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@@ -79,3 +79,25 @@ log_54_2022-4-19-18-17-42_px4_pose_reset.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
+2019-05-24/19_21_36.ulg filter=lfs diff=lfs merge=lfs -text
+2018-09-18/07_55_26.ulg filter=lfs diff=lfs merge=lfs -text
+2019-05-24/19_04_17.ulg filter=lfs diff=lfs merge=lfs -text
+2019-05-24/19_30_46.ulg filter=lfs diff=lfs merge=lfs -text
+2019-05-24/19_13_59.ulg filter=lfs diff=lfs merge=lfs -text
+2019-05-24/19_33_59.ulg filter=lfs diff=lfs merge=lfs -text
+2019-05-24/19_27_14.ulg filter=lfs diff=lfs merge=lfs -text
+2019-05-24/19_42_10.ulg filter=lfs diff=lfs merge=lfs -text
+2018-09-18/07_48_03.ulg filter=lfs diff=lfs merge=lfs -text
+2018-09-18/08_39_17.ulg filter=lfs diff=lfs merge=lfs -text
+2018-09-18/08_04_48.ulg filter=lfs diff=lfs merge=lfs -text
+2019-05-24/19_37_19.ulg filter=lfs diff=lfs merge=lfs -text
+2019-01-01/15_39_02.ulg filter=lfs diff=lfs merge=lfs -text
+2019-01-01/15_35_34.ulg filter=lfs diff=lfs merge=lfs -text
+2019-01-01/14_39_39.ulg filter=lfs diff=lfs merge=lfs -text
+2019-01-01/15_37_30.ulg filter=lfs diff=lfs merge=lfs -text
+2019-01-01/14_44_02.ulg filter=lfs diff=lfs merge=lfs -text
+2020-06-18/14_12_22.ulg filter=lfs diff=lfs merge=lfs -text
+2020-06-18/13_55_18.ulg filter=lfs diff=lfs merge=lfs -text
+2020-06-18/12_55_16.ulg filter=lfs diff=lfs merge=lfs -text
+2020-06-18/14_24_22.ulg filter=lfs diff=lfs merge=lfs -text
+2022-11-16/log_7_2022-12-2-04-40-22_vadi_ilk_otonom_ucus.ulg filter=lfs diff=lfs merge=lfs -text

2018-06-12/18_52_10.ulg.mdat.csv

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+name,value,description
+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,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,0.1945427,The maximum in-flight value of the height sensor innovation consistency test ratio.
+hgt_test_mean,0.050006524,The mean in-flight value of the height sensor innovation consistency test ratio.
+imu_coning_mean,2.5825352e-07,Mean in-flight value of the IMU delta angle coning vibration metric (rad)
+imu_coning_peak,1.0747422e-06,Peak in-flight value of the IMU delta angle coning vibration metric (rad)
+imu_dang_bias_median,1.3028385230004137e-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,0.00053458835,Mean in-flight value of the IMU delta angle high frequency vibration metric (rad)
+imu_hfdang_peak,0.0011441719,Peak in-flight value of the IMU delta angle high frequency vibration metric (rad)
+imu_hfdvel_mean,0.015757602,Mean in-flight value of the IMU delta velocity high frequency vibration metric (m/s)
+imu_hfdvel_peak,0.026210956,Peak in-flight value of the IMU delta velocity high frequency vibration metric (m/s)
+imu_sensor_status,Warning - Vibration,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
+in_air_transition_time,293.4,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,0.20913145,The maximum in-flight value of the magnetic field sensor innovation consistency test ratio.
+mag_test_mean,0.02915289,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,339.0,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,0.0010603885,Median in-flight value of the output observer angular error (rad)
+output_obs_pos_err_median,0.028610872,Median in-flight value of the output observer position error (m)
+output_obs_vel_err_median,0.021115616,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,1.86046511628,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,0.8061113,The maximum in-flight value of the position sensor consolidated innovation consistency test ratio.
+pos_test_mean,0.11371472,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

2018-06-12/19_05_12.ulg.mdat.csv

@@ -0,0 +1,62 @@
+name,value,description
+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,0.0911515,The maximum in-flight value of the height above ground sensor innovation consistency test ratio.
+hagl_test_mean,0.015060466,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,0.13412344,The maximum in-flight value of the height sensor innovation consistency test ratio.
+hgt_test_mean,0.068739265,The mean in-flight value of the height sensor innovation consistency test ratio.
+imu_coning_mean,5.619268e-07,Mean in-flight value of the IMU delta angle coning vibration metric (rad)
+imu_coning_peak,3.5316955e-06,Peak in-flight value of the IMU delta angle coning vibration metric (rad)
+imu_dang_bias_median,2.0052137211591593e-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,0.0007848049,Mean in-flight value of the IMU delta angle high frequency vibration metric (rad)
+imu_hfdang_peak,0.0013464751,Peak in-flight value of the IMU delta angle high frequency vibration metric (rad)
+imu_hfdvel_mean,0.018863289,Mean in-flight value of the IMU delta velocity high frequency vibration metric (m/s)
+imu_hfdvel_peak,0.022908071,Peak in-flight value of the IMU delta velocity high frequency vibration metric (m/s)
+imu_sensor_status,Warning - Output Predictor,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
+in_air_transition_time,690.3,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,0.047168974,The maximum in-flight value of the magnetic field sensor innovation consistency test ratio.
+mag_test_mean,0.0167662,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,744.7,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,0.0006247556,Median in-flight value of the output observer angular error (rad)
+output_obs_pos_err_median,0.43559787,Median in-flight value of the output observer position error (m)
+output_obs_vel_err_median,0.04748367,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,0.004023424,The maximum in-flight value of the position sensor consolidated innovation consistency test ratio.
+pos_test_mean,0.0039968127,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

2018-06-12/19_06_44.ulg.mdat.csv

@@ -0,0 +1,62 @@
+name,value,description
+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,0.036807913,The maximum in-flight value of the height above ground sensor innovation consistency test ratio.
+hagl_test_mean,0.0031686819,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,0.15559219,The maximum in-flight value of the height sensor innovation consistency test ratio.
+hgt_test_mean,0.04243126,The mean in-flight value of the height sensor innovation consistency test ratio.
+imu_coning_mean,5.140858e-07,Mean in-flight value of the IMU delta angle coning vibration metric (rad)
+imu_coning_peak,2.5449478e-06,Peak in-flight value of the IMU delta angle coning vibration metric (rad)
+imu_dang_bias_median,2.1034635152730014e-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,0.0008377056,Mean in-flight value of the IMU delta angle high frequency vibration metric (rad)
+imu_hfdang_peak,0.0016689737,Peak in-flight value of the IMU delta angle high frequency vibration metric (rad)
+imu_hfdvel_mean,0.018968074,Mean in-flight value of the IMU delta velocity high frequency vibration metric (m/s)
+imu_hfdvel_peak,0.029086651,Peak in-flight value of the IMU delta velocity high frequency vibration metric (m/s)
+imu_sensor_status,Warning - Output Predictor,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
+in_air_transition_time,784.5,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,0.016333159,The maximum in-flight value of the magnetic field sensor innovation consistency test ratio.
+mag_test_mean,0.01633316,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,868.8,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,0.00149953,Median in-flight value of the output observer angular error (rad)
+output_obs_pos_err_median,0.06876233,Median in-flight value of the output observer position error (m)
+output_obs_vel_err_median,0.17780297,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,0.004023424,The maximum in-flight value of the position sensor consolidated innovation consistency test ratio.
+pos_test_mean,0.0040234243,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

2018-06-12/19_24_37.ulg.mdat.csv

@@ -0,0 +1,62 @@
+name,value,description
+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,0.13456227,The maximum in-flight value of the height above ground sensor innovation consistency test ratio.
+hagl_test_mean,0.013045576,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,0.2603389,The maximum in-flight value of the height sensor innovation consistency test ratio.
+hgt_test_mean,0.07971216,The mean in-flight value of the height sensor innovation consistency test ratio.
+imu_coning_mean,5.9344615e-07,Mean in-flight value of the IMU delta angle coning vibration metric (rad)
+imu_coning_peak,3.771008e-06,Peak in-flight value of the IMU delta angle coning vibration metric (rad)
+imu_dang_bias_median,2.0502276347482374e-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,0.00077781174,Mean in-flight value of the IMU delta angle high frequency vibration metric (rad)
+imu_hfdang_peak,0.0013303632,Peak in-flight value of the IMU delta angle high frequency vibration metric (rad)
+imu_hfdvel_mean,0.02010622,Mean in-flight value of the IMU delta velocity high frequency vibration metric (m/s)
+imu_hfdvel_peak,0.03722522,Peak in-flight value of the IMU delta velocity high frequency vibration metric (m/s)
+imu_sensor_status,Warning - Vibration,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
+in_air_transition_time,241.2,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,1.81347150259,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,0.67449754,The maximum in-flight value of the magnetic field sensor innovation consistency test ratio.
+mag_test_mean,0.108884595,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,323.4,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,0.0018676167,Median in-flight value of the output observer angular error (rad)
+output_obs_pos_err_median,0.023959495,Median in-flight value of the output observer position error (m)
+output_obs_vel_err_median,0.024141507,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,4.63414634146,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,0.963041,The maximum in-flight value of the position sensor consolidated innovation consistency test ratio.
+pos_test_mean,0.13436735,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

2018-06-12/19_31_16.ulg.mdat.csv

@@ -0,0 +1,62 @@
+name,value,description
+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,0.07351747,The maximum in-flight value of the height above ground sensor innovation consistency test ratio.
+hagl_test_mean,0.00790325,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,0.15007985,The maximum in-flight value of the height sensor innovation consistency test ratio.
+hgt_test_mean,0.06797089,The mean in-flight value of the height sensor innovation consistency test ratio.
+imu_coning_mean,4.5584042e-07,Mean in-flight value of the IMU delta angle coning vibration metric (rad)
+imu_coning_peak,2.1131946e-06,Peak in-flight value of the IMU delta angle coning vibration metric (rad)
+imu_dang_bias_median,2.1860446353022046e-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,0.0007815675,Mean in-flight value of the IMU delta angle high frequency vibration metric (rad)
+imu_hfdang_peak,0.0018193177,Peak in-flight value of the IMU delta angle high frequency vibration metric (rad)
+imu_hfdvel_mean,0.018852782,Mean in-flight value of the IMU delta velocity high frequency vibration metric (m/s)
+imu_hfdvel_peak,0.026677633,Peak in-flight value of the IMU delta velocity high frequency vibration metric (m/s)
+imu_sensor_status,Warning - Output Predictor,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
+in_air_transition_time,650.8,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,0.05040179,The maximum in-flight value of the magnetic field sensor innovation consistency test ratio.
+mag_test_mean,0.050401792,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,712.2,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,0.0009901822,Median in-flight value of the output observer angular error (rad)
+output_obs_pos_err_median,0.6698303,Median in-flight value of the output observer position error (m)
+output_obs_vel_err_median,0.090833604,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,0.12049451,The maximum in-flight value of the position sensor consolidated innovation consistency test ratio.
+pos_test_mean,0.12049449,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

2018-06-12/19_37_11.ulg.mdat.csv

@@ -0,0 +1,62 @@
+name,value,description
+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_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_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
+in_air_transition_time,994.4,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,1003.5,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,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

2018-06-12/19_37_35.ulg.mdat.csv

@@ -0,0 +1,62 @@
+name,value,description
+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_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_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
+in_air_transition_time,1017.8,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,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,1039.3,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,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

2018-06-12/19_38_14.ulg.mdat.csv

@@ -0,0 +1,62 @@
+name,value,description
+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,0.08651192,The maximum in-flight value of the height above ground sensor innovation consistency test ratio.
+hagl_test_mean,0.007523724,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,0.24714811,The maximum in-flight value of the height sensor innovation consistency test ratio.
+hgt_test_mean,0.06668086,The mean in-flight value of the height sensor innovation consistency test ratio.
+imu_coning_mean,3.656168e-07,Mean in-flight value of the IMU delta angle coning vibration metric (rad)
+imu_coning_peak,4.6297605e-06,Peak in-flight value of the IMU delta angle coning vibration metric (rad)
+imu_dang_bias_median,2.111362884326685e-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,0.00070906885,Mean in-flight value of the IMU delta angle high frequency vibration metric (rad)
+imu_hfdang_peak,0.0013645914,Peak in-flight value of the IMU delta angle high frequency vibration metric (rad)
+imu_hfdvel_mean,0.018670298,Mean in-flight value of the IMU delta velocity high frequency vibration metric (m/s)
+imu_hfdvel_peak,0.029415106,Peak in-flight value of the IMU delta velocity high frequency vibration metric (m/s)
+imu_sensor_status,Warning - Vibration,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
+in_air_transition_time,1057.3,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,1.32653061224,The percentage of in-flight consolidated magnetic field sensor innovation consistency test values > 0.5.
+mag_percentage_red,0.204081632653,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,1.9541053,The maximum in-flight value of the magnetic field sensor innovation consistency test ratio.
+mag_test_mean,0.09225005,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,1260.7,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,0.0011385791,Median in-flight value of the output observer angular error (rad)
+output_obs_pos_err_median,0.014021856,Median in-flight value of the output observer position error (m)
+output_obs_vel_err_median,0.014411514,Median in-flight value of the output observer velocity error (m/s)
+pos_fail_percentage,1.49402390438,The percentage of in-flight recorded failure events for the velocity sensor consolidated innovation consistency test.
+pos_percentage_amber,2.09163346614,The percentage of in-flight position sensor consolidated innovation consistency test values > 0.5.
+pos_percentage_red,1.49402390438,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,2.49247,The maximum in-flight value of the position sensor consolidated innovation consistency test ratio.
+pos_test_mean,0.11225577,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,0.204081632653,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

2018-06-12/19_44_57.ulg.mdat.csv

@@ -0,0 +1,62 @@
+name,value,description
+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,0.11591485,The maximum in-flight value of the height above ground sensor innovation consistency test ratio.
+hagl_test_mean,0.008191313,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,0.25690904,The maximum in-flight value of the height sensor innovation consistency test ratio.
+hgt_test_mean,0.06777267,The mean in-flight value of the height sensor innovation consistency test ratio.
+imu_coning_mean,3.749129e-07,Mean in-flight value of the IMU delta angle coning vibration metric (rad)
+imu_coning_peak,4.0112445e-06,Peak in-flight value of the IMU delta angle coning vibration metric (rad)
+imu_dang_bias_median,3.2796184099982115e-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,0.0007601188,Mean in-flight value of the IMU delta angle high frequency vibration metric (rad)
+imu_hfdang_peak,0.0015840365,Peak in-flight value of the IMU delta angle high frequency vibration metric (rad)
+imu_hfdvel_mean,0.018984258,Mean in-flight value of the IMU delta velocity high frequency vibration metric (m/s)
+imu_hfdvel_peak,0.045773696,Peak in-flight value of the IMU delta velocity high frequency vibration metric (m/s)
+imu_sensor_status,Warning - Vibration,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
+in_air_transition_time,1459.8,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,2.76381909548,The percentage of in-flight consolidated magnetic field sensor innovation consistency test values > 0.5.
+mag_percentage_red,5.02512562814,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,1.3834869,The maximum in-flight value of the magnetic field sensor innovation consistency test ratio.
+mag_test_mean,0.19367705,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,1627.1,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,0.0022214078,Median in-flight value of the output observer angular error (rad)
+output_obs_pos_err_median,0.028176539,Median in-flight value of the output observer position error (m)
+output_obs_vel_err_median,0.027995957,Median in-flight value of the output observer velocity error (m/s)
+pos_fail_percentage,3.90243902439,The percentage of in-flight recorded failure events for the velocity sensor consolidated innovation consistency test.
+pos_percentage_amber,1.9512195122,The percentage of in-flight position sensor consolidated innovation consistency test values > 0.5.
+pos_percentage_red,3.90243902439,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,4.248762,The maximum in-flight value of the position sensor consolidated innovation consistency test ratio.
+pos_test_mean,0.21849392,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,5.02512562814,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

2018-06-12/19_55_27.ulg.mdat.csv

@@ -0,0 +1,62 @@
+name,value,description
+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,0.13521574,The maximum in-flight value of the height above ground sensor innovation consistency test ratio.
+hagl_test_mean,0.012103076,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,0.22602093,The maximum in-flight value of the height sensor innovation consistency test ratio.
+hgt_test_mean,0.07710362,The mean in-flight value of the height sensor innovation consistency test ratio.
+imu_coning_mean,7.738333e-07,Mean in-flight value of the IMU delta angle coning vibration metric (rad)
+imu_coning_peak,3.3483184e-06,Peak in-flight value of the IMU delta angle coning vibration metric (rad)
+imu_dang_bias_median,2.444631140498866e-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,0.0009316112,Mean in-flight value of the IMU delta angle high frequency vibration metric (rad)
+imu_hfdang_peak,0.0019482474,Peak in-flight value of the IMU delta angle high frequency vibration metric (rad)
+imu_hfdvel_mean,0.019773176,Mean in-flight value of the IMU delta velocity high frequency vibration metric (m/s)
+imu_hfdvel_peak,0.042331178,Peak in-flight value of the IMU delta velocity high frequency vibration metric (m/s)
+imu_sensor_status,Warning - Vibration,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
+in_air_transition_time,128.7,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,1.59574468085,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,0.78217214,The maximum in-flight value of the magnetic field sensor innovation consistency test ratio.
+mag_test_mean,0.09754534,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,209.0,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,0.0027475867,Median in-flight value of the output observer angular error (rad)
+output_obs_pos_err_median,0.041472074,Median in-flight value of the output observer position error (m)
+output_obs_vel_err_median,0.04021576,Median in-flight value of the output observer velocity error (m/s)
+pos_fail_percentage,5.5,The percentage of in-flight recorded failure events for the velocity sensor consolidated innovation consistency test.
+pos_percentage_amber,6.75,The percentage of in-flight position sensor consolidated innovation consistency test values > 0.5.
+pos_percentage_red,5.5,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,2.298366,The maximum in-flight value of the position sensor consolidated innovation consistency test ratio.
+pos_test_mean,0.2722404,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

2018-06-12/population_data.csv

@@ -0,0 +1,40 @@
+name,value,description
+hagl_fail_pct,0.0,Percentage of logs with height above ground sensor fails
+hagl_test_max_avg,0.09624023757142856,The mean of the maximum in-flight values of the height above ground sensor innovation consistency test ratio
+hagl_test_mean_avg,0.009570869557142857,The mean of the mean in-flight value of the height above ground sensor innovation consistency test ratio
+hagl_warning_pct,0.0,Percentage of logs with height above ground sensor warnings
+hgt_fail_pct,0.0,Percentage of logs with height sensor fails
+hgt_test_max_avg,0.20309439499999998,The mean of the maximum  in-flight values of the height sensor innovation consistency test ratio
+hgt_test_mean_avg,0.065052156125,The mean of the mean in-flight value of the height sensor innovation consistency test ratio
+hgt_warning_pct,0.0,Percentage of logs with height sensor warnings
+imu_coning_max_avg,0.0031281139375000004,The mean of the maximum in-flight values of the IMU delta angle coning vibration level (mrad)
+imu_coning_mean_avg,0.00048723946125,The mean of the mean in-flight value of the IMU delta angle coning vibration level (mrad)
+imu_hfdang_max_avg,1.5257721124999999,The mean of the maximum in-flight values of the IMU high frequency delta angle vibration level (mrad)
+imu_hfdang_mean_avg,0.7646596175,The mean of the mean in-flight value of the IMU delta high frequency delta angle vibration level (mrad)
+imu_hfdvel_max_avg,0.032453563875,The mean of the maximum in-flight values of the IMU high frequency delta velocity vibration level (m/s)
+imu_hfdvel_mean_avg,0.018746962375,The mean of the mean in-flight value of the IMU delta high frequency delta velocity vibration level (m/s)
+mag_fail_pct,0.0,Percentage of logs with magnetometer sensor fails
+mag_test_max_avg,0.639662156625,The mean of the maximum  in-flight values of the magnetic field sensor innovation consistency test ratio
+mag_test_mean_avg,0.07562638462499999,The mean of the mean in-flight value of the magnetic field sensor innovation consistency test ratio
+mag_warning_pct,0.0,Percentage of logs with magnetometer sensor warnings
+master_fail_pct,30.0,Percentage of logs with fails
+master_warning_pct,50.0,Percentage of logs with warnings
+obs_ang_median_avg,1.518755825,The mean of the median in-flight value of the output observer angular tracking error magnitude (mrad)
+obs_pos_median_avg,0.163803917,The mean of the median in-flight value of the output observer position tracking error magnitude (m)
+obs_vel_median_avg,0.05550007475,The mean of the median in-flight value of the output observer velocity tracking error magnitude (m/s)
+ofx_fail_pct_avg,nan,The mean percentage of innovation test fails for the X axis optical flow sensor
+ofy_fail_pct_avg,nan,The mean percentage of innovation test fails for the Y axis optical flow sensor
+pos_fail_pct,30.0,Percentage of logs with position sensor fails
+pos_test_max_avg,1.36716145725,The mean of the maximum  in-flight values of the position sensor innovation consistency test ratio
+pos_test_mean_avg,0.12244836087500001,The mean of the mean in-flight value of the position sensor innovation consistency test ratio
+pos_warning_pct,0.0,Percentage of logs with position sensor warnings
+tas_fail_pct,0.0,Percentage of logs with airspeed ground sensor fails
+tas_test_max_avg,nan,The mean of the maximum  in-flight values of the airspeed sensor innovation consistency test ratio
+tas_test_mean_avg,nan,The mean of the mean in-flight value of the airspeed sensor innovation consistency test ratio
+tas_warning_pct,0.0,Percentage of logs with airspeed sensor warnings
+vel_fail_pct,0.0,Percentage of logs with velocity sensor fails
+vel_test_max_avg,nan,The mean of the maximum  in-flight values of the velocity sensor innovation consistency test ratio
+vel_test_mean_avg,nan,The mean of the mean in-flight value of the velocity sensor innovation consistency test ratio
+vel_warning_pct,0.0,Percentage of logs with velocity sensor warnings
+yaw_fail_pct,20.0,Percentage of logs with yaw sensor fails
+yaw_warning_pct,0.0,Percentage of logs with yaw sensor warnings

2018-06-14/log002.ulg.mdat.csv

@@ -0,0 +1,62 @@
+name,value,description
+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_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_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
+in_air_transition_time,322.8,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,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,329.2,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

2018-06-14/log003.ulg.mdat.csv

@@ -0,0 +1,62 @@
+name,value,description
+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_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_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
+in_air_transition_time,340.0,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,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,360.9,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

2018-06-14/log004.ulg.mdat.csv

@@ -0,0 +1,62 @@
+name,value,description
+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_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_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
+in_air_transition_time,373.0,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,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,385.9,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

2018-06-14/not

@@ -0,0 +1,4 @@
+Kalkış sonrası yalpaladı daha sonra çakıldı
+Kumandada manual kill switch yapıldı ancak sonra bir daha havalandı ve sola doğru kayarak duvara çarpıp düştü
+
+loglarda RC lost gözüküyor

2018-06-14/population_data.pdf

@@ -0,0 +1,10 @@
+%PDF-1.4
+%�� ��
+1 0 obj
+<< /Pages 2 0 R /Type /Catalog >>
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+8 0 obj
+<< /ExtGState 4 0 R /Font 3 0 R /Pattern 5 0 R
+/ProcSet [ /PDF /Text /ImageB /ImageC /ImageI ] /Shading 6 0 R
+/XObject 7 0 R >>
+endobj

2018-09-07/12_51_41.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,0.348249,The maximum in-flight value of the height above ground sensor innovation consistency test ratio.
+hagl_test_mean,0.023428,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,0.123372,The maximum in-flight value of the height sensor innovation consistency test ratio.
+hgt_test_mean,0.0340872,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,1.46791e-06,Mean in-flight value of the IMU delta angle coning vibration metric (rad)
+imu_coning_peak,4.73786e-06,Peak in-flight value of the IMU delta angle coning vibration metric (rad)
+imu_dang_bias_median,1.83750787655e-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,0.00227168,Mean in-flight value of the IMU delta angle high frequency vibration metric (rad)
+imu_hfdang_peak,0.00376846,Peak in-flight value of the IMU delta angle high frequency vibration metric (rad)
+imu_hfdvel_mean,0.0322441,Mean in-flight value of the IMU delta velocity high frequency vibration metric (m/s)
+imu_hfdvel_peak,0.0390769,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,91.5,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,19.2926045016,The percentage of in-flight consolidated magnetic field sensor innovation consistency test values > 0.5.
+mag_percentage_red,41.1575562701,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,2.31542,The maximum in-flight value of the magnetic field sensor innovation consistency test ratio.
+mag_test_mean,0.785281,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,164.4,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,0.00275299,Median in-flight value of the output observer angular error (rad)
+output_obs_pos_err_median,0.0586083,Median in-flight value of the output observer position error (m)
+output_obs_vel_err_median,0.0491922,Median in-flight value of the output observer velocity error (m/s)
+pos_fail_percentage,12.5,The percentage of in-flight recorded failure events for the velocity sensor consolidated innovation consistency test.
+pos_percentage_amber,13.8888888889,The percentage of in-flight position sensor consolidated innovation consistency test values > 0.5.
+pos_percentage_red,12.5,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,3.78502,The maximum in-flight value of the position sensor consolidated innovation consistency test ratio.
+pos_test_mean,0.519041,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,33.1189710611,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_20_12.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,0.39825,The maximum in-flight value of the height above ground sensor innovation consistency test ratio.
+hagl_test_mean,0.035394,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,0.0840181,The maximum in-flight value of the height sensor innovation consistency test ratio.
+hgt_test_mean,0.0281554,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,1.86923e-06,Mean in-flight value of the IMU delta angle coning vibration metric (rad)
+imu_coning_peak,5.45644e-06,Peak in-flight value of the IMU delta angle coning vibration metric (rad)
+imu_dang_bias_median,1.46584719337e-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,0.0025364,Mean in-flight value of the IMU delta angle high frequency vibration metric (rad)
+imu_hfdang_peak,0.00474723,Peak in-flight value of the IMU delta angle high frequency vibration metric (rad)
+imu_hfdvel_mean,0.0361114,Mean in-flight value of the IMU delta velocity high frequency vibration metric (m/s)
+imu_hfdvel_peak,0.0421033,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,35.3,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,21.7741935484,The percentage of in-flight consolidated magnetic field sensor innovation consistency test values > 0.5.
+mag_percentage_red,37.9032258065,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,1.52116,The maximum in-flight value of the magnetic field sensor innovation consistency test ratio.
+mag_test_mean,0.572346,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,70.3,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,0.00190902,Median in-flight value of the output observer angular error (rad)
+output_obs_pos_err_median,0.056296,Median in-flight value of the output observer position error (m)
+output_obs_vel_err_median,0.038918,Median in-flight value of the output observer velocity error (m/s)
+pos_fail_percentage,54.3352601156,The percentage of in-flight recorded failure events for the velocity sensor consolidated innovation consistency test.
+pos_percentage_amber,8.67052023121,The percentage of in-flight position sensor consolidated innovation consistency test values > 0.5.
+pos_percentage_red,54.3352601156,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,72.9176,The maximum in-flight value of the position sensor consolidated innovation consistency test ratio.
+pos_test_mean,1.88571,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,37.0967741935,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_26_48.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,56.2,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,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,74.8,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,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

2018-09-07/13_39_11.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,0.239808153477,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,0.666765,The maximum in-flight value of the height above ground sensor innovation consistency test ratio.
+hagl_test_mean,0.0219853,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,0.105049,The maximum in-flight value of the height sensor innovation consistency test ratio.
+hgt_test_mean,0.0289261,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,1.68769e-06,Mean in-flight value of the IMU delta angle coning vibration metric (rad)
+imu_coning_peak,6.52873e-06,Peak in-flight value of the IMU delta angle coning vibration metric (rad)
+imu_dang_bias_median,1.98780599455e-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,0.00235215,Mean in-flight value of the IMU delta angle high frequency vibration metric (rad)
+imu_hfdang_peak,0.00467675,Peak in-flight value of the IMU delta angle high frequency vibration metric (rad)
+imu_hfdvel_mean,0.0304854,Mean in-flight value of the IMU delta velocity high frequency vibration metric (m/s)
+imu_hfdvel_peak,0.0356808,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,57.5,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,21.1956521739,The percentage of in-flight consolidated magnetic field sensor innovation consistency test values > 0.5.
+mag_percentage_red,30.7065217391,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,2.91744,The maximum in-flight value of the magnetic field sensor innovation consistency test ratio.
+mag_test_mean,0.721199,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,142.0,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,0.00306134,Median in-flight value of the output observer angular error (rad)
+output_obs_pos_err_median,0.0643471,Median in-flight value of the output observer position error (m)
+output_obs_vel_err_median,0.0426881,Median in-flight value of the output observer velocity error (m/s)
+pos_fail_percentage,27.0983213429,The percentage of in-flight recorded failure events for the velocity sensor consolidated innovation consistency test.
+pos_percentage_amber,10.071942446,The percentage of in-flight position sensor consolidated innovation consistency test values > 0.5.
+pos_percentage_red,27.0983213429,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,11.3459,The maximum in-flight value of the position sensor consolidated innovation consistency test ratio.
+pos_test_mean,0.78884,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,30.7065217391,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_52_43.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,0.284715,The maximum in-flight value of the height above ground sensor innovation consistency test ratio.
+hagl_test_mean,0.0242014,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,0.10671,The maximum in-flight value of the height sensor innovation consistency test ratio.
+hgt_test_mean,0.0242867,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,1.42552e-06,Mean in-flight value of the IMU delta angle coning vibration metric (rad)
+imu_coning_peak,3.25596e-06,Peak in-flight value of the IMU delta angle coning vibration metric (rad)
+imu_dang_bias_median,2.66537879729e-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,0.0023033,Mean in-flight value of the IMU delta angle high frequency vibration metric (rad)
+imu_hfdang_peak,0.00394106,Peak in-flight value of the IMU delta angle high frequency vibration metric (rad)
+imu_hfdvel_mean,0.030744,Mean in-flight value of the IMU delta velocity high frequency vibration metric (m/s)
+imu_hfdvel_peak,0.0347842,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,38.1,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,20.197044335,The percentage of in-flight consolidated magnetic field sensor innovation consistency test values > 0.5.
+mag_percentage_red,32.5123152709,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,1.75584,The maximum in-flight value of the magnetic field sensor innovation consistency test ratio.
+mag_test_mean,0.608891,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,89.1,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,0.00316832,Median in-flight value of the output observer angular error (rad)
+output_obs_pos_err_median,0.0532125,Median in-flight value of the output observer position error (m)
+output_obs_vel_err_median,0.035231,Median in-flight value of the output observer velocity error (m/s)
+pos_fail_percentage,22.2222222222,The percentage of in-flight recorded failure events for the velocity sensor consolidated innovation consistency test.
+pos_percentage_amber,9.92063492063,The percentage of in-flight position sensor consolidated innovation consistency test values > 0.5.
+pos_percentage_red,22.2222222222,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,3.09913,The maximum in-flight value of the position sensor consolidated innovation consistency test ratio.
+pos_test_mean,0.626826,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,20.197044335,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

2018-09-07/14_16_20.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,0.225902,The maximum in-flight value of the height above ground sensor innovation consistency test ratio.
+hagl_test_mean,0.016879,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,0.105123,The maximum in-flight value of the height sensor innovation consistency test ratio.
+hgt_test_mean,0.0253857,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,1.52098e-06,Mean in-flight value of the IMU delta angle coning vibration metric (rad)
+imu_coning_peak,3.45889e-06,Peak in-flight value of the IMU delta angle coning vibration metric (rad)
+imu_dang_bias_median,1.51189886175e-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,0.00228659,Mean in-flight value of the IMU delta angle high frequency vibration metric (rad)
+imu_hfdang_peak,0.00371228,Peak in-flight value of the IMU delta angle high frequency vibration metric (rad)
+imu_hfdvel_mean,0.0298286,Mean in-flight value of the IMU delta velocity high frequency vibration metric (m/s)
+imu_hfdvel_peak,0.0347152,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,95.4,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,16.1290322581,The percentage of in-flight consolidated magnetic field sensor innovation consistency test values > 0.5.
+mag_percentage_red,38.7096774194,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,2.46007,The maximum in-flight value of the magnetic field sensor innovation consistency test ratio.
+mag_test_mean,0.712215,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,161.9,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,0.00175935,Median in-flight value of the output observer angular error (rad)
+output_obs_pos_err_median,0.143698,Median in-flight value of the output observer position error (m)
+output_obs_vel_err_median,0.0642361,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,5.18292682927,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,Warning,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,0.807261,The maximum in-flight value of the position sensor consolidated innovation consistency test ratio.
+pos_test_mean,0.213002,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,30.4659498208,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

2018-09-07/14_19_21.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,0.219164,The maximum in-flight value of the height above ground sensor innovation consistency test ratio.
+hagl_test_mean,0.0159044,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,0.119399,The maximum in-flight value of the height sensor innovation consistency test ratio.
+hgt_test_mean,0.0244689,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,1.57537e-06,Mean in-flight value of the IMU delta angle coning vibration metric (rad)
+imu_coning_peak,5.51988e-06,Peak in-flight value of the IMU delta angle coning vibration metric (rad)
+imu_dang_bias_median,2.0542036178e-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,0.00226739,Mean in-flight value of the IMU delta angle high frequency vibration metric (rad)
+imu_hfdang_peak,0.00409669,Peak in-flight value of the IMU delta angle high frequency vibration metric (rad)
+imu_hfdvel_mean,0.0312963,Mean in-flight value of the IMU delta velocity high frequency vibration metric (m/s)
+imu_hfdvel_peak,0.0360221,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,41.6,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,5.0,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,0.610233,The maximum in-flight value of the magnetic field sensor innovation consistency test ratio.
+mag_test_mean,0.186937,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,152.7,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,0.00162649,Median in-flight value of the output observer angular error (rad)
+output_obs_pos_err_median,0.0999748,Median in-flight value of the output observer position error (m)
+output_obs_vel_err_median,0.0458046,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,1.82149362477,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,0.586868,The maximum in-flight value of the position sensor consolidated innovation consistency test ratio.
+pos_test_mean,0.154257,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