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：US10946977B2

公开(公告)日：2021-03-16

申请号：US15959485

申请日：2018-04-23

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： Rajeev Mohan ,  Sreenivasan Govindillam K ,  Srihari Jayathirtha ,  Kalimulla Khan ,  Ravish Udupa

IPC: G08G5/00 ,  G01C21/00 ,  B64D43/00 ,  B64D45/00

Abstract: Methods and systems are provided for integrating aircraft flight parameters generated by an offboard portable electronic device (PED) into an onboard flight management system (FMS). The method comprises selecting the aircraft flight parameters to be generated by the PED for use by the FMS. The current flight data is accessed for the aircraft with the FMS and providing the current flight data to the offboard PED. The rules for the aircraft flight parameters are computed with the offboard PED based on the current flight data for the aircraft and transmitted to a flight management (FM) adapter. The FM adapter confirms that the rules for the aircraft flight parameters comply with operational limits of the aircraft and then translates the rules of the aircraft flight parameters to aircraft operational targets for use by the onboard FMS. The aircraft operational targets are then loaded from the FM adapter into the FMS.

公开(公告)号：US10755583B2

公开(公告)日：2020-08-25

申请号：US15790220

申请日：2017-10-23

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： Abneesh Singla ,  Sreenivasan Govindillam K ,  Srinivas D. Gonabal ,  Pradeep Huncha ,  Vedavyas Rallabandi ,  Jaibir Singh ,  Sunil Kumar KS

IPC: G08G5/00 ,  G08G5/02 ,  G06F3/16

Abstract: A method is provided for monitoring compliance with air traffic control (ATC) instructions by an air crew of an aircraft. First, voice and text ATC commands are received by an ATC instruction moderator support system (AIMSS) located on board the aircraft. The voice and text ATC commands are converted into a data format by the AIMSS. The ATC commands are used to determine an expected aircraft state while a current aircraft state is determined by the aircraft sensors. The current aircraft state is compared with the expected state and determined if it is in compliance. If the current state is in non-compliance, it is determined if the non-compliance is allowable and it is then classified as either no action or incorrect action by the aircrew. Finally, an alert of the noncompliance is generated with the AIMSS.

公开(公告)号：US20190152619A1

公开(公告)日：2019-05-23

申请号：US15959485

申请日：2018-04-23

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： Rajeev Mohan ,  Sreenivasan Govindillam K ,  Srihari Jayathirtha ,  Kalimulla Khan ,  Ravish Udupa

IPC: B64D43/00 ,  G08G5/00

Abstract: Methods and systems are provided for integrating aircraft flight parameters generated by an offboard portable electronic device (PED) into an onboard flight management system (FMS). The method comprises selecting the aircraft flight parameters to be generated by the PED for use by the FMS. The current flight data is accessed for the aircraft with the FMS and providing the current flight data to the offboard PED. The rules for the aircraft flight parameters are computed with the offboard PED based on the current flight data for the aircraft and transmitted to a flight management (FM) adapter. The FM adapter confirms that the rules for the aircraft flight parameters comply with operational limits of the aircraft and then translates the rules of the aircraft flight parameters to aircraft operational targets for use by the onboard FMS. The aircraft operational targets are then loaded from the FM adapter into the FMS.

公开(公告)号：US20190122564A1

公开(公告)日：2019-04-25

申请号：US15790220

申请日：2017-10-23

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： Abneesh Singla ,  Sreenivasan Govindillam K ,  Srinivas D. Gonabal ,  Pradeep Huncha ,  Vedavyas Rallabandi ,  Jaibir Singh ,  Sunil Kumar KS

IPC: G08G5/00

CPC classification number: G08G5/0013 ,  G06F3/167 ,  G08G5/0021 ,  G08G5/0026 ,  G08G5/006 ,  G08G5/0082 ,  G08G5/025

Abstract: A method is provided for monitoring compliance with air traffic control (ATC) instructions by an air crew of an aircraft. First, voice and text ATC commands are received by an ATC instruction moderator support system (AIMSS) located on board the aircraft. The voice and text ATC commands are converted into a data format by the AIMSS. The ATC commands are used to determine an expected aircraft state while a current aircraft state is determined by the aircraft sensors. The current aircraft state is compared with the expected state and determined if it is in compliance. If the current state is in non-compliance, it is determined if the non-compliance is allowable and it is then classified as either no action or incorrect action by the aircrew. Finally, an alert of the noncompliance is generated with the AIMSS.

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.