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公开(公告)号:US11854418B2
公开(公告)日:2023-12-26
申请号:US17070830
申请日:2020-10-14
Applicant: Honeywell International Inc.
Inventor: Vipul Gupta , Lawrence J. Surace , Sujaya Rao , Rajesh Chenchu , Siva Prasad Kolli , Vinod Prakash Singh
CPC classification number: G08G5/045 , G08G5/0013 , G08G5/0043 , G08G5/065 , H04W4/42
Abstract: This disclosure is directed to methods, computer program products, and systems for providing surface vehicle tracking data, including indications of potential collision zones, to an airport map display system onboard an aircraft. In one example, a method includes identifying historical navigation route data, aerodrome guidance features, and a predicted path of a first vehicle. The method further includes determining predicted positions along the predicted path and determining predicted positions of a second vehicle and comparing vehicle envelopes for the two vehicles to determine a predicted collision zone of the vehicles.
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公开(公告)号:US20210256858A1
公开(公告)日:2021-08-19
申请号:US17070830
申请日:2020-10-14
Applicant: Honeywell International Inc.
Inventor: Vipul Gupta , Lawrence J. Surace , Sujaya Rao , Rajesh Chenchu , Siva Prasad Kolli , Vinod Prakash Singh
Abstract: This disclosure is directed to methods, computer program products, and systems for providing surface vehicle tracking data, including indications of potential collision zones, to an airport map display system onboard an aircraft. In one example, a method includes identifying historical navigation route data, aerodrome guidance features, and a predicted path of a first vehicle. The method further includes determining predicted positions along the predicted path and determining predicted positions of a second vehicle and comparing vehicle envelopes for the two vehicles to determine a predicted collision zone of the vehicles.
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公开(公告)号:US10546503B2
公开(公告)日:2020-01-28
申请号:US15683267
申请日:2017-08-22
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor: Rajesh Chenchu , Durga Prasad Dhulipudi , Vijaya Bhaskar Ramisetti , Reshma Seelam , Amit Srivastav , Don Nicholas
Abstract: A method for validating an operational flight path of an aircraft has been developed. First, a flight path for the aircraft is created using navigation, terrain and obstacle data retrieved from off-line databases. Next, real-time terrain and obstacle update information is captured from flight data sensors on board the aircraft while in flight. Also, light direction and range (LIDAR) data from LIDAR sensors on board the aircraft is collected. A boundary profile is calculated for the flight path based upon the real-time terrain and obstacle update information in combination with the LIDAR data. The flight path is validated using the boundary profile. The results of the validation of the flight path is generated as a report for the aircraft crew.
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公开(公告)号:US11509675B2
公开(公告)日:2022-11-22
申请号:US17097558
申请日:2020-11-13
Applicant: Honeywell International Inc.
Inventor: Amit Srivastav , Rajesh Chenchu , Nayyar Azam Khan Rao , Phani Ammi Raju Pothula , Vijayshankaran Iyer
IPC: H04L9/40 , H04L67/12 , H04L43/045 , G06N20/00 , H04L41/16
Abstract: A method of monitoring network traffic of a connected vehicle. The method includes receiving network traffic information from a vehicle gateway, the network traffic information including malicious and/or benign information. The method also includes storing the network traffic information on a data server and periodically updating the network traffic information stored on the data server. The method further includes: pre-processing the network traffic information, the pre-processing the network traffic information including filtering and normalizing the network traffic information; generating a learning model based on the pre-processed network traffic information, the learning model being generated by an artificial intelligence learning; updating the learning model based on additional network traffic information, the additional network traffic information including real-time network data; in accordance with the updated learning model, detecting an anomaly event in the incoming network data; and generating a notification and/or blocking one or more packets associated with the incoming network data.
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公开(公告)号:US20210020056A1
公开(公告)日:2021-01-21
申请号:US16513219
申请日:2019-07-16
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor: Rajesh Chenchu , Amit Srivastav , Raju Siravuri , SivaPrasad Kolli
Abstract: A system for detecting aircraft trajectory anomalies during takeoff or landing is configured to: identify, from a clearance message directed to a first aircraft, an approved runway and an approved landing or takeoff procedure; select a runway-specific trained model appropriate for the approved procedure, the selected trained model having been trained with historical track data from other aircraft performing the approved procedure in connection with the approved runway, the selected trained model configured to provide an expected trajectory for an aircraft during performance of the approved procedure in connection with the approved runway; receive aircraft state information from the first aircraft during performance of the approved procedure; monitor and compare the received aircraft state information to the expected trajectory from the trained model; identify an anomaly and generate an alert when the trajectory of the first aircraft deviates from the expected trajectory by more than a predetermined threshold level.
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公开(公告)号:US20190066518A1
公开(公告)日:2019-02-28
申请号:US15683267
申请日:2017-08-22
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor: Rajesh Chenchu , Durga Prasad Dhulipudi , Vijaya Bhaskar Ramisetti , Reshma Seelam , Amit Srivastav , Don Nicholas
CPC classification number: G08G5/0034 , G08G5/0013 , G08G5/0021 , G08G5/0052 , G08G5/0086 , G08G5/045
Abstract: A method for validating an operational flight path of an aircraft has been developed. First, a flight path for the aircraft is created using navigation, terrain and obstacle data retrieved from off-line databases. Next, real-time terrain and obstacle update information is captured from flight data sensors on board the aircraft while in flight. Also, light direction and range (LIDAR) data from LIDAR sensors on board the aircraft is collected. A boundary profile is calculated for the flight path based upon the real-time terrain and obstacle update information in combination with the LIDAR data. The flight path is validated using the boundary profile. The results of the validation of the flight path is generated as a report for the aircraft crew.
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