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168 lines
6.1 KiB
168 lines
6.1 KiB
#include "Sub.h" |
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/** |
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* |
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* ekf_check.pde - detects failures of the ekf or inertial nav system |
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* triggers an alert to the pilot and helps take countermeasures |
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* |
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*/ |
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#ifndef EKF_CHECK_ITERATIONS_MAX |
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# define EKF_CHECK_ITERATIONS_MAX 10 // 1 second (ie. 10 iterations at 10hz) of bad variances signals a failure |
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#endif |
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#ifndef EKF_CHECK_WARNING_TIME |
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# define EKF_CHECK_WARNING_TIME (30*1000) // warning text messages are sent to ground no more than every 30 seconds |
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#endif |
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//////////////////////////////////////////////////////////////////////////////// |
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// EKF_check strucutre |
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//////////////////////////////////////////////////////////////////////////////// |
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static struct { |
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uint8_t fail_count; // number of iterations ekf or dcm have been out of tolerances |
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uint8_t bad_variance : 1; // true if ekf should be considered untrusted (fail_count has exceeded EKF_CHECK_ITERATIONS_MAX) |
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uint32_t last_warn_time; // system time of last warning in milliseconds. Used to throttle text warnings sent to GCS |
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} ekf_check_state; |
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// ekf_check - detects if ekf variance are out of tolerance and triggers failsafe |
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// should be called at 10hz |
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void Sub::ekf_check() |
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{ |
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// exit immediately if ekf has no origin yet - this assumes the origin can never become unset |
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Location temp_loc; |
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if (!ahrs.get_origin(temp_loc)) { |
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return; |
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} |
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// return immediately if motors are not armed, ekf check is disabled, not using ekf or usb is connected |
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if (!motors.armed() || ap.usb_connected || (g.fs_ekf_thresh <= 0.0f)) { |
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ekf_check_state.fail_count = 0; |
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ekf_check_state.bad_variance = false; |
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AP_Notify::flags.ekf_bad = ekf_check_state.bad_variance; |
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failsafe_ekf_off_event(); // clear failsafe |
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return; |
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} |
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// compare compass and velocity variance vs threshold |
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if (ekf_over_threshold()) { |
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// if compass is not yet flagged as bad |
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if (!ekf_check_state.bad_variance) { |
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// increase counter |
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ekf_check_state.fail_count++; |
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// if counter above max then trigger failsafe |
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if (ekf_check_state.fail_count >= EKF_CHECK_ITERATIONS_MAX) { |
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// limit count from climbing too high |
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ekf_check_state.fail_count = EKF_CHECK_ITERATIONS_MAX; |
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ekf_check_state.bad_variance = true; |
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// log an error in the dataflash |
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Log_Write_Error(ERROR_SUBSYSTEM_EKFCHECK, ERROR_CODE_EKFCHECK_BAD_VARIANCE); |
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// send message to gcs |
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if ((AP_HAL::millis() - ekf_check_state.last_warn_time) > EKF_CHECK_WARNING_TIME) { |
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gcs_send_text(MAV_SEVERITY_CRITICAL,"EKF variance"); |
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ekf_check_state.last_warn_time = AP_HAL::millis(); |
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} |
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failsafe_ekf_event(); |
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} |
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} |
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} else { |
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// reduce counter |
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if (ekf_check_state.fail_count > 0) { |
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ekf_check_state.fail_count--; |
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// if compass is flagged as bad and the counter reaches zero then clear flag |
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if (ekf_check_state.bad_variance && ekf_check_state.fail_count == 0) { |
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ekf_check_state.bad_variance = false; |
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// log recovery in the dataflash |
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Log_Write_Error(ERROR_SUBSYSTEM_EKFCHECK, ERROR_CODE_EKFCHECK_VARIANCE_CLEARED); |
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// clear failsafe |
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failsafe_ekf_off_event(); |
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} |
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} |
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} |
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// set AP_Notify flags |
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AP_Notify::flags.ekf_bad = ekf_check_state.bad_variance; |
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// To-Do: add ekf variances to extended status |
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} |
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// ekf_over_threshold - returns true if the ekf's variance are over the tolerance |
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bool Sub::ekf_over_threshold() |
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{ |
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// return false immediately if disabled |
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if (g.fs_ekf_thresh <= 0.0f) { |
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return false; |
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} |
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// return true immediately if position is bad |
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if (!ekf_position_ok() && !optflow_position_ok()) { |
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return true; |
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} |
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// use EKF to get variance |
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float posVar, hgtVar, tasVar; |
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Vector3f magVar; |
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Vector2f offset; |
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float compass_variance; |
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float vel_variance; |
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ahrs.get_variances(vel_variance, posVar, hgtVar, magVar, tasVar, offset); |
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compass_variance = magVar.length(); |
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// return true if compass and velocity variance over the threshold |
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return (compass_variance >= g.fs_ekf_thresh && vel_variance >= g.fs_ekf_thresh); |
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} |
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// failsafe_ekf_event - perform ekf failsafe |
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void Sub::failsafe_ekf_event() |
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{ |
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// // return immediately if ekf failsafe already triggered |
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// if (failsafe.ekf) { |
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// return; |
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// } |
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// |
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// // do nothing if motors disarmed |
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// if (!motors.armed()) { |
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// return; |
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// } |
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// |
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// // do nothing if not in GPS flight mode and ekf-action is not land-even-stabilize |
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// if (!mode_requires_GPS(control_mode) && (g.fs_ekf_action != FS_EKF_ACTION_LAND_EVEN_STABILIZE)) { |
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// return; |
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// } |
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// |
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// // EKF failsafe event has occurred |
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// failsafe.ekf = true; |
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// Log_Write_Error(ERROR_SUBSYSTEM_FAILSAFE_EKFINAV, ERROR_CODE_FAILSAFE_OCCURRED); |
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// |
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// // take action based on fs_ekf_action parameter |
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// switch (g.fs_ekf_action) { |
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// case FS_EKF_ACTION_ALTHOLD: |
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// // AltHold |
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// if (failsafe.manual_control || !set_mode(ALT_HOLD, MODE_REASON_EKF_FAILSAFE)) { |
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// set_mode_land_with_pause(MODE_REASON_EKF_FAILSAFE); |
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// } |
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// break; |
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// default: |
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// set_mode_land_with_pause(MODE_REASON_EKF_FAILSAFE); |
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// break; |
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// } |
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// |
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// // if flight mode is already LAND ensure it's not the GPS controlled LAND |
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// if (control_mode == LAND) { |
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// land_do_not_use_GPS(); |
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// } |
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} |
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// failsafe_ekf_off_event - actions to take when EKF failsafe is cleared |
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void Sub::failsafe_ekf_off_event(void) |
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{ |
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// return immediately if not in ekf failsafe |
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if (!failsafe.ekf) { |
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return; |
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} |
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// clear flag and log recovery |
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failsafe.ekf = false; |
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Log_Write_Error(ERROR_SUBSYSTEM_FAILSAFE_EKFINAV, ERROR_CODE_FAILSAFE_RESOLVED); |
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}
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