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公开(公告)号:US11030907B1
公开(公告)日:2021-06-08
申请号:US16983191
申请日:2020-08-03
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor: Anoop S , Sabu Mathew , Nathan Krishna Moorthy , Sunitha Panchangam
Abstract: Methods, systems, and apparatuses are provided for a Secondary Runway Aiming Point (SRAP) procedure of an approach by an ownship that includes identifying at least one aircraft making an approach that satisfy a set of preconditions to pair the aircraft to the ownship in the SRAP procedure; calculating a set of results based on lateral and vertical deviations of a paired SRAP aircraft to the ownship, and differential lateral and vertical rates of the paired SRAP aircraft to the ownship; deriving one or more points from the calculated set of results to determine whether in a flight path of the ownship there is an occurrence of an intrusion into a wake of the paired SRAP aircraft during the approach, and generating graphic data to present on the cockpit display the occurrence of the intrusion in the wake of the flight path of the ownship to the paired SRAP aircraft.
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公开(公告)号:US20220165168A1
公开(公告)日:2022-05-26
申请号:US17144401
申请日:2021-01-08
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor: Anoop Surendran , Nathan Krishna Moorthy
Abstract: A system and method to automatically control aerodrome lighting from an aircraft includes selectively retrieving, via a processor, aerodrome lighting data associated with an individual aerodrome from an aerodrome lighting data source. Images are captured, using a camera having a field of view and being mounted on the aircraft, of aerodrome lighting within the camera's field of view. Image data representative of an intensity of light transmitted from the aerodrome lighting within the camera's field of view are supplied from the camera to the processor. The aerodrome lighting data and image data are processed in the processor and, in response to processing the aerodrome lighting data and the image data, commands are selectively supplied, via the processor, to a communication radio that cause the communication radio to transmit RF signals consistent with the light control characteristics associated with the individual aerodrome and based on image data supplied from the camera.
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3.
公开(公告)号:US20240321114A1
公开(公告)日:2024-09-26
申请号:US18318013
申请日:2023-05-16
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor: Ari Narayanan M , Nathan Krishna Moorthy , Sivasankari Paramasivan
CPC classification number: G08G5/0021 , G08G5/003 , G08G5/045
Abstract: A method and system for identifying a restrictive obstacle for a flight plan of an aircraft has been developed. First, both static obstacle data and temporary obstacle data is retrieved for a runway used during takeoff of the aircraft. The relevant data is identified for clearance of the static obstacles and the temporary obstacles. The distance and elevation of the static obstacles and the temporary obstacles is computed from a departure point of the runway. Next, the clearance data required for the aircraft is computed for each of the static obstacles and the temporary obstacles. The most restrictive obstacle is identified based on the clearance data for each of the static obstacles and the temporary obstacles and displayed to the pilot of the aircraft.
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4.
公开(公告)号:US20240021086A1
公开(公告)日:2024-01-18
申请号:US17933194
申请日:2022-09-19
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor: Raghu Shamasundar , Kalimulla Khan , Sreenivasan Govindillam , Nathan Krishna Moorthy
CPC classification number: G08G5/0004 , G06K7/143
Abstract: A flight deck system is configured to: receive a data model populated with flight data obtained while performing a core avionics function; receive configuration information from an external source that identifies a specific plurality of flight data items to extract from the data model; extract from the data model data values for the specific plurality of flight data items identified in the configuration information; generate an optical code that encodes the extracted data values; generate an HMI display that provides a selectable link for causing the optical code to be displayed in the aircraft; cause the HMI display to be display on an aircraft display; and cause the optical code to be displayed on an aircraft display responsive to selection of the selectable link; wherein the optical code provides encoded data values corresponding to the specific plurality of flight data items for decoding and display by a mobile device.
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