公开(公告)号：US20180158343A1

公开(公告)日：2018-06-07

申请号：US15370029

申请日：2016-12-06

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： Pramod Kumar Malviya ,  Pradeep Huncha ,  Vinay Somashekar ,  Sreenivasan Govindillam K ,  Nathan K ,  Anoop S ,  Sunitha Panchangam

IPC: G08G5/00 ,  G01C21/00 ,  B64D43/00

CPC classification number: G08G5/0034 ,  B64D43/00 ,  B64D45/08 ,  G01C21/00 ,  G01C21/20 ,  G01C23/005 ,  G08G5/0021 ,  G08G5/0052 ,  G08G5/025

Abstract: Systems and methods are provided for displaying portions of a route on a coverage map that are non-compliant for a Global Navigation Satellite System (GNSS) navigation system in an aircraft. A route compliance module defines a geodetic reference datum standard based on the GNSS navigation system. A navigation system database has compliance information corresponding to each of a plurality of airports. A flight management system determines the route of the aircraft and a visual display displays the route and the coverage map. The route compliance module identifies a non-compliant region of the coverage map that is not compliant with the geodetic reference datum standard based on the compliance information and adjusts the visual display to differentiate a non-compliant portion of the route extending within the non-compliant region of the coverage map.

公开(公告)号：US20190248504A1

公开(公告)日：2019-08-15

申请号：US15892583

申请日：2018-02-09

Applicant: Honeywell International Inc.

Inventor： Nathan K ,  Sreenivasan Govindillam K

IPC: B64D43/00 ,  G06Q30/04

CPC classification number: B64D43/00 ,  B64D2045/0075 ,  G06Q30/04

Abstract: A method is provided. The method comprises receiving a travel plan for a vehicle including a travel path information; determining a vehicle trajectory using the travel path information; obtaining forecasts of at least one of weather and vehicles proximate in time and location to the vehicle along the vehicle trajectory; determining, based upon at least one of the weather forecast and the other vehicles forecast, if at least one optional function would be beneficial to enable during vehicle travel along the vehicle trajectory; and generating at least one enablement code corresponding to the determined at least one optional function.

公开(公告)号：US10297162B2

公开(公告)日：2019-05-21

申请号：US15392128

申请日：2016-12-28

Applicant: Honeywell International Inc.

Inventor： Sreenivasan Govindillam K ,  Nathan K ,  Sujith Kalarickal

IPC: H04W12/00 ,  G08G5/00 ,  G06Q20/10 ,  G06Q30/04 ,  H04W12/02 ,  H04L9/08 ,  B64D43/00 ,  G06F16/23 ,  G07C5/00

Abstract: In one embodiment, a vehicle is provided. The vehicle comprises a vehicle control system, at least one vehicle control coupled to the vehicle control system, a vehicle communications system coupled to the vehicle control system, wherein the vehicle control system is configured to enable one or more vehicle functions upon receipt of a function enablement key provided through the vehicle communications system from an operations center, and wherein the vehicle control system is configured to transmit confirmation data from the vehicle to the operations center.

公开(公告)号：US20180247548A1

公开(公告)日：2018-08-30

申请号：US15443168

申请日：2017-02-27

Applicant: Honeywell International Inc.

Inventor： Sunitha Panchangam ,  Anoop S ,  Prasanna Murthy Gurajapu ,  Nathan K

IPC: G08G5/00 ,  B64D43/00 ,  H04B7/185 ,  G06T11/60

CPC classification number: G08G5/0091 ,  B64D43/00 ,  G01C23/00 ,  G06T11/60 ,  G08G5/0013 ,  G08G5/0021 ,  G08G5/003 ,  G08G5/0052 ,  H04B7/18506 ,  H04W84/005

Abstract: A method of supplementing high design assurance level system information for an aircraft is provided. The method includes dynamically gathering low design assurance level information from the internet with a communication system based on a requests by a cockpit browser. The low design assurance level information is parsed with the high design assurance level information with a parser of the cockpit browser to generate combined assurance level information. The combined assurance level information is displayed on a display.

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.

公开(公告)号：US20180182252A1

公开(公告)日：2018-06-28

申请号：US15392128

申请日：2016-12-28

Applicant: Honeywell International Inc.

Inventor： Sreenivasan Govindillam K ,  Nathan K ,  Sujith Kalarickal

IPC: G08G5/00 ,  G06Q20/10 ,  G06Q30/04 ,  H04W12/02 ,  H04L9/08 ,  G06F17/30 ,  B64D43/00

CPC classification number: G08G5/0095 ,  B64D43/00 ,  G06F17/30377 ,  G06Q20/102 ,  G06Q30/04 ,  G07C5/008 ,  H04L9/0866 ,  H04L2209/80 ,  H04L2209/84 ,  H04W12/02

Abstract: In one embodiment, a vehicle is provided. The vehicle comprises a vehicle control system, at least one vehicle control coupled to the vehicle control system, a vehicle communications system coupled to the vehicle control system, wherein the vehicle control system is configured to enable one or more vehicle functions upon receipt of a function enablement key provided through the vehicle communications system from an operations center, and wherein the vehicle control system is configured to transmit confirmation data from the vehicle to the operations center.

公开(公告)号：US20210061485A1

公开(公告)日：2021-03-04

申请号：US17098116

申请日：2020-11-13

Applicant: Honeywell International Inc.

Inventor： Nathan K ,  Sreenivasan Govindillam K

IPC: B64D43/00 ,  G06Q30/04

Abstract: A method is provided. The method comprises receiving a travel plan for a vehicle including a travel path information; determining a vehicle trajectory using the travel path information; obtaining forecasts of at least one of weather and vehicles proximate in time and location to the vehicle along the vehicle trajectory; determining, based upon at least one of the weather forecast and the other vehicles forecast, if at least one optional function would be beneficial to enable during vehicle travel along the vehicle trajectory; and generating at least one enablement code corresponding to the determined at least one optional function.

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.

公开(公告)号：US10176721B2

公开(公告)日：2019-01-08

申请号：US15370029

申请日：2016-12-06

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： Pramod Kumar Malviya ,  Pradeep Huncha ,  Vinay Somashekar ,  Sreenivasan Govindillam K ,  Nathan K ,  Anoop S ,  Sunitha Panchangam

IPC: G08G5/00 ,  B64D45/08 ,  G01C23/00 ,  G01C21/20 ,  G01C21/00 ,  B64D43/00

Abstract: Systems and methods are provided for displaying portions of a route on a coverage map that are non-compliant for a Global Navigation Satellite System (GNSS) navigation system in an aircraft. A route compliance module defines a geodetic reference datum standard based on the GNSS navigation system. A navigation system database has compliance information corresponding to each of a plurality of airports. A flight management system determines the route of the aircraft and a visual display displays the route and the coverage map. The route compliance module identifies a non-compliant region of the coverage map that is not compliant with the geodetic reference datum standard based on the compliance information and adjusts the visual display to differentiate a non-compliant portion of the route extending within the non-compliant region of the coverage map.