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@@ -73,3 +73,9 @@ log_7_2020-11-20-14-31-06.ulg filter=lfs diff=lfs merge=lfs -text
 23_36_13.ulg filter=lfs diff=lfs merge=lfs -text
 2018-09-18/08_57_01.ulg filter=lfs diff=lfs merge=lfs -text
 2018-09-18/07_41_25.ulg filter=lfs diff=lfs merge=lfs -text
+log_54_2022-4-19-18-17-42_px4_pose_reset.ulg filter=lfs diff=lfs merge=lfs -text
+2018-09-18/08_48_35.ulg filter=lfs diff=lfs merge=lfs -text
+2018-09-18/08_51_40.ulg filter=lfs diff=lfs merge=lfs -text
+2018-09-18/07_44_24.ulg filter=lfs diff=lfs merge=lfs -text
+2018-09-18/09_02_23.ulg filter=lfs diff=lfs merge=lfs -text
+2018-09-18/07_38_12.ulg filter=lfs diff=lfs merge=lfs -text

2018-09-07/12_39_45.ulg.mdat.csv

@@ -0,0 +1,66 @@
+name,value,description
+filter_fault_status,Pass,Internal Filter check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+filter_faults_max,0,Largest recorded value of the filter internal fault bitmask. Should always be zero.
+flow_sensor_status,Pass,Optical Flow sensor check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+hagl_fail_percentage,0.0,The percentage of in-flight recorded failure events for the height above ground sensor innovation consistency test.
+hagl_percentage_amber,0.0,The percentage of in-flight height above ground sensor innovation consistency test values > 0.5.
+hagl_percentage_red,0.0,The percentage of in-flight height above ground sensor innovation consistency test values > 1.0.
+hagl_sensor_status,Pass,Height above ground sensor check summary. This sensor data is normally sourced from a rangefinder sensor. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+hagl_test_max,0.453353,The maximum in-flight value of the height above ground sensor innovation consistency test ratio.
+hagl_test_mean,0.0211382,The mean in-flight value of the height above ground sensor innovation consistency test ratio.
+hgt_fail_percentage,0.0,The percentage of in-flight recorded failure events for the height sensor innovation consistency test.
+hgt_percentage_amber,0.0,The percentage of in-flight height sensor innovation consistency test values > 0.5.
+hgt_percentage_red,0.0,The percentage of in-flight height sensor innovation consistency test values > 1.0.
+hgt_sensor_status,Pass,Height sensor check summary. This sensor data can be sourced from either Baro or GPS or range finder or external vision system. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no anomalies were detected and no further investigation is required
+hgt_test_max,0.188986,The maximum in-flight value of the height sensor innovation consistency test ratio.
+hgt_test_mean,0.03344,The mean in-flight value of the height sensor innovation consistency test ratio.
+imu_bias_check,Pass,IMU bias check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+imu_coning_mean,1.55055e-06,Mean in-flight value of the IMU delta angle coning vibration metric (rad)
+imu_coning_peak,4.80696e-06,Peak in-flight value of the IMU delta angle coning vibration metric (rad)
+imu_dang_bias_median,1.20485156105e-05,Median in-flight value of the delta angle bias vector length (rad)
+imu_dvel_bias_median,0.00270824611902,Median in-flight value of the delta velocity bias vector length (m/s)
+imu_hfdang_mean,0.00227472,Mean in-flight value of the IMU delta angle high frequency vibration metric (rad)
+imu_hfdang_peak,0.00481886,Peak in-flight value of the IMU delta angle high frequency vibration metric (rad)
+imu_hfdvel_mean,0.0311802,Mean in-flight value of the IMU delta velocity high frequency vibration metric (m/s)
+imu_hfdvel_peak,0.0400721,Peak in-flight value of the IMU delta velocity high frequency vibration metric (m/s)
+imu_output_predictor_check,Warning,IMU output predictor check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+imu_sensor_status,Warning,IMU sensor check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+imu_vibration_check,Warning,IMU vibration check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+in_air_transition_time,109.6,The time in seconds measured from startup that the EKF transtioned into in-air mode. Set to a nan if a transition event is not detected.
+mag_percentage_amber,10.9665427509,The percentage of in-flight consolidated magnetic field sensor innovation consistency test values > 0.5.
+mag_percentage_red,13.3828996283,The percentage of in-flight consolidated magnetic field sensor innovation consistency test values > 1.0.
+mag_sensor_status,Fail,Magnetometer sensor check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+mag_test_max,2.4517,The maximum in-flight value of the magnetic field sensor innovation consistency test ratio.
+mag_test_mean,0.424382,The mean in-flight value of the magnetic field sensor innovation consistency test ratio.
+magx_fail_percentage,7.24907063197,The percentage of in-flight recorded failure events for the X-axis magnetic field sensor innovation consistency test.
+magy_fail_percentage,5.76208178439,The percentage of in-flight recorded failure events for the Y-axis magnetic field sensor innovation consistency test.
+magz_fail_percentage,8.36431226766,The percentage of in-flight recorded failure events for the Z-axis magnetic field sensor innovation consistency test.
+master_status,Fail,Master check status which can be either Pass Warning or Fail. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+ofx_fail_percentage,nan,The percentage of in-flight recorded failure events for the optical flow sensor X-axis innovation consistency test.
+ofy_fail_percentage,nan,The percentage of in-flight recorded failure events for the optical flow sensor Y-axis innovation consistency test.
+on_ground_transition_time,228.4,The time in seconds measured from startup  that the EKF transitioned out of in-air mode. Set to a nan if a transition event is not detected.
+output_obs_ang_err_median,0.00547681,Median in-flight value of the output observer angular error (rad)
+output_obs_pos_err_median,0.240655,Median in-flight value of the output observer position error (m)
+output_obs_vel_err_median,0.0643244,Median in-flight value of the output observer velocity error (m/s)
+pos_fail_percentage,5.79216354344,The percentage of in-flight recorded failure events for the velocity sensor consolidated innovation consistency test.
+pos_percentage_amber,8.51788756388,The percentage of in-flight position sensor consolidated innovation consistency test values > 0.5.
+pos_percentage_red,5.79216354344,The percentage of in-flight position sensor consolidated innovation consistency test values > 1.0.
+pos_sensor_status,Fail,Position sensor check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+pos_test_max,6.63768,The maximum in-flight value of the position sensor consolidated innovation consistency test ratio.
+pos_test_mean,0.471759,The mean in-flight value of the position sensor consolidated innovation consistency test ratio.
+tas_fail_percentage,nan,The percentage of in-flight recorded failure events for the airspeed sensor innovation consistency test.
+tas_percentage_amber,nan,The percentage of in-flight airspeed sensor innovation consistency test values > 0.5.
+tas_percentage_red,nan,The percentage of in-flight airspeed sensor innovation consistency test values > 1.0.
+tas_sensor_status,Pass,Airspeed sensor check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+tas_test_max,nan,The maximum in-flight value of the airspeed sensor innovation consistency test ratio.
+tas_test_mean,nan,The mean in-flight value of the airspeed sensor innovation consistency test ratio.
+tilt_align_time,nan,The time in seconds measured from startup that the EKF completed the tilt alignment. A nan value indicates that the alignment had completed before logging started or alignment did not complete.
+vel_fail_percentage,7.6660988075,The percentage of in-flight recorded failure events for the velocity sensor consolidated innovation consistency test.
+vel_percentage_amber,13.7989778535,The percentage of in-flight velocity sensor consolidated innovation consistency test values > 0.5.
+vel_percentage_red,7.6660988075,The percentage of in-flight velocity sensor consolidated innovation consistency test values > 1.0.
+vel_sensor_status,Fail,Velocity sensor check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+vel_test_max,4.01943,The maximum in-flight value of the velocity sensor consolidated innovation consistency test ratio.
+vel_test_mean,0.418834,The mean in-flight value of the velocity sensor consolidated innovation consistency test ratio.
+yaw_align_time,nan,The time in seconds measured from startup that the EKF completed the yaw alignment.
+yaw_fail_percentage,0.0,The percentage of in-flight recorded failure events for the yaw sensor innovation consistency test.
+yaw_sensor_status,Pass,Yaw sensor check summary. This sensor data can be sourced from the magnetometer or an external vision system. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required

2018-09-07/13_23_31.ulg.mdat.csv

@@ -0,0 +1,66 @@
+name,value,description
+filter_fault_status,Pass,Internal Filter check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+filter_faults_max,0,Largest recorded value of the filter internal fault bitmask. Should always be zero.
+flow_sensor_status,Pass,Optical Flow sensor check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+hagl_fail_percentage,0.0,The percentage of in-flight recorded failure events for the height above ground sensor innovation consistency test.
+hagl_percentage_amber,0.0,The percentage of in-flight height above ground sensor innovation consistency test values > 0.5.
+hagl_percentage_red,0.0,The percentage of in-flight height above ground sensor innovation consistency test values > 1.0.
+hagl_sensor_status,Pass,Height above ground sensor check summary. This sensor data is normally sourced from a rangefinder sensor. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+hagl_test_max,0.415293,The maximum in-flight value of the height above ground sensor innovation consistency test ratio.
+hagl_test_mean,0.0380489,The mean in-flight value of the height above ground sensor innovation consistency test ratio.
+hgt_fail_percentage,0.0,The percentage of in-flight recorded failure events for the height sensor innovation consistency test.
+hgt_percentage_amber,0.0,The percentage of in-flight height sensor innovation consistency test values > 0.5.
+hgt_percentage_red,0.0,The percentage of in-flight height sensor innovation consistency test values > 1.0.
+hgt_sensor_status,Pass,Height sensor check summary. This sensor data can be sourced from either Baro or GPS or range finder or external vision system. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no anomalies were detected and no further investigation is required
+hgt_test_max,0.10633,The maximum in-flight value of the height sensor innovation consistency test ratio.
+hgt_test_mean,0.0315511,The mean in-flight value of the height sensor innovation consistency test ratio.
+imu_bias_check,Pass,IMU bias check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+imu_coning_mean,1.87994e-06,Mean in-flight value of the IMU delta angle coning vibration metric (rad)
+imu_coning_peak,2.82491e-06,Peak in-flight value of the IMU delta angle coning vibration metric (rad)
+imu_dang_bias_median,2.67133147253e-05,Median in-flight value of the delta angle bias vector length (rad)
+imu_dvel_bias_median,0.0,Median in-flight value of the delta velocity bias vector length (m/s)
+imu_hfdang_mean,0.00286666,Mean in-flight value of the IMU delta angle high frequency vibration metric (rad)
+imu_hfdang_peak,0.00435189,Peak in-flight value of the IMU delta angle high frequency vibration metric (rad)
+imu_hfdvel_mean,0.0360256,Mean in-flight value of the IMU delta velocity high frequency vibration metric (m/s)
+imu_hfdvel_peak,0.0412719,Peak in-flight value of the IMU delta velocity high frequency vibration metric (m/s)
+imu_output_predictor_check,Pass,IMU output predictor check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+imu_sensor_status,Warning,IMU sensor check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+imu_vibration_check,Warning,IMU vibration check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+in_air_transition_time,39.3,The time in seconds measured from startup that the EKF transtioned into in-air mode. Set to a nan if a transition event is not detected.
+mag_percentage_amber,13.7254901961,The percentage of in-flight consolidated magnetic field sensor innovation consistency test values > 0.5.
+mag_percentage_red,42.1568627451,The percentage of in-flight consolidated magnetic field sensor innovation consistency test values > 1.0.
+mag_sensor_status,Warning,Magnetometer sensor check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+mag_test_max,1.83796,The maximum in-flight value of the magnetic field sensor innovation consistency test ratio.
+mag_test_mean,0.600065,The mean in-flight value of the magnetic field sensor innovation consistency test ratio.
+magx_fail_percentage,0.0,The percentage of in-flight recorded failure events for the X-axis magnetic field sensor innovation consistency test.
+magy_fail_percentage,0.0,The percentage of in-flight recorded failure events for the Y-axis magnetic field sensor innovation consistency test.
+magz_fail_percentage,0.0,The percentage of in-flight recorded failure events for the Z-axis magnetic field sensor innovation consistency test.
+master_status,Fail,Master check status which can be either Pass Warning or Fail. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+ofx_fail_percentage,nan,The percentage of in-flight recorded failure events for the optical flow sensor X-axis innovation consistency test.
+ofy_fail_percentage,nan,The percentage of in-flight recorded failure events for the optical flow sensor Y-axis innovation consistency test.
+on_ground_transition_time,70.5,The time in seconds measured from startup  that the EKF transitioned out of in-air mode. Set to a nan if a transition event is not detected.
+output_obs_ang_err_median,0.00336383,Median in-flight value of the output observer angular error (rad)
+output_obs_pos_err_median,0.0520934,Median in-flight value of the output observer position error (m)
+output_obs_vel_err_median,0.0413504,Median in-flight value of the output observer velocity error (m/s)
+pos_fail_percentage,21.1920529801,The percentage of in-flight recorded failure events for the velocity sensor consolidated innovation consistency test.
+pos_percentage_amber,17.2185430464,The percentage of in-flight position sensor consolidated innovation consistency test values > 0.5.
+pos_percentage_red,21.1920529801,The percentage of in-flight position sensor consolidated innovation consistency test values > 1.0.
+pos_sensor_status,Fail,Position sensor check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+pos_test_max,2.62984,The maximum in-flight value of the position sensor consolidated innovation consistency test ratio.
+pos_test_mean,0.699873,The mean in-flight value of the position sensor consolidated innovation consistency test ratio.
+tas_fail_percentage,nan,The percentage of in-flight recorded failure events for the airspeed sensor innovation consistency test.
+tas_percentage_amber,nan,The percentage of in-flight airspeed sensor innovation consistency test values > 0.5.
+tas_percentage_red,nan,The percentage of in-flight airspeed sensor innovation consistency test values > 1.0.
+tas_sensor_status,Pass,Airspeed sensor check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+tas_test_max,nan,The maximum in-flight value of the airspeed sensor innovation consistency test ratio.
+tas_test_mean,nan,The mean in-flight value of the airspeed sensor innovation consistency test ratio.
+tilt_align_time,nan,The time in seconds measured from startup that the EKF completed the tilt alignment. A nan value indicates that the alignment had completed before logging started or alignment did not complete.
+vel_fail_percentage,nan,The percentage of in-flight recorded failure events for the velocity sensor consolidated innovation consistency test.
+vel_percentage_amber,nan,The percentage of in-flight velocity sensor consolidated innovation consistency test values > 0.5.
+vel_percentage_red,nan,The percentage of in-flight velocity sensor consolidated innovation consistency test values > 1.0.
+vel_sensor_status,Pass,Velocity sensor check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+vel_test_max,nan,The maximum in-flight value of the velocity sensor consolidated innovation consistency test ratio.
+vel_test_mean,nan,The mean in-flight value of the velocity sensor consolidated innovation consistency test ratio.
+yaw_align_time,nan,The time in seconds measured from startup that the EKF completed the yaw alignment.
+yaw_fail_percentage,42.1568627451,The percentage of in-flight recorded failure events for the yaw sensor innovation consistency test.
+yaw_sensor_status,Fail,Yaw sensor check summary. This sensor data can be sourced from the magnetometer or an external vision system. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required

2018-09-07/13_29_47.ulg.mdat.csv

@@ -0,0 +1,66 @@
+name,value,description
+filter_fault_status,Pass,Internal Filter check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+filter_faults_max,0,Largest recorded value of the filter internal fault bitmask. Should always be zero.
+flow_sensor_status,Pass,Optical Flow sensor check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+hagl_fail_percentage,0.0,The percentage of in-flight recorded failure events for the height above ground sensor innovation consistency test.
+hagl_percentage_amber,0.0,The percentage of in-flight height above ground sensor innovation consistency test values > 0.5.
+hagl_percentage_red,0.0,The percentage of in-flight height above ground sensor innovation consistency test values > 1.0.
+hagl_sensor_status,Pass,Height above ground sensor check summary. This sensor data is normally sourced from a rangefinder sensor. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+hagl_test_max,0.394022,The maximum in-flight value of the height above ground sensor innovation consistency test ratio.
+hagl_test_mean,0.0207652,The mean in-flight value of the height above ground sensor innovation consistency test ratio.
+hgt_fail_percentage,0.0,The percentage of in-flight recorded failure events for the height sensor innovation consistency test.
+hgt_percentage_amber,0.0,The percentage of in-flight height sensor innovation consistency test values > 0.5.
+hgt_percentage_red,0.0,The percentage of in-flight height sensor innovation consistency test values > 1.0.
+hgt_sensor_status,Pass,Height sensor check summary. This sensor data can be sourced from either Baro or GPS or range finder or external vision system. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no anomalies were detected and no further investigation is required
+hgt_test_max,0.0848837,The maximum in-flight value of the height sensor innovation consistency test ratio.
+hgt_test_mean,0.0267673,The mean in-flight value of the height sensor innovation consistency test ratio.
+imu_bias_check,Pass,IMU bias check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+imu_coning_mean,1.46182e-06,Mean in-flight value of the IMU delta angle coning vibration metric (rad)
+imu_coning_peak,3.16051e-06,Peak in-flight value of the IMU delta angle coning vibration metric (rad)
+imu_dang_bias_median,8.02823033197e-06,Median in-flight value of the delta angle bias vector length (rad)
+imu_dvel_bias_median,0.0,Median in-flight value of the delta velocity bias vector length (m/s)
+imu_hfdang_mean,0.00233196,Mean in-flight value of the IMU delta angle high frequency vibration metric (rad)
+imu_hfdang_peak,0.00360146,Peak in-flight value of the IMU delta angle high frequency vibration metric (rad)
+imu_hfdvel_mean,0.0336619,Mean in-flight value of the IMU delta velocity high frequency vibration metric (m/s)
+imu_hfdvel_peak,0.0411097,Peak in-flight value of the IMU delta velocity high frequency vibration metric (m/s)
+imu_output_predictor_check,Pass,IMU output predictor check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+imu_sensor_status,Warning,IMU sensor check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+imu_vibration_check,Warning,IMU vibration check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+in_air_transition_time,36.3,The time in seconds measured from startup that the EKF transtioned into in-air mode. Set to a nan if a transition event is not detected.
+mag_percentage_amber,41.4201183432,The percentage of in-flight consolidated magnetic field sensor innovation consistency test values > 0.5.
+mag_percentage_red,21.3017751479,The percentage of in-flight consolidated magnetic field sensor innovation consistency test values > 1.0.
+mag_sensor_status,Warning,Magnetometer sensor check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+mag_test_max,1.70284,The maximum in-flight value of the magnetic field sensor innovation consistency test ratio.
+mag_test_mean,0.543473,The mean in-flight value of the magnetic field sensor innovation consistency test ratio.
+magx_fail_percentage,0.0,The percentage of in-flight recorded failure events for the X-axis magnetic field sensor innovation consistency test.
+magy_fail_percentage,0.0,The percentage of in-flight recorded failure events for the Y-axis magnetic field sensor innovation consistency test.
+magz_fail_percentage,0.0,The percentage of in-flight recorded failure events for the Z-axis magnetic field sensor innovation consistency test.
+master_status,Fail,Master check status which can be either Pass Warning or Fail. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+ofx_fail_percentage,nan,The percentage of in-flight recorded failure events for the optical flow sensor X-axis innovation consistency test.
+ofy_fail_percentage,nan,The percentage of in-flight recorded failure events for the optical flow sensor Y-axis innovation consistency test.
+on_ground_transition_time,80.4,The time in seconds measured from startup  that the EKF transitioned out of in-air mode. Set to a nan if a transition event is not detected.
+output_obs_ang_err_median,0.00402346,Median in-flight value of the output observer angular error (rad)
+output_obs_pos_err_median,0.0473642,Median in-flight value of the output observer position error (m)
+output_obs_vel_err_median,0.0374163,Median in-flight value of the output observer velocity error (m/s)
+pos_fail_percentage,23.8532110092,The percentage of in-flight recorded failure events for the velocity sensor consolidated innovation consistency test.
+pos_percentage_amber,12.3853211009,The percentage of in-flight position sensor consolidated innovation consistency test values > 0.5.
+pos_percentage_red,23.8532110092,The percentage of in-flight position sensor consolidated innovation consistency test values > 1.0.
+pos_sensor_status,Fail,Position sensor check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+pos_test_max,5.90539,The maximum in-flight value of the position sensor consolidated innovation consistency test ratio.
+pos_test_mean,1.04582,The mean in-flight value of the position sensor consolidated innovation consistency test ratio.
+tas_fail_percentage,nan,The percentage of in-flight recorded failure events for the airspeed sensor innovation consistency test.
+tas_percentage_amber,nan,The percentage of in-flight airspeed sensor innovation consistency test values > 0.5.
+tas_percentage_red,nan,The percentage of in-flight airspeed sensor innovation consistency test values > 1.0.
+tas_sensor_status,Pass,Airspeed sensor check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+tas_test_max,nan,The maximum in-flight value of the airspeed sensor innovation consistency test ratio.
+tas_test_mean,nan,The mean in-flight value of the airspeed sensor innovation consistency test ratio.
+tilt_align_time,nan,The time in seconds measured from startup that the EKF completed the tilt alignment. A nan value indicates that the alignment had completed before logging started or alignment did not complete.
+vel_fail_percentage,nan,The percentage of in-flight recorded failure events for the velocity sensor consolidated innovation consistency test.
+vel_percentage_amber,nan,The percentage of in-flight velocity sensor consolidated innovation consistency test values > 0.5.
+vel_percentage_red,nan,The percentage of in-flight velocity sensor consolidated innovation consistency test values > 1.0.
+vel_sensor_status,Pass,Velocity sensor check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+vel_test_max,nan,The maximum in-flight value of the velocity sensor consolidated innovation consistency test ratio.
+vel_test_mean,nan,The mean in-flight value of the velocity sensor consolidated innovation consistency test ratio.
+yaw_align_time,nan,The time in seconds measured from startup that the EKF completed the yaw alignment.
+yaw_fail_percentage,17.1597633136,The percentage of in-flight recorded failure events for the yaw sensor innovation consistency test.
+yaw_sensor_status,Fail,Yaw sensor check summary. This sensor data can be sourced from the magnetometer or an external vision system. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required

2018-09-08/17_26_26.ulg.mdat.csv

@@ -0,0 +1,66 @@
+name,value,description
+filter_fault_status,Pass,Internal Filter check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+filter_faults_max,0,Largest recorded value of the filter internal fault bitmask. Should always be zero.
+flow_sensor_status,Pass,Optical Flow sensor check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+hagl_fail_percentage,0.0,The percentage of in-flight recorded failure events for the height above ground sensor innovation consistency test.
+hagl_percentage_amber,0.0,The percentage of in-flight height above ground sensor innovation consistency test values > 0.5.
+hagl_percentage_red,0.0,The percentage of in-flight height above ground sensor innovation consistency test values > 1.0.
+hagl_sensor_status,Pass,Height above ground sensor check summary. This sensor data is normally sourced from a rangefinder sensor. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+hagl_test_max,0.267484,The maximum in-flight value of the height above ground sensor innovation consistency test ratio.
+hagl_test_mean,0.0237437,The mean in-flight value of the height above ground sensor innovation consistency test ratio.
+hgt_fail_percentage,0.0,The percentage of in-flight recorded failure events for the height sensor innovation consistency test.
+hgt_percentage_amber,0.0,The percentage of in-flight height sensor innovation consistency test values > 0.5.
+hgt_percentage_red,0.0,The percentage of in-flight height sensor innovation consistency test values > 1.0.
+hgt_sensor_status,Pass,Height sensor check summary. This sensor data can be sourced from either Baro or GPS or range finder or external vision system. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no anomalies were detected and no further investigation is required
+hgt_test_max,0.0612991,The maximum in-flight value of the height sensor innovation consistency test ratio.
+hgt_test_mean,0.0174559,The mean in-flight value of the height sensor innovation consistency test ratio.
+imu_bias_check,Pass,IMU bias check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+imu_coning_mean,1.74092e-06,Mean in-flight value of the IMU delta angle coning vibration metric (rad)
+imu_coning_peak,2.8619e-06,Peak in-flight value of the IMU delta angle coning vibration metric (rad)
+imu_dang_bias_median,1.72112983994e-05,Median in-flight value of the delta angle bias vector length (rad)
+imu_dvel_bias_median,0.0,Median in-flight value of the delta velocity bias vector length (m/s)
+imu_hfdang_mean,0.00229597,Mean in-flight value of the IMU delta angle high frequency vibration metric (rad)
+imu_hfdang_peak,0.0033698,Peak in-flight value of the IMU delta angle high frequency vibration metric (rad)
+imu_hfdvel_mean,0.0240689,Mean in-flight value of the IMU delta velocity high frequency vibration metric (m/s)
+imu_hfdvel_peak,0.0268309,Peak in-flight value of the IMU delta velocity high frequency vibration metric (m/s)
+imu_output_predictor_check,Pass,IMU output predictor check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+imu_sensor_status,Warning,IMU sensor check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+imu_vibration_check,Warning,IMU vibration check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+in_air_transition_time,45.0,The time in seconds measured from startup that the EKF transtioned into in-air mode. Set to a nan if a transition event is not detected.
+mag_percentage_amber,0.0,The percentage of in-flight consolidated magnetic field sensor innovation consistency test values > 0.5.
+mag_percentage_red,0.0,The percentage of in-flight consolidated magnetic field sensor innovation consistency test values > 1.0.
+mag_sensor_status,Pass,Magnetometer sensor check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+mag_test_max,0.488852,The maximum in-flight value of the magnetic field sensor innovation consistency test ratio.
+mag_test_mean,0.127659,The mean in-flight value of the magnetic field sensor innovation consistency test ratio.
+magx_fail_percentage,0.0,The percentage of in-flight recorded failure events for the X-axis magnetic field sensor innovation consistency test.
+magy_fail_percentage,0.0,The percentage of in-flight recorded failure events for the Y-axis magnetic field sensor innovation consistency test.
+magz_fail_percentage,0.0,The percentage of in-flight recorded failure events for the Z-axis magnetic field sensor innovation consistency test.
+master_status,Warning,Master check status which can be either Pass Warning or Fail. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+ofx_fail_percentage,nan,The percentage of in-flight recorded failure events for the optical flow sensor X-axis innovation consistency test.
+ofy_fail_percentage,nan,The percentage of in-flight recorded failure events for the optical flow sensor Y-axis innovation consistency test.
+on_ground_transition_time,103.9,The time in seconds measured from startup  that the EKF transitioned out of in-air mode. Set to a nan if a transition event is not detected.
+output_obs_ang_err_median,0.000557168,Median in-flight value of the output observer angular error (rad)
+output_obs_pos_err_median,0.0191662,Median in-flight value of the output observer position error (m)
+output_obs_vel_err_median,0.00794995,Median in-flight value of the output observer velocity error (m/s)
+pos_fail_percentage,0.0,The percentage of in-flight recorded failure events for the velocity sensor consolidated innovation consistency test.
+pos_percentage_amber,0.0,The percentage of in-flight position sensor consolidated innovation consistency test values > 0.5.
+pos_percentage_red,0.0,The percentage of in-flight position sensor consolidated innovation consistency test values > 1.0.
+pos_sensor_status,Pass,Position sensor check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+pos_test_max,0.186307,The maximum in-flight value of the position sensor consolidated innovation consistency test ratio.
+pos_test_mean,0.0512611,The mean in-flight value of the position sensor consolidated innovation consistency test ratio.
+tas_fail_percentage,nan,The percentage of in-flight recorded failure events for the airspeed sensor innovation consistency test.
+tas_percentage_amber,nan,The percentage of in-flight airspeed sensor innovation consistency test values > 0.5.
+tas_percentage_red,nan,The percentage of in-flight airspeed sensor innovation consistency test values > 1.0.
+tas_sensor_status,Pass,Airspeed sensor check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+tas_test_max,nan,The maximum in-flight value of the airspeed sensor innovation consistency test ratio.
+tas_test_mean,nan,The mean in-flight value of the airspeed sensor innovation consistency test ratio.
+tilt_align_time,nan,The time in seconds measured from startup that the EKF completed the tilt alignment. A nan value indicates that the alignment had completed before logging started or alignment did not complete.
+vel_fail_percentage,nan,The percentage of in-flight recorded failure events for the velocity sensor consolidated innovation consistency test.
+vel_percentage_amber,nan,The percentage of in-flight velocity sensor consolidated innovation consistency test values > 0.5.
+vel_percentage_red,nan,The percentage of in-flight velocity sensor consolidated innovation consistency test values > 1.0.
+vel_sensor_status,Pass,Velocity sensor check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+vel_test_max,nan,The maximum in-flight value of the velocity sensor consolidated innovation consistency test ratio.
+vel_test_mean,nan,The mean in-flight value of the velocity sensor consolidated innovation consistency test ratio.
+yaw_align_time,nan,The time in seconds measured from startup that the EKF completed the yaw alignment.
+yaw_fail_percentage,0.0,The percentage of in-flight recorded failure events for the yaw sensor innovation consistency test.
+yaw_sensor_status,Pass,Yaw sensor check summary. This sensor data can be sourced from the magnetometer or an external vision system. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required

2018-09-08/17_30_27.ulg.mdat.csv

@@ -0,0 +1,66 @@
+name,value,description
+filter_fault_status,Pass,Internal Filter check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+filter_faults_max,0,Largest recorded value of the filter internal fault bitmask. Should always be zero.
+flow_sensor_status,Pass,Optical Flow sensor check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+hagl_fail_percentage,0.0,The percentage of in-flight recorded failure events for the height above ground sensor innovation consistency test.
+hagl_percentage_amber,0.0,The percentage of in-flight height above ground sensor innovation consistency test values > 0.5.
+hagl_percentage_red,0.0,The percentage of in-flight height above ground sensor innovation consistency test values > 1.0.
+hagl_sensor_status,Pass,Height above ground sensor check summary. This sensor data is normally sourced from a rangefinder sensor. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+hagl_test_max,0.264673,The maximum in-flight value of the height above ground sensor innovation consistency test ratio.
+hagl_test_mean,0.02261,The mean in-flight value of the height above ground sensor innovation consistency test ratio.
+hgt_fail_percentage,0.0,The percentage of in-flight recorded failure events for the height sensor innovation consistency test.
+hgt_percentage_amber,0.0,The percentage of in-flight height sensor innovation consistency test values > 0.5.
+hgt_percentage_red,0.0,The percentage of in-flight height sensor innovation consistency test values > 1.0.
+hgt_sensor_status,Pass,Height sensor check summary. This sensor data can be sourced from either Baro or GPS or range finder or external vision system. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no anomalies were detected and no further investigation is required
+hgt_test_max,0.0729305,The maximum in-flight value of the height sensor innovation consistency test ratio.
+hgt_test_mean,0.0209558,The mean in-flight value of the height sensor innovation consistency test ratio.
+imu_bias_check,Pass,IMU bias check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+imu_coning_mean,1.9575e-06,Mean in-flight value of the IMU delta angle coning vibration metric (rad)
+imu_coning_peak,4.19232e-06,Peak in-flight value of the IMU delta angle coning vibration metric (rad)
+imu_dang_bias_median,2.90339480044e-05,Median in-flight value of the delta angle bias vector length (rad)
+imu_dvel_bias_median,0.0,Median in-flight value of the delta velocity bias vector length (m/s)
+imu_hfdang_mean,0.00244943,Mean in-flight value of the IMU delta angle high frequency vibration metric (rad)
+imu_hfdang_peak,0.00452715,Peak in-flight value of the IMU delta angle high frequency vibration metric (rad)
+imu_hfdvel_mean,0.0258568,Mean in-flight value of the IMU delta velocity high frequency vibration metric (m/s)
+imu_hfdvel_peak,0.0309102,Peak in-flight value of the IMU delta velocity high frequency vibration metric (m/s)
+imu_output_predictor_check,Pass,IMU output predictor check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+imu_sensor_status,Warning,IMU sensor check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+imu_vibration_check,Warning,IMU vibration check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+in_air_transition_time,46.0,The time in seconds measured from startup that the EKF transtioned into in-air mode. Set to a nan if a transition event is not detected.
+mag_percentage_amber,0.0,The percentage of in-flight consolidated magnetic field sensor innovation consistency test values > 0.5.
+mag_percentage_red,0.0,The percentage of in-flight consolidated magnetic field sensor innovation consistency test values > 1.0.
+mag_sensor_status,Pass,Magnetometer sensor check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+mag_test_max,0.348092,The maximum in-flight value of the magnetic field sensor innovation consistency test ratio.
+mag_test_mean,0.1204,The mean in-flight value of the magnetic field sensor innovation consistency test ratio.
+magx_fail_percentage,0.0,The percentage of in-flight recorded failure events for the X-axis magnetic field sensor innovation consistency test.
+magy_fail_percentage,0.0,The percentage of in-flight recorded failure events for the Y-axis magnetic field sensor innovation consistency test.
+magz_fail_percentage,0.0,The percentage of in-flight recorded failure events for the Z-axis magnetic field sensor innovation consistency test.
+master_status,Warning,Master check status which can be either Pass Warning or Fail. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+ofx_fail_percentage,nan,The percentage of in-flight recorded failure events for the optical flow sensor X-axis innovation consistency test.
+ofy_fail_percentage,nan,The percentage of in-flight recorded failure events for the optical flow sensor Y-axis innovation consistency test.
+on_ground_transition_time,137.1,The time in seconds measured from startup  that the EKF transitioned out of in-air mode. Set to a nan if a transition event is not detected.
+output_obs_ang_err_median,0.000454446,Median in-flight value of the output observer angular error (rad)
+output_obs_pos_err_median,0.0149185,Median in-flight value of the output observer position error (m)
+output_obs_vel_err_median,0.0060517,Median in-flight value of the output observer velocity error (m/s)
+pos_fail_percentage,0.0,The percentage of in-flight recorded failure events for the velocity sensor consolidated innovation consistency test.
+pos_percentage_amber,0.0,The percentage of in-flight position sensor consolidated innovation consistency test values > 0.5.
+pos_percentage_red,0.0,The percentage of in-flight position sensor consolidated innovation consistency test values > 1.0.
+pos_sensor_status,Pass,Position sensor check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+pos_test_max,0.185793,The maximum in-flight value of the position sensor consolidated innovation consistency test ratio.
+pos_test_mean,0.0425431,The mean in-flight value of the position sensor consolidated innovation consistency test ratio.
+tas_fail_percentage,nan,The percentage of in-flight recorded failure events for the airspeed sensor innovation consistency test.
+tas_percentage_amber,nan,The percentage of in-flight airspeed sensor innovation consistency test values > 0.5.
+tas_percentage_red,nan,The percentage of in-flight airspeed sensor innovation consistency test values > 1.0.
+tas_sensor_status,Pass,Airspeed sensor check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+tas_test_max,nan,The maximum in-flight value of the airspeed sensor innovation consistency test ratio.
+tas_test_mean,nan,The mean in-flight value of the airspeed sensor innovation consistency test ratio.
+tilt_align_time,nan,The time in seconds measured from startup that the EKF completed the tilt alignment. A nan value indicates that the alignment had completed before logging started or alignment did not complete.
+vel_fail_percentage,nan,The percentage of in-flight recorded failure events for the velocity sensor consolidated innovation consistency test.
+vel_percentage_amber,nan,The percentage of in-flight velocity sensor consolidated innovation consistency test values > 0.5.
+vel_percentage_red,nan,The percentage of in-flight velocity sensor consolidated innovation consistency test values > 1.0.
+vel_sensor_status,Pass,Velocity sensor check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+vel_test_max,nan,The maximum in-flight value of the velocity sensor consolidated innovation consistency test ratio.
+vel_test_mean,nan,The mean in-flight value of the velocity sensor consolidated innovation consistency test ratio.
+yaw_align_time,nan,The time in seconds measured from startup that the EKF completed the yaw alignment.
+yaw_fail_percentage,0.0,The percentage of in-flight recorded failure events for the yaw sensor innovation consistency test.
+yaw_sensor_status,Pass,Yaw sensor check summary. This sensor data can be sourced from the magnetometer or an external vision system. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required

2018-09-08/17_36_24.ulg.mdat.csv

@@ -0,0 +1,66 @@
+name,value,description
+filter_fault_status,Pass,Internal Filter check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+filter_faults_max,0,Largest recorded value of the filter internal fault bitmask. Should always be zero.
+flow_sensor_status,Pass,Optical Flow sensor check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+hagl_fail_percentage,0.0,The percentage of in-flight recorded failure events for the height above ground sensor innovation consistency test.
+hagl_percentage_amber,0.0,The percentage of in-flight height above ground sensor innovation consistency test values > 0.5.
+hagl_percentage_red,0.0,The percentage of in-flight height above ground sensor innovation consistency test values > 1.0.
+hagl_sensor_status,Pass,Height above ground sensor check summary. This sensor data is normally sourced from a rangefinder sensor. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+hagl_test_max,0.29958,The maximum in-flight value of the height above ground sensor innovation consistency test ratio.
+hagl_test_mean,0.0298594,The mean in-flight value of the height above ground sensor innovation consistency test ratio.
+hgt_fail_percentage,0.0,The percentage of in-flight recorded failure events for the height sensor innovation consistency test.
+hgt_percentage_amber,0.0,The percentage of in-flight height sensor innovation consistency test values > 0.5.
+hgt_percentage_red,0.0,The percentage of in-flight height sensor innovation consistency test values > 1.0.
+hgt_sensor_status,Pass,Height sensor check summary. This sensor data can be sourced from either Baro or GPS or range finder or external vision system. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no anomalies were detected and no further investigation is required
+hgt_test_max,0.0790737,The maximum in-flight value of the height sensor innovation consistency test ratio.
+hgt_test_mean,0.0216026,The mean in-flight value of the height sensor innovation consistency test ratio.
+imu_bias_check,Pass,IMU bias check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+imu_coning_mean,1.98013e-06,Mean in-flight value of the IMU delta angle coning vibration metric (rad)
+imu_coning_peak,5.00026e-06,Peak in-flight value of the IMU delta angle coning vibration metric (rad)
+imu_dang_bias_median,1.61105910427e-05,Median in-flight value of the delta angle bias vector length (rad)
+imu_dvel_bias_median,0.0,Median in-flight value of the delta velocity bias vector length (m/s)
+imu_hfdang_mean,0.00245704,Mean in-flight value of the IMU delta angle high frequency vibration metric (rad)
+imu_hfdang_peak,0.00409151,Peak in-flight value of the IMU delta angle high frequency vibration metric (rad)
+imu_hfdvel_mean,0.0263247,Mean in-flight value of the IMU delta velocity high frequency vibration metric (m/s)
+imu_hfdvel_peak,0.0301696,Peak in-flight value of the IMU delta velocity high frequency vibration metric (m/s)
+imu_output_predictor_check,Pass,IMU output predictor check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+imu_sensor_status,Warning,IMU sensor check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+imu_vibration_check,Warning,IMU vibration check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+in_air_transition_time,66.2,The time in seconds measured from startup that the EKF transtioned into in-air mode. Set to a nan if a transition event is not detected.
+mag_percentage_amber,1.25,The percentage of in-flight consolidated magnetic field sensor innovation consistency test values > 0.5.
+mag_percentage_red,0.0,The percentage of in-flight consolidated magnetic field sensor innovation consistency test values > 1.0.
+mag_sensor_status,Pass,Magnetometer sensor check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+mag_test_max,0.51569,The maximum in-flight value of the magnetic field sensor innovation consistency test ratio.
+mag_test_mean,0.119904,The mean in-flight value of the magnetic field sensor innovation consistency test ratio.
+magx_fail_percentage,0.0,The percentage of in-flight recorded failure events for the X-axis magnetic field sensor innovation consistency test.
+magy_fail_percentage,0.0,The percentage of in-flight recorded failure events for the Y-axis magnetic field sensor innovation consistency test.
+magz_fail_percentage,0.0,The percentage of in-flight recorded failure events for the Z-axis magnetic field sensor innovation consistency test.
+master_status,Warning,Master check status which can be either Pass Warning or Fail. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+ofx_fail_percentage,nan,The percentage of in-flight recorded failure events for the optical flow sensor X-axis innovation consistency test.
+ofy_fail_percentage,nan,The percentage of in-flight recorded failure events for the optical flow sensor Y-axis innovation consistency test.
+on_ground_transition_time,143.8,The time in seconds measured from startup  that the EKF transitioned out of in-air mode. Set to a nan if a transition event is not detected.
+output_obs_ang_err_median,0.000595128,Median in-flight value of the output observer angular error (rad)
+output_obs_pos_err_median,0.0203731,Median in-flight value of the output observer position error (m)
+output_obs_vel_err_median,0.00858495,Median in-flight value of the output observer velocity error (m/s)
+pos_fail_percentage,0.0,The percentage of in-flight recorded failure events for the velocity sensor consolidated innovation consistency test.
+pos_percentage_amber,0.0,The percentage of in-flight position sensor consolidated innovation consistency test values > 0.5.
+pos_percentage_red,0.0,The percentage of in-flight position sensor consolidated innovation consistency test values > 1.0.
+pos_sensor_status,Pass,Position sensor check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+pos_test_max,0.269956,The maximum in-flight value of the position sensor consolidated innovation consistency test ratio.
+pos_test_mean,0.0581099,The mean in-flight value of the position sensor consolidated innovation consistency test ratio.
+tas_fail_percentage,nan,The percentage of in-flight recorded failure events for the airspeed sensor innovation consistency test.
+tas_percentage_amber,nan,The percentage of in-flight airspeed sensor innovation consistency test values > 0.5.
+tas_percentage_red,nan,The percentage of in-flight airspeed sensor innovation consistency test values > 1.0.
+tas_sensor_status,Pass,Airspeed sensor check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+tas_test_max,nan,The maximum in-flight value of the airspeed sensor innovation consistency test ratio.
+tas_test_mean,nan,The mean in-flight value of the airspeed sensor innovation consistency test ratio.
+tilt_align_time,nan,The time in seconds measured from startup that the EKF completed the tilt alignment. A nan value indicates that the alignment had completed before logging started or alignment did not complete.
+vel_fail_percentage,nan,The percentage of in-flight recorded failure events for the velocity sensor consolidated innovation consistency test.
+vel_percentage_amber,nan,The percentage of in-flight velocity sensor consolidated innovation consistency test values > 0.5.
+vel_percentage_red,nan,The percentage of in-flight velocity sensor consolidated innovation consistency test values > 1.0.
+vel_sensor_status,Pass,Velocity sensor check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+vel_test_max,nan,The maximum in-flight value of the velocity sensor consolidated innovation consistency test ratio.
+vel_test_mean,nan,The mean in-flight value of the velocity sensor consolidated innovation consistency test ratio.
+yaw_align_time,nan,The time in seconds measured from startup that the EKF completed the yaw alignment.
+yaw_fail_percentage,0.0,The percentage of in-flight recorded failure events for the yaw sensor innovation consistency test.
+yaw_sensor_status,Pass,Yaw sensor check summary. This sensor data can be sourced from the magnetometer or an external vision system. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required

2018-09-08/17_40_05.ulg.mdat.csv

@@ -0,0 +1,66 @@
+name,value,description
+filter_fault_status,Pass,Internal Filter check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+filter_faults_max,0,Largest recorded value of the filter internal fault bitmask. Should always be zero.
+flow_sensor_status,Pass,Optical Flow sensor check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+hagl_fail_percentage,0.0,The percentage of in-flight recorded failure events for the height above ground sensor innovation consistency test.
+hagl_percentage_amber,0.0,The percentage of in-flight height above ground sensor innovation consistency test values > 0.5.
+hagl_percentage_red,0.0,The percentage of in-flight height above ground sensor innovation consistency test values > 1.0.
+hagl_sensor_status,Pass,Height above ground sensor check summary. This sensor data is normally sourced from a rangefinder sensor. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+hagl_test_max,0.152461,The maximum in-flight value of the height above ground sensor innovation consistency test ratio.
+hagl_test_mean,0.0295262,The mean in-flight value of the height above ground sensor innovation consistency test ratio.
+hgt_fail_percentage,0.0,The percentage of in-flight recorded failure events for the height sensor innovation consistency test.
+hgt_percentage_amber,0.0,The percentage of in-flight height sensor innovation consistency test values > 0.5.
+hgt_percentage_red,0.0,The percentage of in-flight height sensor innovation consistency test values > 1.0.
+hgt_sensor_status,Pass,Height sensor check summary. This sensor data can be sourced from either Baro or GPS or range finder or external vision system. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no anomalies were detected and no further investigation is required
+hgt_test_max,0.0578858,The maximum in-flight value of the height sensor innovation consistency test ratio.
+hgt_test_mean,0.0190019,The mean in-flight value of the height sensor innovation consistency test ratio.
+imu_bias_check,Pass,IMU bias check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+imu_coning_mean,2.212e-06,Mean in-flight value of the IMU delta angle coning vibration metric (rad)
+imu_coning_peak,3.30096e-06,Peak in-flight value of the IMU delta angle coning vibration metric (rad)
+imu_dang_bias_median,1.08603764125e-05,Median in-flight value of the delta angle bias vector length (rad)
+imu_dvel_bias_median,0.0,Median in-flight value of the delta velocity bias vector length (m/s)
+imu_hfdang_mean,0.00257749,Mean in-flight value of the IMU delta angle high frequency vibration metric (rad)
+imu_hfdang_peak,0.00326999,Peak in-flight value of the IMU delta angle high frequency vibration metric (rad)
+imu_hfdvel_mean,0.0261595,Mean in-flight value of the IMU delta velocity high frequency vibration metric (m/s)
+imu_hfdvel_peak,0.0286547,Peak in-flight value of the IMU delta velocity high frequency vibration metric (m/s)
+imu_output_predictor_check,Pass,IMU output predictor check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+imu_sensor_status,Warning,IMU sensor check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+imu_vibration_check,Warning,IMU vibration check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+in_air_transition_time,44.9,The time in seconds measured from startup that the EKF transtioned into in-air mode. Set to a nan if a transition event is not detected.
+mag_percentage_amber,0.0,The percentage of in-flight consolidated magnetic field sensor innovation consistency test values > 0.5.
+mag_percentage_red,0.0,The percentage of in-flight consolidated magnetic field sensor innovation consistency test values > 1.0.
+mag_sensor_status,Pass,Magnetometer sensor check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+mag_test_max,0.303231,The maximum in-flight value of the magnetic field sensor innovation consistency test ratio.
+mag_test_mean,0.100578,The mean in-flight value of the magnetic field sensor innovation consistency test ratio.
+magx_fail_percentage,0.0,The percentage of in-flight recorded failure events for the X-axis magnetic field sensor innovation consistency test.
+magy_fail_percentage,0.0,The percentage of in-flight recorded failure events for the Y-axis magnetic field sensor innovation consistency test.
+magz_fail_percentage,0.0,The percentage of in-flight recorded failure events for the Z-axis magnetic field sensor innovation consistency test.
+master_status,Warning,Master check status which can be either Pass Warning or Fail. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+ofx_fail_percentage,nan,The percentage of in-flight recorded failure events for the optical flow sensor X-axis innovation consistency test.
+ofy_fail_percentage,nan,The percentage of in-flight recorded failure events for the optical flow sensor Y-axis innovation consistency test.
+on_ground_transition_time,82.0,The time in seconds measured from startup  that the EKF transitioned out of in-air mode. Set to a nan if a transition event is not detected.
+output_obs_ang_err_median,0.000552887,Median in-flight value of the output observer angular error (rad)
+output_obs_pos_err_median,0.0240787,Median in-flight value of the output observer position error (m)
+output_obs_vel_err_median,0.0100734,Median in-flight value of the output observer velocity error (m/s)
+pos_fail_percentage,0.0,The percentage of in-flight recorded failure events for the velocity sensor consolidated innovation consistency test.
+pos_percentage_amber,0.0,The percentage of in-flight position sensor consolidated innovation consistency test values > 0.5.
+pos_percentage_red,0.0,The percentage of in-flight position sensor consolidated innovation consistency test values > 1.0.
+pos_sensor_status,Pass,Position sensor check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+pos_test_max,0.126097,The maximum in-flight value of the position sensor consolidated innovation consistency test ratio.
+pos_test_mean,0.0540361,The mean in-flight value of the position sensor consolidated innovation consistency test ratio.
+tas_fail_percentage,nan,The percentage of in-flight recorded failure events for the airspeed sensor innovation consistency test.
+tas_percentage_amber,nan,The percentage of in-flight airspeed sensor innovation consistency test values > 0.5.
+tas_percentage_red,nan,The percentage of in-flight airspeed sensor innovation consistency test values > 1.0.
+tas_sensor_status,Pass,Airspeed sensor check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+tas_test_max,nan,The maximum in-flight value of the airspeed sensor innovation consistency test ratio.
+tas_test_mean,nan,The mean in-flight value of the airspeed sensor innovation consistency test ratio.
+tilt_align_time,nan,The time in seconds measured from startup that the EKF completed the tilt alignment. A nan value indicates that the alignment had completed before logging started or alignment did not complete.
+vel_fail_percentage,nan,The percentage of in-flight recorded failure events for the velocity sensor consolidated innovation consistency test.
+vel_percentage_amber,nan,The percentage of in-flight velocity sensor consolidated innovation consistency test values > 0.5.
+vel_percentage_red,nan,The percentage of in-flight velocity sensor consolidated innovation consistency test values > 1.0.
+vel_sensor_status,Pass,Velocity sensor check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+vel_test_max,nan,The maximum in-flight value of the velocity sensor consolidated innovation consistency test ratio.
+vel_test_mean,nan,The mean in-flight value of the velocity sensor consolidated innovation consistency test ratio.
+yaw_align_time,nan,The time in seconds measured from startup that the EKF completed the yaw alignment.
+yaw_fail_percentage,0.0,The percentage of in-flight recorded failure events for the yaw sensor innovation consistency test.
+yaw_sensor_status,Pass,Yaw sensor check summary. This sensor data can be sourced from the magnetometer or an external vision system. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required

2018-09-08/17_41_57.ulg.mdat.csv

@@ -0,0 +1,66 @@
+name,value,description
+filter_fault_status,Pass,Internal Filter check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+filter_faults_max,0,Largest recorded value of the filter internal fault bitmask. Should always be zero.
+flow_sensor_status,Pass,Optical Flow sensor check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+hagl_fail_percentage,0.0,The percentage of in-flight recorded failure events for the height above ground sensor innovation consistency test.
+hagl_percentage_amber,0.0,The percentage of in-flight height above ground sensor innovation consistency test values > 0.5.
+hagl_percentage_red,0.0,The percentage of in-flight height above ground sensor innovation consistency test values > 1.0.
+hagl_sensor_status,Pass,Height above ground sensor check summary. This sensor data is normally sourced from a rangefinder sensor. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+hagl_test_max,0.15427,The maximum in-flight value of the height above ground sensor innovation consistency test ratio.
+hagl_test_mean,0.0280182,The mean in-flight value of the height above ground sensor innovation consistency test ratio.
+hgt_fail_percentage,0.0,The percentage of in-flight recorded failure events for the height sensor innovation consistency test.
+hgt_percentage_amber,0.0,The percentage of in-flight height sensor innovation consistency test values > 0.5.
+hgt_percentage_red,0.0,The percentage of in-flight height sensor innovation consistency test values > 1.0.
+hgt_sensor_status,Pass,Height sensor check summary. This sensor data can be sourced from either Baro or GPS or range finder or external vision system. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no anomalies were detected and no further investigation is required
+hgt_test_max,0.0720129,The maximum in-flight value of the height sensor innovation consistency test ratio.
+hgt_test_mean,0.0194178,The mean in-flight value of the height sensor innovation consistency test ratio.
+imu_bias_check,Pass,IMU bias check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+imu_coning_mean,1.98248e-06,Mean in-flight value of the IMU delta angle coning vibration metric (rad)
+imu_coning_peak,3.53888e-06,Peak in-flight value of the IMU delta angle coning vibration metric (rad)
+imu_dang_bias_median,1.19677405339e-05,Median in-flight value of the delta angle bias vector length (rad)
+imu_dvel_bias_median,0.0,Median in-flight value of the delta velocity bias vector length (m/s)
+imu_hfdang_mean,0.00245327,Mean in-flight value of the IMU delta angle high frequency vibration metric (rad)
+imu_hfdang_peak,0.00303229,Peak in-flight value of the IMU delta angle high frequency vibration metric (rad)
+imu_hfdvel_mean,0.0267547,Mean in-flight value of the IMU delta velocity high frequency vibration metric (m/s)
+imu_hfdvel_peak,0.0313035,Peak in-flight value of the IMU delta velocity high frequency vibration metric (m/s)
+imu_output_predictor_check,Pass,IMU output predictor check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+imu_sensor_status,Warning,IMU sensor check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+imu_vibration_check,Warning,IMU vibration check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+in_air_transition_time,45.2,The time in seconds measured from startup that the EKF transtioned into in-air mode. Set to a nan if a transition event is not detected.
+mag_percentage_amber,0.0,The percentage of in-flight consolidated magnetic field sensor innovation consistency test values > 0.5.
+mag_percentage_red,0.0,The percentage of in-flight consolidated magnetic field sensor innovation consistency test values > 1.0.
+mag_sensor_status,Pass,Magnetometer sensor check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+mag_test_max,0.244553,The maximum in-flight value of the magnetic field sensor innovation consistency test ratio.
+mag_test_mean,0.0963572,The mean in-flight value of the magnetic field sensor innovation consistency test ratio.
+magx_fail_percentage,0.0,The percentage of in-flight recorded failure events for the X-axis magnetic field sensor innovation consistency test.
+magy_fail_percentage,0.0,The percentage of in-flight recorded failure events for the Y-axis magnetic field sensor innovation consistency test.
+magz_fail_percentage,0.0,The percentage of in-flight recorded failure events for the Z-axis magnetic field sensor innovation consistency test.
+master_status,Warning,Master check status which can be either Pass Warning or Fail. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+ofx_fail_percentage,nan,The percentage of in-flight recorded failure events for the optical flow sensor X-axis innovation consistency test.
+ofy_fail_percentage,nan,The percentage of in-flight recorded failure events for the optical flow sensor Y-axis innovation consistency test.
+on_ground_transition_time,90.6,The time in seconds measured from startup  that the EKF transitioned out of in-air mode. Set to a nan if a transition event is not detected.
+output_obs_ang_err_median,0.000539052,Median in-flight value of the output observer angular error (rad)
+output_obs_pos_err_median,0.0131239,Median in-flight value of the output observer position error (m)
+output_obs_vel_err_median,0.00534568,Median in-flight value of the output observer velocity error (m/s)
+pos_fail_percentage,0.0,The percentage of in-flight recorded failure events for the velocity sensor consolidated innovation consistency test.
+pos_percentage_amber,0.0,The percentage of in-flight position sensor consolidated innovation consistency test values > 0.5.
+pos_percentage_red,0.0,The percentage of in-flight position sensor consolidated innovation consistency test values > 1.0.
+pos_sensor_status,Pass,Position sensor check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+pos_test_max,0.104603,The maximum in-flight value of the position sensor consolidated innovation consistency test ratio.
+pos_test_mean,0.0362503,The mean in-flight value of the position sensor consolidated innovation consistency test ratio.
+tas_fail_percentage,nan,The percentage of in-flight recorded failure events for the airspeed sensor innovation consistency test.
+tas_percentage_amber,nan,The percentage of in-flight airspeed sensor innovation consistency test values > 0.5.
+tas_percentage_red,nan,The percentage of in-flight airspeed sensor innovation consistency test values > 1.0.
+tas_sensor_status,Pass,Airspeed sensor check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+tas_test_max,nan,The maximum in-flight value of the airspeed sensor innovation consistency test ratio.
+tas_test_mean,nan,The mean in-flight value of the airspeed sensor innovation consistency test ratio.
+tilt_align_time,nan,The time in seconds measured from startup that the EKF completed the tilt alignment. A nan value indicates that the alignment had completed before logging started or alignment did not complete.
+vel_fail_percentage,nan,The percentage of in-flight recorded failure events for the velocity sensor consolidated innovation consistency test.
+vel_percentage_amber,nan,The percentage of in-flight velocity sensor consolidated innovation consistency test values > 0.5.
+vel_percentage_red,nan,The percentage of in-flight velocity sensor consolidated innovation consistency test values > 1.0.
+vel_sensor_status,Pass,Velocity sensor check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+vel_test_max,nan,The maximum in-flight value of the velocity sensor consolidated innovation consistency test ratio.
+vel_test_mean,nan,The mean in-flight value of the velocity sensor consolidated innovation consistency test ratio.
+yaw_align_time,nan,The time in seconds measured from startup that the EKF completed the yaw alignment.
+yaw_fail_percentage,0.0,The percentage of in-flight recorded failure events for the yaw sensor innovation consistency test.
+yaw_sensor_status,Pass,Yaw sensor check summary. This sensor data can be sourced from the magnetometer or an external vision system. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required

2018-09-08/17_44_37.ulg.mdat.csv

@@ -0,0 +1,66 @@
+name,value,description
+filter_fault_status,Pass,Internal Filter check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+filter_faults_max,0,Largest recorded value of the filter internal fault bitmask. Should always be zero.
+flow_sensor_status,Pass,Optical Flow sensor check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+hagl_fail_percentage,0.0,The percentage of in-flight recorded failure events for the height above ground sensor innovation consistency test.
+hagl_percentage_amber,0.0,The percentage of in-flight height above ground sensor innovation consistency test values > 0.5.
+hagl_percentage_red,0.0,The percentage of in-flight height above ground sensor innovation consistency test values > 1.0.
+hagl_sensor_status,Pass,Height above ground sensor check summary. This sensor data is normally sourced from a rangefinder sensor. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+hagl_test_max,0.128318,The maximum in-flight value of the height above ground sensor innovation consistency test ratio.
+hagl_test_mean,0.0231392,The mean in-flight value of the height above ground sensor innovation consistency test ratio.
+hgt_fail_percentage,0.0,The percentage of in-flight recorded failure events for the height sensor innovation consistency test.
+hgt_percentage_amber,0.0,The percentage of in-flight height sensor innovation consistency test values > 0.5.
+hgt_percentage_red,0.0,The percentage of in-flight height sensor innovation consistency test values > 1.0.
+hgt_sensor_status,Pass,Height sensor check summary. This sensor data can be sourced from either Baro or GPS or range finder or external vision system. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no anomalies were detected and no further investigation is required
+hgt_test_max,0.0978938,The maximum in-flight value of the height sensor innovation consistency test ratio.
+hgt_test_mean,0.0235257,The mean in-flight value of the height sensor innovation consistency test ratio.
+imu_bias_check,Pass,IMU bias check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+imu_coning_mean,2.10298e-06,Mean in-flight value of the IMU delta angle coning vibration metric (rad)
+imu_coning_peak,3.38798e-06,Peak in-flight value of the IMU delta angle coning vibration metric (rad)
+imu_dang_bias_median,9.27691142555e-06,Median in-flight value of the delta angle bias vector length (rad)
+imu_dvel_bias_median,0.0,Median in-flight value of the delta velocity bias vector length (m/s)
+imu_hfdang_mean,0.00257143,Mean in-flight value of the IMU delta angle high frequency vibration metric (rad)
+imu_hfdang_peak,0.00361732,Peak in-flight value of the IMU delta angle high frequency vibration metric (rad)
+imu_hfdvel_mean,0.0271413,Mean in-flight value of the IMU delta velocity high frequency vibration metric (m/s)
+imu_hfdvel_peak,0.0314668,Peak in-flight value of the IMU delta velocity high frequency vibration metric (m/s)
+imu_output_predictor_check,Pass,IMU output predictor check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+imu_sensor_status,Warning,IMU sensor check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+imu_vibration_check,Warning,IMU vibration check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+in_air_transition_time,87.8,The time in seconds measured from startup that the EKF transtioned into in-air mode. Set to a nan if a transition event is not detected.
+mag_percentage_amber,0.0,The percentage of in-flight consolidated magnetic field sensor innovation consistency test values > 0.5.
+mag_percentage_red,0.0,The percentage of in-flight consolidated magnetic field sensor innovation consistency test values > 1.0.
+mag_sensor_status,Pass,Magnetometer sensor check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+mag_test_max,0.318132,The maximum in-flight value of the magnetic field sensor innovation consistency test ratio.
+mag_test_mean,0.116437,The mean in-flight value of the magnetic field sensor innovation consistency test ratio.
+magx_fail_percentage,0.0,The percentage of in-flight recorded failure events for the X-axis magnetic field sensor innovation consistency test.
+magy_fail_percentage,0.0,The percentage of in-flight recorded failure events for the Y-axis magnetic field sensor innovation consistency test.
+magz_fail_percentage,0.0,The percentage of in-flight recorded failure events for the Z-axis magnetic field sensor innovation consistency test.
+master_status,Warning,Master check status which can be either Pass Warning or Fail. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+ofx_fail_percentage,nan,The percentage of in-flight recorded failure events for the optical flow sensor X-axis innovation consistency test.
+ofy_fail_percentage,nan,The percentage of in-flight recorded failure events for the optical flow sensor Y-axis innovation consistency test.
+on_ground_transition_time,181.7,The time in seconds measured from startup  that the EKF transitioned out of in-air mode. Set to a nan if a transition event is not detected.
+output_obs_ang_err_median,0.00031346,Median in-flight value of the output observer angular error (rad)
+output_obs_pos_err_median,0.00912229,Median in-flight value of the output observer position error (m)
+output_obs_vel_err_median,0.00328942,Median in-flight value of the output observer velocity error (m/s)
+pos_fail_percentage,0.0,The percentage of in-flight recorded failure events for the velocity sensor consolidated innovation consistency test.
+pos_percentage_amber,0.0,The percentage of in-flight position sensor consolidated innovation consistency test values > 0.5.
+pos_percentage_red,0.0,The percentage of in-flight position sensor consolidated innovation consistency test values > 1.0.
+pos_sensor_status,Pass,Position sensor check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+pos_test_max,0.0873154,The maximum in-flight value of the position sensor consolidated innovation consistency test ratio.
+pos_test_mean,0.0209026,The mean in-flight value of the position sensor consolidated innovation consistency test ratio.
+tas_fail_percentage,nan,The percentage of in-flight recorded failure events for the airspeed sensor innovation consistency test.
+tas_percentage_amber,nan,The percentage of in-flight airspeed sensor innovation consistency test values > 0.5.
+tas_percentage_red,nan,The percentage of in-flight airspeed sensor innovation consistency test values > 1.0.
+tas_sensor_status,Pass,Airspeed sensor check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+tas_test_max,nan,The maximum in-flight value of the airspeed sensor innovation consistency test ratio.
+tas_test_mean,nan,The mean in-flight value of the airspeed sensor innovation consistency test ratio.
+tilt_align_time,nan,The time in seconds measured from startup that the EKF completed the tilt alignment. A nan value indicates that the alignment had completed before logging started or alignment did not complete.
+vel_fail_percentage,nan,The percentage of in-flight recorded failure events for the velocity sensor consolidated innovation consistency test.
+vel_percentage_amber,nan,The percentage of in-flight velocity sensor consolidated innovation consistency test values > 0.5.
+vel_percentage_red,nan,The percentage of in-flight velocity sensor consolidated innovation consistency test values > 1.0.
+vel_sensor_status,Pass,Velocity sensor check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+vel_test_max,nan,The maximum in-flight value of the velocity sensor consolidated innovation consistency test ratio.
+vel_test_mean,nan,The mean in-flight value of the velocity sensor consolidated innovation consistency test ratio.
+yaw_align_time,nan,The time in seconds measured from startup that the EKF completed the yaw alignment.
+yaw_fail_percentage,0.0,The percentage of in-flight recorded failure events for the yaw sensor innovation consistency test.
+yaw_sensor_status,Pass,Yaw sensor check summary. This sensor data can be sourced from the magnetometer or an external vision system. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required

2018-09-08/17_48_46.ulg.mdat.csv

@@ -0,0 +1,66 @@
+name,value,description
+filter_fault_status,Pass,Internal Filter check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+filter_faults_max,0,Largest recorded value of the filter internal fault bitmask. Should always be zero.
+flow_sensor_status,Pass,Optical Flow sensor check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+hagl_fail_percentage,0.0,The percentage of in-flight recorded failure events for the height above ground sensor innovation consistency test.
+hagl_percentage_amber,0.0,The percentage of in-flight height above ground sensor innovation consistency test values > 0.5.
+hagl_percentage_red,0.0,The percentage of in-flight height above ground sensor innovation consistency test values > 1.0.
+hagl_sensor_status,Pass,Height above ground sensor check summary. This sensor data is normally sourced from a rangefinder sensor. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+hagl_test_max,0.247265,The maximum in-flight value of the height above ground sensor innovation consistency test ratio.
+hagl_test_mean,0.0283184,The mean in-flight value of the height above ground sensor innovation consistency test ratio.
+hgt_fail_percentage,0.0,The percentage of in-flight recorded failure events for the height sensor innovation consistency test.
+hgt_percentage_amber,0.0,The percentage of in-flight height sensor innovation consistency test values > 0.5.
+hgt_percentage_red,0.0,The percentage of in-flight height sensor innovation consistency test values > 1.0.
+hgt_sensor_status,Pass,Height sensor check summary. This sensor data can be sourced from either Baro or GPS or range finder or external vision system. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no anomalies were detected and no further investigation is required
+hgt_test_max,0.0590948,The maximum in-flight value of the height sensor innovation consistency test ratio.
+hgt_test_mean,0.0193689,The mean in-flight value of the height sensor innovation consistency test ratio.
+imu_bias_check,Pass,IMU bias check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+imu_coning_mean,2.28193e-06,Mean in-flight value of the IMU delta angle coning vibration metric (rad)
+imu_coning_peak,4.00088e-06,Peak in-flight value of the IMU delta angle coning vibration metric (rad)
+imu_dang_bias_median,2.20183078586e-05,Median in-flight value of the delta angle bias vector length (rad)
+imu_dvel_bias_median,0.0,Median in-flight value of the delta velocity bias vector length (m/s)
+imu_hfdang_mean,0.00261232,Mean in-flight value of the IMU delta angle high frequency vibration metric (rad)
+imu_hfdang_peak,0.00378122,Peak in-flight value of the IMU delta angle high frequency vibration metric (rad)
+imu_hfdvel_mean,0.0275722,Mean in-flight value of the IMU delta velocity high frequency vibration metric (m/s)
+imu_hfdvel_peak,0.0318854,Peak in-flight value of the IMU delta velocity high frequency vibration metric (m/s)
+imu_output_predictor_check,Pass,IMU output predictor check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+imu_sensor_status,Warning,IMU sensor check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+imu_vibration_check,Warning,IMU vibration check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+in_air_transition_time,92.7,The time in seconds measured from startup that the EKF transtioned into in-air mode. Set to a nan if a transition event is not detected.
+mag_percentage_amber,0.0,The percentage of in-flight consolidated magnetic field sensor innovation consistency test values > 0.5.
+mag_percentage_red,0.0,The percentage of in-flight consolidated magnetic field sensor innovation consistency test values > 1.0.
+mag_sensor_status,Pass,Magnetometer sensor check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+mag_test_max,0.388647,The maximum in-flight value of the magnetic field sensor innovation consistency test ratio.
+mag_test_mean,0.12379,The mean in-flight value of the magnetic field sensor innovation consistency test ratio.
+magx_fail_percentage,0.0,The percentage of in-flight recorded failure events for the X-axis magnetic field sensor innovation consistency test.
+magy_fail_percentage,0.0,The percentage of in-flight recorded failure events for the Y-axis magnetic field sensor innovation consistency test.
+magz_fail_percentage,0.0,The percentage of in-flight recorded failure events for the Z-axis magnetic field sensor innovation consistency test.
+master_status,Warning,Master check status which can be either Pass Warning or Fail. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+ofx_fail_percentage,nan,The percentage of in-flight recorded failure events for the optical flow sensor X-axis innovation consistency test.
+ofy_fail_percentage,nan,The percentage of in-flight recorded failure events for the optical flow sensor Y-axis innovation consistency test.
+on_ground_transition_time,130.0,The time in seconds measured from startup  that the EKF transitioned out of in-air mode. Set to a nan if a transition event is not detected.
+output_obs_ang_err_median,0.000603634,Median in-flight value of the output observer angular error (rad)
+output_obs_pos_err_median,0.0237932,Median in-flight value of the output observer position error (m)
+output_obs_vel_err_median,0.00994645,Median in-flight value of the output observer velocity error (m/s)
+pos_fail_percentage,0.0,The percentage of in-flight recorded failure events for the velocity sensor consolidated innovation consistency test.
+pos_percentage_amber,0.0,The percentage of in-flight position sensor consolidated innovation consistency test values > 0.5.
+pos_percentage_red,0.0,The percentage of in-flight position sensor consolidated innovation consistency test values > 1.0.
+pos_sensor_status,Pass,Position sensor check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+pos_test_max,0.113635,The maximum in-flight value of the position sensor consolidated innovation consistency test ratio.
+pos_test_mean,0.0353749,The mean in-flight value of the position sensor consolidated innovation consistency test ratio.
+tas_fail_percentage,nan,The percentage of in-flight recorded failure events for the airspeed sensor innovation consistency test.
+tas_percentage_amber,nan,The percentage of in-flight airspeed sensor innovation consistency test values > 0.5.
+tas_percentage_red,nan,The percentage of in-flight airspeed sensor innovation consistency test values > 1.0.
+tas_sensor_status,Pass,Airspeed sensor check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+tas_test_max,nan,The maximum in-flight value of the airspeed sensor innovation consistency test ratio.
+tas_test_mean,nan,The mean in-flight value of the airspeed sensor innovation consistency test ratio.
+tilt_align_time,nan,The time in seconds measured from startup that the EKF completed the tilt alignment. A nan value indicates that the alignment had completed before logging started or alignment did not complete.
+vel_fail_percentage,nan,The percentage of in-flight recorded failure events for the velocity sensor consolidated innovation consistency test.
+vel_percentage_amber,nan,The percentage of in-flight velocity sensor consolidated innovation consistency test values > 0.5.
+vel_percentage_red,nan,The percentage of in-flight velocity sensor consolidated innovation consistency test values > 1.0.
+vel_sensor_status,Pass,Velocity sensor check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+vel_test_max,nan,The maximum in-flight value of the velocity sensor consolidated innovation consistency test ratio.
+vel_test_mean,nan,The mean in-flight value of the velocity sensor consolidated innovation consistency test ratio.
+yaw_align_time,nan,The time in seconds measured from startup that the EKF completed the yaw alignment.
+yaw_fail_percentage,0.0,The percentage of in-flight recorded failure events for the yaw sensor innovation consistency test.
+yaw_sensor_status,Pass,Yaw sensor check summary. This sensor data can be sourced from the magnetometer or an external vision system. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required

2018-09-08/17_50_22.ulg.mdat.csv

@@ -0,0 +1,66 @@
+name,value,description
+filter_fault_status,Pass,Internal Filter check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+filter_faults_max,0,Largest recorded value of the filter internal fault bitmask. Should always be zero.
+flow_sensor_status,Pass,Optical Flow sensor check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+hagl_fail_percentage,0.0,The percentage of in-flight recorded failure events for the height above ground sensor innovation consistency test.
+hagl_percentage_amber,0.0,The percentage of in-flight height above ground sensor innovation consistency test values > 0.5.
+hagl_percentage_red,0.0,The percentage of in-flight height above ground sensor innovation consistency test values > 1.0.
+hagl_sensor_status,Pass,Height above ground sensor check summary. This sensor data is normally sourced from a rangefinder sensor. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+hagl_test_max,0.160513,The maximum in-flight value of the height above ground sensor innovation consistency test ratio.
+hagl_test_mean,0.0229894,The mean in-flight value of the height above ground sensor innovation consistency test ratio.
+hgt_fail_percentage,0.0,The percentage of in-flight recorded failure events for the height sensor innovation consistency test.
+hgt_percentage_amber,0.0,The percentage of in-flight height sensor innovation consistency test values > 0.5.
+hgt_percentage_red,0.0,The percentage of in-flight height sensor innovation consistency test values > 1.0.
+hgt_sensor_status,Pass,Height sensor check summary. This sensor data can be sourced from either Baro or GPS or range finder or external vision system. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no anomalies were detected and no further investigation is required
+hgt_test_max,0.0847849,The maximum in-flight value of the height sensor innovation consistency test ratio.
+hgt_test_mean,0.0206276,The mean in-flight value of the height sensor innovation consistency test ratio.
+imu_bias_check,Pass,IMU bias check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+imu_coning_mean,2.29647e-06,Mean in-flight value of the IMU delta angle coning vibration metric (rad)
+imu_coning_peak,8.45576e-06,Peak in-flight value of the IMU delta angle coning vibration metric (rad)
+imu_dang_bias_median,1.22847264254e-05,Median in-flight value of the delta angle bias vector length (rad)
+imu_dvel_bias_median,0.0,Median in-flight value of the delta velocity bias vector length (m/s)
+imu_hfdang_mean,0.0025885,Mean in-flight value of the IMU delta angle high frequency vibration metric (rad)
+imu_hfdang_peak,0.00370104,Peak in-flight value of the IMU delta angle high frequency vibration metric (rad)
+imu_hfdvel_mean,0.0274591,Mean in-flight value of the IMU delta velocity high frequency vibration metric (m/s)
+imu_hfdvel_peak,0.0328202,Peak in-flight value of the IMU delta velocity high frequency vibration metric (m/s)
+imu_output_predictor_check,Pass,IMU output predictor check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+imu_sensor_status,Warning,IMU sensor check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+imu_vibration_check,Warning,IMU vibration check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+in_air_transition_time,38.0,The time in seconds measured from startup that the EKF transtioned into in-air mode. Set to a nan if a transition event is not detected.
+mag_percentage_amber,0.0,The percentage of in-flight consolidated magnetic field sensor innovation consistency test values > 0.5.
+mag_percentage_red,0.0,The percentage of in-flight consolidated magnetic field sensor innovation consistency test values > 1.0.
+mag_sensor_status,Pass,Magnetometer sensor check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+mag_test_max,0.432617,The maximum in-flight value of the magnetic field sensor innovation consistency test ratio.
+mag_test_mean,0.0863485,The mean in-flight value of the magnetic field sensor innovation consistency test ratio.
+magx_fail_percentage,0.0,The percentage of in-flight recorded failure events for the X-axis magnetic field sensor innovation consistency test.
+magy_fail_percentage,0.0,The percentage of in-flight recorded failure events for the Y-axis magnetic field sensor innovation consistency test.
+magz_fail_percentage,0.0,The percentage of in-flight recorded failure events for the Z-axis magnetic field sensor innovation consistency test.
+master_status,Warning,Master check status which can be either Pass Warning or Fail. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+ofx_fail_percentage,nan,The percentage of in-flight recorded failure events for the optical flow sensor X-axis innovation consistency test.
+ofy_fail_percentage,nan,The percentage of in-flight recorded failure events for the optical flow sensor Y-axis innovation consistency test.
+on_ground_transition_time,144.7,The time in seconds measured from startup  that the EKF transitioned out of in-air mode. Set to a nan if a transition event is not detected.
+output_obs_ang_err_median,0.000227143,Median in-flight value of the output observer angular error (rad)
+output_obs_pos_err_median,0.00872288,Median in-flight value of the output observer position error (m)
+output_obs_vel_err_median,0.00311547,Median in-flight value of the output observer velocity error (m/s)
+pos_fail_percentage,0.0,The percentage of in-flight recorded failure events for the velocity sensor consolidated innovation consistency test.
+pos_percentage_amber,0.0,The percentage of in-flight position sensor consolidated innovation consistency test values > 0.5.
+pos_percentage_red,0.0,The percentage of in-flight position sensor consolidated innovation consistency test values > 1.0.
+pos_sensor_status,Pass,Position sensor check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+pos_test_max,0.100301,The maximum in-flight value of the position sensor consolidated innovation consistency test ratio.
+pos_test_mean,0.0203211,The mean in-flight value of the position sensor consolidated innovation consistency test ratio.
+tas_fail_percentage,nan,The percentage of in-flight recorded failure events for the airspeed sensor innovation consistency test.
+tas_percentage_amber,nan,The percentage of in-flight airspeed sensor innovation consistency test values > 0.5.
+tas_percentage_red,nan,The percentage of in-flight airspeed sensor innovation consistency test values > 1.0.
+tas_sensor_status,Pass,Airspeed sensor check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+tas_test_max,nan,The maximum in-flight value of the airspeed sensor innovation consistency test ratio.
+tas_test_mean,nan,The mean in-flight value of the airspeed sensor innovation consistency test ratio.
+tilt_align_time,nan,The time in seconds measured from startup that the EKF completed the tilt alignment. A nan value indicates that the alignment had completed before logging started or alignment did not complete.
+vel_fail_percentage,nan,The percentage of in-flight recorded failure events for the velocity sensor consolidated innovation consistency test.
+vel_percentage_amber,nan,The percentage of in-flight velocity sensor consolidated innovation consistency test values > 0.5.
+vel_percentage_red,nan,The percentage of in-flight velocity sensor consolidated innovation consistency test values > 1.0.
+vel_sensor_status,Pass,Velocity sensor check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+vel_test_max,nan,The maximum in-flight value of the velocity sensor consolidated innovation consistency test ratio.
+vel_test_mean,nan,The mean in-flight value of the velocity sensor consolidated innovation consistency test ratio.
+yaw_align_time,nan,The time in seconds measured from startup that the EKF completed the yaw alignment.
+yaw_fail_percentage,0.0,The percentage of in-flight recorded failure events for the yaw sensor innovation consistency test.
+yaw_sensor_status,Pass,Yaw sensor check summary. This sensor data can be sourced from the magnetometer or an external vision system. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required

2018-09-08/17_58_39.ulg.mdat.csv

@@ -0,0 +1,66 @@
+name,value,description
+filter_fault_status,Pass,Internal Filter check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+filter_faults_max,0,Largest recorded value of the filter internal fault bitmask. Should always be zero.
+flow_sensor_status,Pass,Optical Flow sensor check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+hagl_fail_percentage,0.0,The percentage of in-flight recorded failure events for the height above ground sensor innovation consistency test.
+hagl_percentage_amber,0.0,The percentage of in-flight height above ground sensor innovation consistency test values > 0.5.
+hagl_percentage_red,0.0,The percentage of in-flight height above ground sensor innovation consistency test values > 1.0.
+hagl_sensor_status,Pass,Height above ground sensor check summary. This sensor data is normally sourced from a rangefinder sensor. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+hagl_test_max,0.194772,The maximum in-flight value of the height above ground sensor innovation consistency test ratio.
+hagl_test_mean,0.0250334,The mean in-flight value of the height above ground sensor innovation consistency test ratio.
+hgt_fail_percentage,0.0,The percentage of in-flight recorded failure events for the height sensor innovation consistency test.
+hgt_percentage_amber,0.0,The percentage of in-flight height sensor innovation consistency test values > 0.5.
+hgt_percentage_red,0.0,The percentage of in-flight height sensor innovation consistency test values > 1.0.
+hgt_sensor_status,Pass,Height sensor check summary. This sensor data can be sourced from either Baro or GPS or range finder or external vision system. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no anomalies were detected and no further investigation is required
+hgt_test_max,0.0724525,The maximum in-flight value of the height sensor innovation consistency test ratio.
+hgt_test_mean,0.0213812,The mean in-flight value of the height sensor innovation consistency test ratio.
+imu_bias_check,Pass,IMU bias check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+imu_coning_mean,2.24983e-06,Mean in-flight value of the IMU delta angle coning vibration metric (rad)
+imu_coning_peak,4.80312e-06,Peak in-flight value of the IMU delta angle coning vibration metric (rad)
+imu_dang_bias_median,2.78798076678e-05,Median in-flight value of the delta angle bias vector length (rad)
+imu_dvel_bias_median,0.0,Median in-flight value of the delta velocity bias vector length (m/s)
+imu_hfdang_mean,0.00263146,Mean in-flight value of the IMU delta angle high frequency vibration metric (rad)
+imu_hfdang_peak,0.00413657,Peak in-flight value of the IMU delta angle high frequency vibration metric (rad)
+imu_hfdvel_mean,0.0275508,Mean in-flight value of the IMU delta velocity high frequency vibration metric (m/s)
+imu_hfdvel_peak,0.0302137,Peak in-flight value of the IMU delta velocity high frequency vibration metric (m/s)
+imu_output_predictor_check,Pass,IMU output predictor check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+imu_sensor_status,Warning,IMU sensor check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+imu_vibration_check,Warning,IMU vibration check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+in_air_transition_time,47.3,The time in seconds measured from startup that the EKF transtioned into in-air mode. Set to a nan if a transition event is not detected.
+mag_percentage_amber,0.0,The percentage of in-flight consolidated magnetic field sensor innovation consistency test values > 0.5.
+mag_percentage_red,0.0,The percentage of in-flight consolidated magnetic field sensor innovation consistency test values > 1.0.
+mag_sensor_status,Pass,Magnetometer sensor check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+mag_test_max,0.202728,The maximum in-flight value of the magnetic field sensor innovation consistency test ratio.
+mag_test_mean,0.109101,The mean in-flight value of the magnetic field sensor innovation consistency test ratio.
+magx_fail_percentage,0.0,The percentage of in-flight recorded failure events for the X-axis magnetic field sensor innovation consistency test.
+magy_fail_percentage,0.0,The percentage of in-flight recorded failure events for the Y-axis magnetic field sensor innovation consistency test.
+magz_fail_percentage,0.0,The percentage of in-flight recorded failure events for the Z-axis magnetic field sensor innovation consistency test.
+master_status,Fail,Master check status which can be either Pass Warning or Fail. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+ofx_fail_percentage,nan,The percentage of in-flight recorded failure events for the optical flow sensor X-axis innovation consistency test.
+ofy_fail_percentage,nan,The percentage of in-flight recorded failure events for the optical flow sensor Y-axis innovation consistency test.
+on_ground_transition_time,81.3,The time in seconds measured from startup  that the EKF transitioned out of in-air mode. Set to a nan if a transition event is not detected.
+output_obs_ang_err_median,0.000341057,Median in-flight value of the output observer angular error (rad)
+output_obs_pos_err_median,0.0154077,Median in-flight value of the output observer position error (m)
+output_obs_vel_err_median,0.00908425,Median in-flight value of the output observer velocity error (m/s)
+pos_fail_percentage,20.8333333333,The percentage of in-flight recorded failure events for the velocity sensor consolidated innovation consistency test.
+pos_percentage_amber,5.95238095238,The percentage of in-flight position sensor consolidated innovation consistency test values > 0.5.
+pos_percentage_red,20.8333333333,The percentage of in-flight position sensor consolidated innovation consistency test values > 1.0.
+pos_sensor_status,Fail,Position sensor check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+pos_test_max,11.6235,The maximum in-flight value of the position sensor consolidated innovation consistency test ratio.
+pos_test_mean,0.795533,The mean in-flight value of the position sensor consolidated innovation consistency test ratio.
+tas_fail_percentage,nan,The percentage of in-flight recorded failure events for the airspeed sensor innovation consistency test.
+tas_percentage_amber,nan,The percentage of in-flight airspeed sensor innovation consistency test values > 0.5.
+tas_percentage_red,nan,The percentage of in-flight airspeed sensor innovation consistency test values > 1.0.
+tas_sensor_status,Pass,Airspeed sensor check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+tas_test_max,nan,The maximum in-flight value of the airspeed sensor innovation consistency test ratio.
+tas_test_mean,nan,The mean in-flight value of the airspeed sensor innovation consistency test ratio.
+tilt_align_time,nan,The time in seconds measured from startup that the EKF completed the tilt alignment. A nan value indicates that the alignment had completed before logging started or alignment did not complete.
+vel_fail_percentage,nan,The percentage of in-flight recorded failure events for the velocity sensor consolidated innovation consistency test.
+vel_percentage_amber,nan,The percentage of in-flight velocity sensor consolidated innovation consistency test values > 0.5.
+vel_percentage_red,nan,The percentage of in-flight velocity sensor consolidated innovation consistency test values > 1.0.
+vel_sensor_status,Pass,Velocity sensor check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+vel_test_max,nan,The maximum in-flight value of the velocity sensor consolidated innovation consistency test ratio.
+vel_test_mean,nan,The mean in-flight value of the velocity sensor consolidated innovation consistency test ratio.
+yaw_align_time,nan,The time in seconds measured from startup that the EKF completed the yaw alignment.
+yaw_fail_percentage,0.0,The percentage of in-flight recorded failure events for the yaw sensor innovation consistency test.
+yaw_sensor_status,Pass,Yaw sensor check summary. This sensor data can be sourced from the magnetometer or an external vision system. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required

2018-09-08/18_01_14.ulg.mdat.csv

@@ -0,0 +1,66 @@
+name,value,description
+filter_fault_status,Pass,Internal Filter check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+filter_faults_max,0,Largest recorded value of the filter internal fault bitmask. Should always be zero.
+flow_sensor_status,Pass,Optical Flow sensor check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+hagl_fail_percentage,0.0,The percentage of in-flight recorded failure events for the height above ground sensor innovation consistency test.
+hagl_percentage_amber,0.0,The percentage of in-flight height above ground sensor innovation consistency test values > 0.5.
+hagl_percentage_red,0.0,The percentage of in-flight height above ground sensor innovation consistency test values > 1.0.
+hagl_sensor_status,Pass,Height above ground sensor check summary. This sensor data is normally sourced from a rangefinder sensor. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+hagl_test_max,0.147743,The maximum in-flight value of the height above ground sensor innovation consistency test ratio.
+hagl_test_mean,0.0221183,The mean in-flight value of the height above ground sensor innovation consistency test ratio.
+hgt_fail_percentage,0.0,The percentage of in-flight recorded failure events for the height sensor innovation consistency test.
+hgt_percentage_amber,0.0,The percentage of in-flight height sensor innovation consistency test values > 0.5.
+hgt_percentage_red,0.0,The percentage of in-flight height sensor innovation consistency test values > 1.0.
+hgt_sensor_status,Pass,Height sensor check summary. This sensor data can be sourced from either Baro or GPS or range finder or external vision system. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no anomalies were detected and no further investigation is required
+hgt_test_max,0.0550056,The maximum in-flight value of the height sensor innovation consistency test ratio.
+hgt_test_mean,0.0203559,The mean in-flight value of the height sensor innovation consistency test ratio.
+imu_bias_check,Pass,IMU bias check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+imu_coning_mean,2.30062e-06,Mean in-flight value of the IMU delta angle coning vibration metric (rad)
+imu_coning_peak,4.2969e-06,Peak in-flight value of the IMU delta angle coning vibration metric (rad)
+imu_dang_bias_median,1.57265770656e-05,Median in-flight value of the delta angle bias vector length (rad)
+imu_dvel_bias_median,0.0,Median in-flight value of the delta velocity bias vector length (m/s)
+imu_hfdang_mean,0.00274852,Mean in-flight value of the IMU delta angle high frequency vibration metric (rad)
+imu_hfdang_peak,0.00375201,Peak in-flight value of the IMU delta angle high frequency vibration metric (rad)
+imu_hfdvel_mean,0.0280242,Mean in-flight value of the IMU delta velocity high frequency vibration metric (m/s)
+imu_hfdvel_peak,0.031483,Peak in-flight value of the IMU delta velocity high frequency vibration metric (m/s)
+imu_output_predictor_check,Pass,IMU output predictor check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+imu_sensor_status,Warning,IMU sensor check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+imu_vibration_check,Warning,IMU vibration check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+in_air_transition_time,64.0,The time in seconds measured from startup that the EKF transtioned into in-air mode. Set to a nan if a transition event is not detected.
+mag_percentage_amber,0.0,The percentage of in-flight consolidated magnetic field sensor innovation consistency test values > 0.5.
+mag_percentage_red,0.0,The percentage of in-flight consolidated magnetic field sensor innovation consistency test values > 1.0.
+mag_sensor_status,Pass,Magnetometer sensor check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+mag_test_max,0.135816,The maximum in-flight value of the magnetic field sensor innovation consistency test ratio.
+mag_test_mean,0.0670108,The mean in-flight value of the magnetic field sensor innovation consistency test ratio.
+magx_fail_percentage,0.0,The percentage of in-flight recorded failure events for the X-axis magnetic field sensor innovation consistency test.
+magy_fail_percentage,0.0,The percentage of in-flight recorded failure events for the Y-axis magnetic field sensor innovation consistency test.
+magz_fail_percentage,0.0,The percentage of in-flight recorded failure events for the Z-axis magnetic field sensor innovation consistency test.
+master_status,Warning,Master check status which can be either Pass Warning or Fail. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+ofx_fail_percentage,nan,The percentage of in-flight recorded failure events for the optical flow sensor X-axis innovation consistency test.
+ofy_fail_percentage,nan,The percentage of in-flight recorded failure events for the optical flow sensor Y-axis innovation consistency test.
+on_ground_transition_time,98.4,The time in seconds measured from startup  that the EKF transitioned out of in-air mode. Set to a nan if a transition event is not detected.
+output_obs_ang_err_median,0.000247483,Median in-flight value of the output observer angular error (rad)
+output_obs_pos_err_median,0.0225547,Median in-flight value of the output observer position error (m)
+output_obs_vel_err_median,0.00941124,Median in-flight value of the output observer velocity error (m/s)
+pos_fail_percentage,0.0,The percentage of in-flight recorded failure events for the velocity sensor consolidated innovation consistency test.
+pos_percentage_amber,0.0,The percentage of in-flight position sensor consolidated innovation consistency test values > 0.5.
+pos_percentage_red,0.0,The percentage of in-flight position sensor consolidated innovation consistency test values > 1.0.
+pos_sensor_status,Pass,Position sensor check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+pos_test_max,0.141372,The maximum in-flight value of the position sensor consolidated innovation consistency test ratio.
+pos_test_mean,0.0664136,The mean in-flight value of the position sensor consolidated innovation consistency test ratio.
+tas_fail_percentage,nan,The percentage of in-flight recorded failure events for the airspeed sensor innovation consistency test.
+tas_percentage_amber,nan,The percentage of in-flight airspeed sensor innovation consistency test values > 0.5.
+tas_percentage_red,nan,The percentage of in-flight airspeed sensor innovation consistency test values > 1.0.
+tas_sensor_status,Pass,Airspeed sensor check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+tas_test_max,nan,The maximum in-flight value of the airspeed sensor innovation consistency test ratio.
+tas_test_mean,nan,The mean in-flight value of the airspeed sensor innovation consistency test ratio.
+tilt_align_time,nan,The time in seconds measured from startup that the EKF completed the tilt alignment. A nan value indicates that the alignment had completed before logging started or alignment did not complete.
+vel_fail_percentage,nan,The percentage of in-flight recorded failure events for the velocity sensor consolidated innovation consistency test.
+vel_percentage_amber,nan,The percentage of in-flight velocity sensor consolidated innovation consistency test values > 0.5.
+vel_percentage_red,nan,The percentage of in-flight velocity sensor consolidated innovation consistency test values > 1.0.
+vel_sensor_status,Pass,Velocity sensor check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+vel_test_max,nan,The maximum in-flight value of the velocity sensor consolidated innovation consistency test ratio.
+vel_test_mean,nan,The mean in-flight value of the velocity sensor consolidated innovation consistency test ratio.
+yaw_align_time,nan,The time in seconds measured from startup that the EKF completed the yaw alignment.
+yaw_fail_percentage,0.0,The percentage of in-flight recorded failure events for the yaw sensor innovation consistency test.
+yaw_sensor_status,Pass,Yaw sensor check summary. This sensor data can be sourced from the magnetometer or an external vision system. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required

2018-09-08/18_03_08.ulg.mdat.csv

@@ -0,0 +1,66 @@
+name,value,description
+filter_fault_status,Pass,Internal Filter check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+filter_faults_max,0,Largest recorded value of the filter internal fault bitmask. Should always be zero.
+flow_sensor_status,Pass,Optical Flow sensor check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+hagl_fail_percentage,nan,The percentage of in-flight recorded failure events for the height above ground sensor innovation consistency test.
+hagl_percentage_amber,nan,The percentage of in-flight height above ground sensor innovation consistency test values > 0.5.
+hagl_percentage_red,nan,The percentage of in-flight height above ground sensor innovation consistency test values > 1.0.
+hagl_sensor_status,Pass,Height above ground sensor check summary. This sensor data is normally sourced from a rangefinder sensor. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+hagl_test_max,nan,The maximum in-flight value of the height above ground sensor innovation consistency test ratio.
+hagl_test_mean,nan,The mean in-flight value of the height above ground sensor innovation consistency test ratio.
+hgt_fail_percentage,nan,The percentage of in-flight recorded failure events for the height sensor innovation consistency test.
+hgt_percentage_amber,nan,The percentage of in-flight height sensor innovation consistency test values > 0.5.
+hgt_percentage_red,nan,The percentage of in-flight height sensor innovation consistency test values > 1.0.
+hgt_sensor_status,Pass,Height sensor check summary. This sensor data can be sourced from either Baro or GPS or range finder or external vision system. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no anomalies were detected and no further investigation is required
+hgt_test_max,nan,The maximum in-flight value of the height sensor innovation consistency test ratio.
+hgt_test_mean,nan,The mean in-flight value of the height sensor innovation consistency test ratio.
+imu_bias_check,Pass,IMU bias check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+imu_coning_mean,nan,Mean in-flight value of the IMU delta angle coning vibration metric (rad)
+imu_coning_peak,nan,Peak in-flight value of the IMU delta angle coning vibration metric (rad)
+imu_dang_bias_median,nan,Median in-flight value of the delta angle bias vector length (rad)
+imu_dvel_bias_median,nan,Median in-flight value of the delta velocity bias vector length (m/s)
+imu_hfdang_mean,nan,Mean in-flight value of the IMU delta angle high frequency vibration metric (rad)
+imu_hfdang_peak,nan,Peak in-flight value of the IMU delta angle high frequency vibration metric (rad)
+imu_hfdvel_mean,nan,Mean in-flight value of the IMU delta velocity high frequency vibration metric (m/s)
+imu_hfdvel_peak,nan,Peak in-flight value of the IMU delta velocity high frequency vibration metric (m/s)
+imu_output_predictor_check,Pass,IMU output predictor check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+imu_sensor_status,Pass,IMU sensor check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+imu_vibration_check,Pass,IMU vibration check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+in_air_transition_time,35.1,The time in seconds measured from startup that the EKF transtioned into in-air mode. Set to a nan if a transition event is not detected.
+mag_percentage_amber,nan,The percentage of in-flight consolidated magnetic field sensor innovation consistency test values > 0.5.
+mag_percentage_red,nan,The percentage of in-flight consolidated magnetic field sensor innovation consistency test values > 1.0.
+mag_sensor_status,Pass,Magnetometer sensor check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+mag_test_max,nan,The maximum in-flight value of the magnetic field sensor innovation consistency test ratio.
+mag_test_mean,nan,The mean in-flight value of the magnetic field sensor innovation consistency test ratio.
+magx_fail_percentage,nan,The percentage of in-flight recorded failure events for the X-axis magnetic field sensor innovation consistency test.
+magy_fail_percentage,nan,The percentage of in-flight recorded failure events for the Y-axis magnetic field sensor innovation consistency test.
+magz_fail_percentage,nan,The percentage of in-flight recorded failure events for the Z-axis magnetic field sensor innovation consistency test.
+master_status,Pass,Master check status which can be either Pass Warning or Fail. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+ofx_fail_percentage,nan,The percentage of in-flight recorded failure events for the optical flow sensor X-axis innovation consistency test.
+ofy_fail_percentage,nan,The percentage of in-flight recorded failure events for the optical flow sensor Y-axis innovation consistency test.
+on_ground_transition_time,64.9,The time in seconds measured from startup  that the EKF transitioned out of in-air mode. Set to a nan if a transition event is not detected.
+output_obs_ang_err_median,nan,Median in-flight value of the output observer angular error (rad)
+output_obs_pos_err_median,nan,Median in-flight value of the output observer position error (m)
+output_obs_vel_err_median,nan,Median in-flight value of the output observer velocity error (m/s)
+pos_fail_percentage,nan,The percentage of in-flight recorded failure events for the velocity sensor consolidated innovation consistency test.
+pos_percentage_amber,nan,The percentage of in-flight position sensor consolidated innovation consistency test values > 0.5.
+pos_percentage_red,nan,The percentage of in-flight position sensor consolidated innovation consistency test values > 1.0.
+pos_sensor_status,Pass,Position sensor check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+pos_test_max,nan,The maximum in-flight value of the position sensor consolidated innovation consistency test ratio.
+pos_test_mean,nan,The mean in-flight value of the position sensor consolidated innovation consistency test ratio.
+tas_fail_percentage,nan,The percentage of in-flight recorded failure events for the airspeed sensor innovation consistency test.
+tas_percentage_amber,nan,The percentage of in-flight airspeed sensor innovation consistency test values > 0.5.
+tas_percentage_red,nan,The percentage of in-flight airspeed sensor innovation consistency test values > 1.0.
+tas_sensor_status,Pass,Airspeed sensor check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+tas_test_max,nan,The maximum in-flight value of the airspeed sensor innovation consistency test ratio.
+tas_test_mean,nan,The mean in-flight value of the airspeed sensor innovation consistency test ratio.
+tilt_align_time,nan,The time in seconds measured from startup that the EKF completed the tilt alignment. A nan value indicates that the alignment had completed before logging started or alignment did not complete.
+vel_fail_percentage,nan,The percentage of in-flight recorded failure events for the velocity sensor consolidated innovation consistency test.
+vel_percentage_amber,nan,The percentage of in-flight velocity sensor consolidated innovation consistency test values > 0.5.
+vel_percentage_red,nan,The percentage of in-flight velocity sensor consolidated innovation consistency test values > 1.0.
+vel_sensor_status,Pass,Velocity sensor check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+vel_test_max,nan,The maximum in-flight value of the velocity sensor consolidated innovation consistency test ratio.
+vel_test_mean,nan,The mean in-flight value of the velocity sensor consolidated innovation consistency test ratio.
+yaw_align_time,nan,The time in seconds measured from startup that the EKF completed the yaw alignment.
+yaw_fail_percentage,nan,The percentage of in-flight recorded failure events for the yaw sensor innovation consistency test.
+yaw_sensor_status,Pass,Yaw sensor check summary. This sensor data can be sourced from the magnetometer or an external vision system. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required

2018-09-08/18_07_55.ulg.mdat.csv

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+name,value,description
+filter_fault_status,Pass,Internal Filter check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+filter_faults_max,0,Largest recorded value of the filter internal fault bitmask. Should always be zero.
+flow_sensor_status,Pass,Optical Flow sensor check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+hagl_fail_percentage,0.0,The percentage of in-flight recorded failure events for the height above ground sensor innovation consistency test.
+hagl_percentage_amber,0.0,The percentage of in-flight height above ground sensor innovation consistency test values > 0.5.
+hagl_percentage_red,0.0,The percentage of in-flight height above ground sensor innovation consistency test values > 1.0.
+hagl_sensor_status,Pass,Height above ground sensor check summary. This sensor data is normally sourced from a rangefinder sensor. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+hagl_test_max,0.163596,The maximum in-flight value of the height above ground sensor innovation consistency test ratio.
+hagl_test_mean,0.0232966,The mean in-flight value of the height above ground sensor innovation consistency test ratio.
+hgt_fail_percentage,0.0,The percentage of in-flight recorded failure events for the height sensor innovation consistency test.
+hgt_percentage_amber,0.0,The percentage of in-flight height sensor innovation consistency test values > 0.5.
+hgt_percentage_red,0.0,The percentage of in-flight height sensor innovation consistency test values > 1.0.
+hgt_sensor_status,Pass,Height sensor check summary. This sensor data can be sourced from either Baro or GPS or range finder or external vision system. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no anomalies were detected and no further investigation is required
+hgt_test_max,0.0651768,The maximum in-flight value of the height sensor innovation consistency test ratio.
+hgt_test_mean,0.0166364,The mean in-flight value of the height sensor innovation consistency test ratio.
+imu_bias_check,Pass,IMU bias check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+imu_coning_mean,1.74432e-06,Mean in-flight value of the IMU delta angle coning vibration metric (rad)
+imu_coning_peak,5.72391e-06,Peak in-flight value of the IMU delta angle coning vibration metric (rad)
+imu_dang_bias_median,2.11688191313e-05,Median in-flight value of the delta angle bias vector length (rad)
+imu_dvel_bias_median,0.0,Median in-flight value of the delta velocity bias vector length (m/s)
+imu_hfdang_mean,0.00229468,Mean in-flight value of the IMU delta angle high frequency vibration metric (rad)
+imu_hfdang_peak,0.00289503,Peak in-flight value of the IMU delta angle high frequency vibration metric (rad)
+imu_hfdvel_mean,0.0254264,Mean in-flight value of the IMU delta velocity high frequency vibration metric (m/s)
+imu_hfdvel_peak,0.0285985,Peak in-flight value of the IMU delta velocity high frequency vibration metric (m/s)
+imu_output_predictor_check,Pass,IMU output predictor check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+imu_sensor_status,Warning,IMU sensor check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+imu_vibration_check,Warning,IMU vibration check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+in_air_transition_time,139.1,The time in seconds measured from startup that the EKF transtioned into in-air mode. Set to a nan if a transition event is not detected.
+mag_percentage_amber,0.0,The percentage of in-flight consolidated magnetic field sensor innovation consistency test values > 0.5.
+mag_percentage_red,0.0,The percentage of in-flight consolidated magnetic field sensor innovation consistency test values > 1.0.
+mag_sensor_status,Pass,Magnetometer sensor check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+mag_test_max,0.282691,The maximum in-flight value of the magnetic field sensor innovation consistency test ratio.
+mag_test_mean,0.0852875,The mean in-flight value of the magnetic field sensor innovation consistency test ratio.
+magx_fail_percentage,0.0,The percentage of in-flight recorded failure events for the X-axis magnetic field sensor innovation consistency test.
+magy_fail_percentage,0.0,The percentage of in-flight recorded failure events for the Y-axis magnetic field sensor innovation consistency test.
+magz_fail_percentage,0.0,The percentage of in-flight recorded failure events for the Z-axis magnetic field sensor innovation consistency test.
+master_status,Warning,Master check status which can be either Pass Warning or Fail. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+ofx_fail_percentage,nan,The percentage of in-flight recorded failure events for the optical flow sensor X-axis innovation consistency test.
+ofy_fail_percentage,nan,The percentage of in-flight recorded failure events for the optical flow sensor Y-axis innovation consistency test.
+on_ground_transition_time,222.9,The time in seconds measured from startup  that the EKF transitioned out of in-air mode. Set to a nan if a transition event is not detected.
+output_obs_ang_err_median,0.000733596,Median in-flight value of the output observer angular error (rad)
+output_obs_pos_err_median,0.0111879,Median in-flight value of the output observer position error (m)
+output_obs_vel_err_median,0.00442852,Median in-flight value of the output observer velocity error (m/s)
+pos_fail_percentage,0.0,The percentage of in-flight recorded failure events for the velocity sensor consolidated innovation consistency test.
+pos_percentage_amber,0.0,The percentage of in-flight position sensor consolidated innovation consistency test values > 0.5.
+pos_percentage_red,0.0,The percentage of in-flight position sensor consolidated innovation consistency test values > 1.0.
+pos_sensor_status,Pass,Position sensor check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+pos_test_max,0.0684734,The maximum in-flight value of the position sensor consolidated innovation consistency test ratio.
+pos_test_mean,0.0208023,The mean in-flight value of the position sensor consolidated innovation consistency test ratio.
+tas_fail_percentage,nan,The percentage of in-flight recorded failure events for the airspeed sensor innovation consistency test.
+tas_percentage_amber,nan,The percentage of in-flight airspeed sensor innovation consistency test values > 0.5.
+tas_percentage_red,nan,The percentage of in-flight airspeed sensor innovation consistency test values > 1.0.
+tas_sensor_status,Pass,Airspeed sensor check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+tas_test_max,nan,The maximum in-flight value of the airspeed sensor innovation consistency test ratio.
+tas_test_mean,nan,The mean in-flight value of the airspeed sensor innovation consistency test ratio.
+tilt_align_time,nan,The time in seconds measured from startup that the EKF completed the tilt alignment. A nan value indicates that the alignment had completed before logging started or alignment did not complete.
+vel_fail_percentage,nan,The percentage of in-flight recorded failure events for the velocity sensor consolidated innovation consistency test.
+vel_percentage_amber,nan,The percentage of in-flight velocity sensor consolidated innovation consistency test values > 0.5.
+vel_percentage_red,nan,The percentage of in-flight velocity sensor consolidated innovation consistency test values > 1.0.
+vel_sensor_status,Pass,Velocity sensor check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required
+vel_test_max,nan,The maximum in-flight value of the velocity sensor consolidated innovation consistency test ratio.
+vel_test_mean,nan,The mean in-flight value of the velocity sensor consolidated innovation consistency test ratio.
+yaw_align_time,nan,The time in seconds measured from startup that the EKF completed the yaw alignment.
+yaw_fail_percentage,0.0,The percentage of in-flight recorded failure events for the yaw sensor innovation consistency test.
+yaw_sensor_status,Pass,Yaw sensor check summary. This sensor data can be sourced from the magnetometer or an external vision system. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required