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    SYSTEM AND METHOD TO AUTOMATICALLY CONSTRUCT A FLIGHT PLAN FROM A DATA SET FOR AN AERIAL VEHICLE
    1.
    发明申请
    SYSTEM AND METHOD TO AUTOMATICALLY CONSTRUCT A FLIGHT PLAN FROM A DATA SET FOR AN AERIAL VEHICLE 有权

    公开(公告)号：US20210343159A1

    公开(公告)日：2021-11-04

    申请号：US16904227

    申请日：2020-06-17

    Applicant: Honeywell International Inc.

    Inventor： Sanju Kuriakose ,  Anoop S ,  Sabu Mathew ,  Niranjan Kumar ,  Jan Hart ,  Janaki Seetharaman

    IPC: G08G5/00 ,  G06F16/29

    Abstract: A system for automatically constructing a flight plan that aligns with a boundary line is provided. The system has a controller that is configured to: automatically select a set of geographical (geo) coordinate waypoints along a boundary line using waypoints from the geographical database responsive to flight crew input; refine the set of geo coordinate waypoints using a calculated turn initiation distance and a turn completion distance for every waypoint; further refine the refined set of geo coordinate waypoints based on the course change between waypoints; generate a set of courses and distances between waypoints through computing, for each set of two consecutive waypoints in the further refined set of geo coordinate waypoints, the course and distance between the two consecutive waypoints; and construct the flight plan based on the waypoints in the further refined set of geo coordinate waypoints and the set of courses and distances between waypoints.

    Methods, systems, and apparatuses for identifying and indicating the secondary runway aiming point (SRAP) approach procedures
    2.
    发明授权
    Methods, systems, and apparatuses for identifying and indicating the secondary runway aiming point (SRAP) approach procedures 有权

    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

    IPC: G01C23/00 ,  G08G5/02 ,  G08G5/00

    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.

    Safe sonic altitude generation
    4.
    发明授权
    Safe sonic altitude generation 有权

    公开(公告)号：US10460612B2

    公开(公告)日：2019-10-29

    申请号：US15823867

    申请日：2017-11-28

    Applicant: HONEYWELL INTERNATIONAL INC.

    Inventor： Nathan K ,  Anoop S ,  Sabu Mathew

    IPC: G08G5/00 ,  B64C30/00

    Abstract: Methods and systems for flight control of a supersonic ownship are provided. The systems utilize sources of weather data, a flight management system (FMS) of the supersonic ownship, and sources of neighbor traffic data. The systems generate a complete neighbor traffic flight trajectory, and then process the complete neighbor traffic flight trajectory with a flight plan of the supersonic ownship, aircraft specific parameters, and forecasted and real-time weather data to generate therefrom a safe sonic altitude for flying the supersonic ownship. The safe sonic altitude is transmitted to air traffic control (ATC) as a request for an assignment. Upon receiving the assignment from ATC, the systems notify the pilot of the assignment and continue monitoring airspace for real-time changes in the flight path trajectory of the neighbor traffic. The sonic altitude is updated based on a detected real-time change in the flight path trajectory of the neighbor traffic.

    System and method to automatically construct a flight plan from a data set for an aerial vehicle
    7.
    发明授权
    System and method to automatically construct a flight plan from a data set for an aerial vehicle 有权

    公开(公告)号：US11348472B2

    公开(公告)日：2022-05-31

    申请号：US16904227

    申请日：2020-06-17

    Applicant: HONEYWELL INTERNATIONAL INC.

    Inventor： Sanju Kuriakose ,  Anoop S ,  Sabu Mathew ,  Niranjan Kumar ,  Jan Hart ,  Janaki Seetharaman

    IPC: G08G5/00 ,  G06F16/29

    Abstract: A system for automatically constructing a flight plan that aligns with a boundary line is provided. The system has a controller that is configured to: automatically select a set of geographical (geo) coordinate waypoints along a boundary line using waypoints from the geographical database responsive to flight crew input; refine the set of geo coordinate waypoints using a calculated turn initiation distance and a turn completion distance for every waypoint; further refine the refined set of geo coordinate waypoints based on the course change between waypoints; generate a set of courses and distances between waypoints through computing, for each set of two consecutive waypoints in the further refined set of geo coordinate waypoints, the course and distance between the two consecutive waypoints; and construct the flight plan based on the waypoints in the further refined set of geo coordinate waypoints and the set of courses and distances between waypoints.

    SAFE SONIC ALTITUDE GENERATION
    9.
    发明申请
    SAFE SONIC ALTITUDE GENERATION 审中-公开

    公开(公告)号：US20190164437A1

    公开(公告)日：2019-05-30

    申请号：US15823867

    申请日：2017-11-28

    Applicant: HONEYWELL INTERNATIONAL INC.

    Inventor： Nathan K ,  Anoop S ,  Sabu Mathew

    IPC: G08G5/00

    CPC classification number: G08G5/0039 ,  B64C30/00 ,  G08G5/0013 ,  G08G5/0021 ,  G08G5/0047 ,  G08G5/0052 ,  G08G5/0091

    Abstract: Methods and systems for flight control of a supersonic ownship are provided. The systems utilize sources of weather data, a flight management system (FMS) of the supersonic ownship, and sources of neighbor traffic data. The systems generate a complete neighbor traffic flight trajectory, and then process the complete neighbor traffic flight trajectory with a flight plan of the supersonic ownship, aircraft specific parameters, and forecasted and real-time weather data to generate therefrom a safe sonic altitude for flying the supersonic ownship. The safe sonic altitude is transmitted to air traffic control (ATC) as a request for an assignment. Upon receiving the assignment from ATC, the systems notify the pilot of the assignment and continue monitoring airspace for real-time changes in the flight path trajectory of the neighbor traffic. The sonic altitude is updated based on a detected real-time change in the flight path trajectory of the neighbor traffic.

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