-
公开(公告)号:US20250091730A1
公开(公告)日:2025-03-20
申请号:US18818803
申请日:2024-08-29
Applicant: Honeywell International Inc.
Inventor: Kirupakar J , Kalimulla Khan , Ramkumar Rajendran , Shirish Katti , Mahima Banerjee , Rohit Pandita , Jyothsna Peram
Abstract: Techniques for optimizing flight safety operations for an aircraft are described. In operation, aircraft operational parameters corresponding to a plurality of flight operations are retrieved. The aircraft operational parameters are then analyzed using a first machine learning model to identify a first flight operation, where the first flight operation comprises at least one aircraft operational parameter with deviation beyond a threshold. At least one potential flight safety incident corresponding to the first flight operation is then identified using the at least one aircraft operational parameter. The at least one potential flight safety incident is then analyzed using a second machine learning model to identify a corrective action for the potential flight safety incident, where the second machine learning model is trained using flight safety artifacts comprising a plurality of flight safety incidents and corrective actions to be initiated in response to the plurality of flight safety incidents. The corrective action is then subjected to an avionics digital twin to ascertain that the corrective action mitigates the at least one potential flight safety incident. The corrective action is then recommended for the at least one potential flight safety incident.