pos_stddev_threshold) { |
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@ -1216,8 +1167,17 @@ FixedwingEstimator::task_main()
@@ -1216,8 +1167,17 @@ FixedwingEstimator::task_main()
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_baro_gps_offset = 0.0f; |
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_ekf->InitialiseFilter(initVelNED, 0.0, 0.0, 0.0f, 0.0f); |
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} else if (_ekf->statesInitialised) { |
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// We're apparently initialized in this case now
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int check = check_filter_state(); |
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if (check) { |
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// Let the system re-initialize itself
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continue; |
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} |
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// Run the strapdown INS equations every IMU update
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_ekf->UpdateStrapdownEquationsNED(); |
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#if 0 |
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@ -1285,7 +1245,7 @@ FixedwingEstimator::task_main()
@@ -1285,7 +1245,7 @@ FixedwingEstimator::task_main()
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// run the fusion step
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_ekf->FuseVelposNED(); |
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} else if (!_gps_initialized && _ekf->statesInitialised) { |
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} else if (!_gps_initialized) { |
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// Convert GPS measurements to Pos NE, hgt and Vel NED
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_ekf->velNED[0] = 0.0f; |
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_ekf->velNED[1] = 0.0f; |
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@ -1307,7 +1267,7 @@ FixedwingEstimator::task_main()
@@ -1307,7 +1267,7 @@ FixedwingEstimator::task_main()
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_ekf->fusePosData = false; |
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} |
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if (newHgtData && _ekf->statesInitialised) { |
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if (newHgtData) { |
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// Could use a blend of GPS and baro alt data if desired
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_ekf->hgtMea = 1.0f * (_ekf->baroHgt - _baro_ref); |
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_ekf->fuseHgtData = true; |
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@ -1321,7 +1281,7 @@ FixedwingEstimator::task_main()
@@ -1321,7 +1281,7 @@ FixedwingEstimator::task_main()
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} |
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// Fuse Magnetometer Measurements
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if (newDataMag && _ekf->statesInitialised) { |
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if (newDataMag) { |
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_ekf->fuseMagData = true; |
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_ekf->RecallStates(_ekf->statesAtMagMeasTime, (IMUmsec - _parameters.mag_delay_ms)); // Assume 50 msec avg delay for magnetometer data
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@ -1335,7 +1295,7 @@ FixedwingEstimator::task_main()
@@ -1335,7 +1295,7 @@ FixedwingEstimator::task_main()
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} |
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// Fuse Airspeed Measurements
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if (newAdsData && _ekf->statesInitialised && _ekf->VtasMeas > 8.0f) { |
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if (newAdsData && _ekf->VtasMeas > 7.0f) { |
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_ekf->fuseVtasData = true; |
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_ekf->RecallStates(_ekf->statesAtVtasMeasTime, (IMUmsec - _parameters.tas_delay_ms)); // assume 100 msec avg delay for airspeed data
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_ekf->FuseAirspeed(); |
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@ -1403,7 +1363,7 @@ FixedwingEstimator::task_main()
@@ -1403,7 +1363,7 @@ FixedwingEstimator::task_main()
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_velocity_xy_filtered = 0.95f*_velocity_xy_filtered + 0.05f*sqrtf(_local_pos.vx*_local_pos.vx + _local_pos.vy*_local_pos.vy); |
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_velocity_z_filtered = 0.95f*_velocity_z_filtered + 0.05f*fabsf(_local_pos.vz); |
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_airspeed_filtered = 0.95f*_airspeed_filtered + + 0.05f*_airspeed.true_airspeed_m_s; |
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_airspeed_filtered = 0.95f*_airspeed_filtered + 0.05f*_airspeed.true_airspeed_m_s; |
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/* crude land detector for fixedwing only,
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@ -1494,27 +1454,28 @@ FixedwingEstimator::task_main()
@@ -1494,27 +1454,28 @@ FixedwingEstimator::task_main()
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} |
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} |
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} |
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if (hrt_elapsed_time(&_wind.timestamp) > 99000) { |
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_wind.timestamp = _global_pos.timestamp; |
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_wind.windspeed_north = _ekf->states[14]; |
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_wind.windspeed_east = _ekf->states[15]; |
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_wind.covariance_north = _ekf->P[14][14]; |
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_wind.covariance_east = _ekf->P[15][15]; |
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if (hrt_elapsed_time(&_wind.timestamp) > 99000) { |
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_wind.timestamp = _global_pos.timestamp; |
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_wind.windspeed_north = _ekf->states[14]; |
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_wind.windspeed_east = _ekf->states[15]; |
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_wind.covariance_north = _ekf->P[14][14]; |
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_wind.covariance_east = _ekf->P[15][15]; |
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/* lazily publish the wind estimate only once available */ |
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if (_wind_pub > 0) { |
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/* publish the wind estimate */ |
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orb_publish(ORB_ID(wind_estimate), _wind_pub, &_wind); |
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/* lazily publish the wind estimate only once available */ |
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if (_wind_pub > 0) { |
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/* publish the wind estimate */ |
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orb_publish(ORB_ID(wind_estimate), _wind_pub, &_wind); |
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} else { |
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/* advertise and publish */ |
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_wind_pub = orb_advertise(ORB_ID(wind_estimate), &_wind); |
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} |
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} |
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} else { |
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/* advertise and publish */ |
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_wind_pub = orb_advertise(ORB_ID(wind_estimate), &_wind); |
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} |
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} |
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} |
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} |
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