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estimator_status_flags.msg
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estimator_status_flags.msg
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uint64 timestamp # time since system start (microseconds)
uint64 timestamp_sample # the timestamp of the raw data (microseconds)
# filter control status
uint32 control_status_changes # number of filter control status (cs) changes
bool cs_tilt_align # 0 - true if the filter tilt alignment is complete
bool cs_yaw_align # 1 - true if the filter yaw alignment is complete
bool cs_gps # 2 - true if GPS measurement fusion is intended
bool cs_opt_flow # 3 - true if optical flow measurements fusion is intended
bool cs_mag_hdg # 4 - true if a simple magnetic yaw heading fusion is intended
bool cs_mag_3d # 5 - true if 3-axis magnetometer measurement fusion is inteded
bool cs_mag_dec # 6 - true if synthetic magnetic declination measurements fusion is intended
bool cs_in_air # 7 - true when the vehicle is airborne
bool cs_wind # 8 - true when wind velocity is being estimated
bool cs_baro_hgt # 9 - true when baro height is being fused as a primary height reference
bool cs_rng_hgt # 10 - true when range finder height is being fused as a primary height reference
bool cs_gps_hgt # 11 - true when GPS height is being fused as a primary height reference
bool cs_ev_pos # 12 - true when local position data fusion from external vision is intended
bool cs_ev_yaw # 13 - true when yaw data from external vision measurements fusion is intended
bool cs_ev_hgt # 14 - true when height data from external vision measurements is being fused
bool cs_fuse_beta # 15 - true when synthetic sideslip measurements are being fused
bool cs_mag_field_disturbed # 16 - true when the mag field does not match the expected strength
bool cs_fixed_wing # 17 - true when the vehicle is operating as a fixed wing vehicle
bool cs_mag_fault # 18 - true when the magnetometer has been declared faulty and is no longer being used
bool cs_fuse_aspd # 19 - true when airspeed measurements are being fused
bool cs_gnd_effect # 20 - true when protection from ground effect induced static pressure rise is active
bool cs_rng_stuck # 21 - true when rng data wasn't ready for more than 10s and new rng values haven't changed enough
bool cs_gps_yaw # 22 - true when yaw (not ground course) data fusion from a GPS receiver is intended
bool cs_mag_aligned_in_flight # 23 - true when the in-flight mag field alignment has been completed
bool cs_ev_vel # 24 - true when local frame velocity data fusion from external vision measurements is intended
bool cs_synthetic_mag_z # 25 - true when we are using a synthesized measurement for the magnetometer Z component
bool cs_vehicle_at_rest # 26 - true when the vehicle is at rest
# fault status
uint32 fault_status_changes # number of filter fault status (fs) changes
bool fs_bad_mag_x # 0 - true if the fusion of the magnetometer X-axis has encountered a numerical error
bool fs_bad_mag_y # 1 - true if the fusion of the magnetometer Y-axis has encountered a numerical error
bool fs_bad_mag_z # 2 - true if the fusion of the magnetometer Z-axis has encountered a numerical error
bool fs_bad_hdg # 3 - true if the fusion of the heading angle has encountered a numerical error
bool fs_bad_mag_decl # 4 - true if the fusion of the magnetic declination has encountered a numerical error
bool fs_bad_airspeed # 5 - true if fusion of the airspeed has encountered a numerical error
bool fs_bad_sideslip # 6 - true if fusion of the synthetic sideslip constraint has encountered a numerical error
bool fs_bad_optflow_x # 7 - true if fusion of the optical flow X axis has encountered a numerical error
bool fs_bad_optflow_y # 8 - true if fusion of the optical flow Y axis has encountered a numerical error
bool fs_bad_vel_n # 9 - true if fusion of the North velocity has encountered a numerical error
bool fs_bad_vel_e # 10 - true if fusion of the East velocity has encountered a numerical error
bool fs_bad_vel_d # 11 - true if fusion of the Down velocity has encountered a numerical error
bool fs_bad_pos_n # 12 - true if fusion of the North position has encountered a numerical error
bool fs_bad_pos_e # 13 - true if fusion of the East position has encountered a numerical error
bool fs_bad_pos_d # 14 - true if fusion of the Down position has encountered a numerical error
bool fs_bad_acc_bias # 15 - true if bad delta velocity bias estimates have been detected
bool fs_bad_acc_vertical # 16 - true if bad vertical accelerometer data has been detected
bool fs_bad_acc_clipping # 17 - true if delta velocity data contains clipping (asymmetric railing)
# innovation test failures
uint32 innovation_fault_status_changes # number of innovation fault status (reject) changes
bool reject_hor_vel # 0 - true if horizontal velocity observations have been rejected
bool reject_ver_vel # 1 - true if vertical velocity observations have been rejected
bool reject_hor_pos # 2 - true if horizontal position observations have been rejected
bool reject_ver_pos # 3 - true if vertical position observations have been rejected
bool reject_mag_x # 4 - true if the X magnetometer observation has been rejected
bool reject_mag_y # 5 - true if the Y magnetometer observation has been rejected
bool reject_mag_z # 6 - true if the Z magnetometer observation has been rejected
bool reject_yaw # 7 - true if the yaw observation has been rejected
bool reject_airspeed # 8 - true if the airspeed observation has been rejected
bool reject_sideslip # 9 - true if the synthetic sideslip observation has been rejected
bool reject_hagl # 10 - true if the height above ground observation has been rejected
bool reject_optflow_x # 11 - true if the X optical flow observation has been rejected
bool reject_optflow_y # 12 - true if the Y optical flow observation has been rejected