Patent classifications
B64D45/00
SYSTEM AND METHOD FOR CONTEXTUALLY-INFORMED FAULT DIAGNOSTICS USING STRUCTURAL-TEMPORAL ANALYSIS OF FAULT PROPAGATION GRAPHS
A method is provided for diagnosing a failure on an aircraft that includes aircraft systems and monitors configured to report effects of failure modes of the aircraft systems. The method includes receiving a fault report that indicates one or more of the monitors that reported the effects of a failure mode in an aircraft system of the aircraft systems, and accessing a fault pattern library that describes relationships between possible failure modes and patterns of those of the monitors configured to report the effects of the possible failure modes. The method also includes diagnosing the failure mode of the aircraft system from the one or more of the monitors that reported, and using the fault pattern library and a greedy selection algorithm, determining a maintenance action for the failure mode; and generating a maintenance message including at least the maintenance action.
SYSTEM AND METHOD FOR CONTEXTUALLY-INFORMED FAULT DIAGNOSTICS USING STRUCTURAL-TEMPORAL ANALYSIS OF FAULT PROPAGATION GRAPHS
A method is provided for diagnosing a failure on an aircraft that includes aircraft systems and monitors configured to report effects of failure modes of the aircraft systems. The method includes receiving a fault report that indicates one or more of the monitors that reported the effects of a failure mode in an aircraft system of the aircraft systems, and accessing a fault pattern library that describes relationships between possible failure modes and patterns of those of the monitors configured to report the effects of the possible failure modes. The method also includes diagnosing the failure mode of the aircraft system from the one or more of the monitors that reported, and using the fault pattern library and a greedy selection algorithm, determining a maintenance action for the failure mode; and generating a maintenance message including at least the maintenance action.
PHYSIOLOGICAL AND BEHAVIOURAL METHODS TO ASSESS PILOT READINESS
A system and method for automatically assessing pilot readiness via a plurality of biometric sensors includes continuously receiving biometric data including vision-based data; the biometric vision-based data is compared to a task specific set of movements and facial expressions as defined by known anchor points. A deviation is calculated based on the vision-based data and task specific set of movements and expressions, and the deviation is compared to an acceptable threshold for pilot readiness. Other biometric data may be included to refine the readiness assessment.
PHYSIOLOGICAL AND BEHAVIOURAL METHODS TO ASSESS PILOT READINESS
A system and method for automatically assessing pilot readiness via a plurality of biometric sensors includes continuously receiving biometric data including vision-based data; the biometric vision-based data is compared to a task specific set of movements and facial expressions as defined by known anchor points. A deviation is calculated based on the vision-based data and task specific set of movements and expressions, and the deviation is compared to an acceptable threshold for pilot readiness. Other biometric data may be included to refine the readiness assessment.
FLIGHT RECORDER SYSTEM AND METHOD
A flight recorder system of an aircraft includes a resource controller module (RCM) communicatively coupled, via a switch fabric, to a set of flight recorder system modules (FRM). Each FRM comprises a respective control module, a respective local memory, and a respective set of input and output (I/O) ports communicatively coupled to the switch fabric. The RCM is configured to detect a respective FRM coupled to the switch fabric, and based on the detection, configure an operation of the FRM, and wherein the respective local memory of the FRM is readable by the RCM, and shareable with the other FRMs via the switch fabric.
FLIGHT RECORDER SYSTEM AND METHOD
A flight recorder system of an aircraft includes a resource controller module (RCM) communicatively coupled, via a switch fabric, to a set of flight recorder system modules (FRM). Each FRM comprises a respective control module, a respective local memory, and a respective set of input and output (I/O) ports communicatively coupled to the switch fabric. The RCM is configured to detect a respective FRM coupled to the switch fabric, and based on the detection, configure an operation of the FRM, and wherein the respective local memory of the FRM is readable by the RCM, and shareable with the other FRMs via the switch fabric.
COGNITIVE BATTERY FOR RETURN TO SERVICE
A computerized system for recognizing the need for cognitive tests due to a physiological event and administering such tests includes a plurality of biometric monitoring devices and a pilot input device. When a physiological event is identified, the system selects an appropriate battery of tests and automatically administers those tests. The system offers the opportunity to automate pilot evaluation for single pilot operations, and to reduce the burden on a co-pilot. The cognitive tests may be specific to the physiological event, and may be compared to a pilot-specific profile when evaluating the results
PILOT SAFETY SYSTEM WITH CONTEXT-SENSITIVE SCAN PATTERN MONITORING AND ALERTING
An aircraft-based pilot safety system (PSS) includes cameras or other gaze sensors fixed at an aircraft pilot and configured to capture an image stream focused on the pilot's eyes. The gaze sensors continually assess the gaze direction of the pilot (e.g., toward a display, instrument panel, and/or indicator within the cockpit that the pilot is currently looking at or focusing on) and thereby can establish when the pilot is executing a scan pattern and if that scan pattern is nominal for the current flight context by comparing the scan pattern to context-specific reference scan patterns. If, for example, the pilot's gaze deviates from where it should be (e.g., as determined by the current flight segment) or the current scan pattern is interrupted, the system may prompt the pilot to redirect their gaze or resume the scan pattern.
PILOT SAFETY SYSTEM WITH CONTEXT-SENSITIVE SCAN PATTERN MONITORING AND ALERTING
An aircraft-based pilot safety system (PSS) includes cameras or other gaze sensors fixed at an aircraft pilot and configured to capture an image stream focused on the pilot's eyes. The gaze sensors continually assess the gaze direction of the pilot (e.g., toward a display, instrument panel, and/or indicator within the cockpit that the pilot is currently looking at or focusing on) and thereby can establish when the pilot is executing a scan pattern and if that scan pattern is nominal for the current flight context by comparing the scan pattern to context-specific reference scan patterns. If, for example, the pilot's gaze deviates from where it should be (e.g., as determined by the current flight segment) or the current scan pattern is interrupted, the system may prompt the pilot to redirect their gaze or resume the scan pattern.
VEHICLE OPERATOR MONITORING SYSTEM WITH SMART ACTIVE ENGAGEMENT AND DISENGAGEMENT
An operator safety system (OSS) monitors the physiological well-being of an aircraft pilot or vehicle operator, and has engaged and disengaged operational states (the engaged state associated with active monitoring). The OSS includes a smart engage/disengage system incorporating presence sensors (e.g., visual, seat-based) installed in the cockpit or control area of the vehicle. When the presence sensors determine that the pilot/operator is no longer present in their seat but the OSS is still engaged, the OSS prompts the operator to disengage the OSS (e.g., via single-touch display interface or remotely to a mobile device). When the presence sensors determine that the operator is present or seated, but the OSS is disengaged, the OSS prompts the operator to re-engage the OSS.