公开(公告)号：US12148311B2

公开(公告)日：2024-11-19

申请号：US17007822

申请日：2020-08-31

Applicant: Honeywell International Inc.

Inventor： Aralakuppe Yogesha ,  Shouvik Das ,  Mohammed Ibrahim Mohideen ,  Perumal Kumar ,  Rafeek Sainudeen ,  Parag Rao ,  Abhishek Alladi

IPC: B64U30/20 ,  G05D1/00 ,  G06N20/00 ,  G08G5/00

Abstract: Disclosed are methods, systems, and non-transitory computer-readable medium for managing energy use in a vehicle. For instance, the method may include receiving forecasted data from a first external source, receiving real-time data corresponding to at least one weather parameter at a first location at a first time, and continuously determining whether to perform an adjustment to a control parameter of the vehicle by using a machine learning model that is based on the forecasted data for the at least one weather parameter, the real-time data for the at least one weather parameter, a battery condition of the vehicle, and/or an estimated amount of energy consumed by traveling along a first navigation path.

公开(公告)号：US20240274019A1

公开(公告)日：2024-08-15

申请号：US18193213

申请日：2023-03-30

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： Mohammed Ibrahim Mohideen ,  Anil Kumar Songa ,  Saravanakumar Gurusamy ,  Bincicil Mathew ,  Anita Sure ,  Harish Nagarajaiah ,  Roshini Mehboob

IPC: G08G5/04 ,  B64D43/00 ,  B64D47/04 ,  F21S8/00 ,  F21V21/15 ,  G08G5/00

CPC classification number: G08G5/045 ,  B64D43/00 ,  B64D47/04 ,  F21S8/003 ,  F21V21/15 ,  G08G5/0047 ,  G08G5/0073 ,  B64C27/04

Abstract: Methods and systems are provided for promoting collision threat awareness for a mobile platform. The system comprises a searchlight to emit a beam of light and means for articulating the searchlight, a sensor system to sense a location, elevation, and orientation of the mobile platform and/or locations and elevations of obstacles including terrain and manmade objects, a source of data including the locations and elevations of the obstacles, and a controller configured to, by a processor: identify a first obstacle that poses a collision threat to the mobile platform based on the location, elevation, and/or orientation of the mobile platform and the location and elevation of the first obstacle, and operate the searchlight assembly to: automatically direct the beam of light toward the first obstacle, and/or automatically direct the beam of light toward an escape route that allows the mobile platform to avoid collision with the first obstacle.

公开(公告)号：US12033515B2

公开(公告)日：2024-07-09

申请号：US17815295

申请日：2022-07-27

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： Prem Kumar T ,  Karthic V ,  Kalaiarasu Velappan ,  Gireesh Kumar R N ,  Mohammed Ibrahim Mohideen ,  Janakiram Thiyagarajan

IPC: G08G5/00 ,  G08G5/02 ,  G08G5/04

CPC classification number: G08G5/0008 ,  G08G5/0021 ,  G08G5/0078 ,  G08G5/0091 ,  G08G5/025 ,  G08G5/045

Abstract: A system and method of transmitting an aircraft report (AIREP) from a first aircraft having an enabled aircraft autoland system includes retrieving, via a first processing system, standard AIREP data from one or more avionic systems within the first aircraft, the standard AIREP data including standard AIREP reporting information. The first processing system retrieves autoland enablement data that indicates whether the autoland system was manually or automatically enabled, and also retrieves autoland information data from the one or more avionics systems, where the autoland information data includes current aircraft state data and current flight plan data and is different from the standard AIREP data. The autoland information data is appended to the standard AIREP data to generate an AIREP-autoland message and the AIREP-autoland message is transmitted.

公开(公告)号：US20240124153A1

公开(公告)日：2024-04-18

申请号：US18069375

申请日：2022-12-21

Applicant: Honeywell International Inc.

Inventor： Sadguni Venkataswamy ,  Suresh Bazawada ,  Anil Kumar Songa ,  Mohammed Ibrahim Mohideen

IPC: B64D45/00 ,  G01C23/00

CPC classification number: B64D45/00 ,  G01C23/00 ,  B64C29/0008

Abstract: A method of providing contextual display modes for a vertical takeoff and landing (VTOL) vehicle including obtaining aircraft flight information including a current position and altitude; retrieving vertiport information for a vertiport at the current position of the aircraft; displaying, to one or more operators of the aircraft, a takeoff synthetic vision display mode; transitioning, as the current altitude approaches the transitional altitude, from the takeoff synthetic vision display mode to a cruise synthetic vision display mode, wherein the cruise synthetic vision display mode represents the view from a cruise display viewpoint at the current altitude of the aircraft and at the current position of the aircraft; and displaying, in response to the current altitude equaling or exceeding the transitional altitude, the cruise synthetic vision display mode.

公开(公告)号：US20230161341A1

公开(公告)日：2023-05-25

申请号：US17646702

申请日：2021-12-31

Applicant: Honeywell International Inc.

Inventor： Roberto Gudino MONTOYA ,  Yash Lakhmichand THAWANI ,  Subash SAMUTHIRAPANDIAN ,  Rahul PRADHAN ,  Mohammed Ibrahim Mohideen ,  Jacob Kirk Maxfield

IPC: G05D1/00 ,  G05D1/10 ,  B64D47/08 ,  B64C39/02

CPC classification number: G05D1/0044 ,  G05D1/0038 ,  G05D1/101 ,  G05D1/0094 ,  B64D47/08 ,  B64C39/024 ,  B64C2201/127 ,  B64C2201/146 ,  B64C2201/18

Abstract: Embodiments of the present disclosure assist pilots of aerial vehicles in performing particular operations utilizing improved user interface(s). In some contexts, pilots performing vertical takeoffs or vertical landings cannot visually inspect the environment around the vehicle. Embodiments of the present disclosure utilize virtual elements, including a virtual corridor and virtual vehicle corresponding to an aerial vehicle, to enable improved visualization and control of an aerial vehicle within a particular environment. Utilizing representation(s) of the virtual elements, including a virtual corridor and/or virtual vehicle, embodiments of the present disclosure provide improved user interfaces that assist a pilot in safely controlling an aerial vehicle (even without visual inspection of a real-world environment) during vertical takeoff and/or vertical landing.

公开(公告)号：US20220348350A1

公开(公告)日：2022-11-03

申请号：US17352526

申请日：2021-06-21

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： Anoop S ,  Mohammed Ibrahim Mohideen

IPC: B64D43/02 ,  G08G5/00

Abstract: Methods and systems are provided for displaying multiple time rings on an avionic display. The method includes displaying at least a first time ring in an avionic display; displaying at least a second time ring in the avionic display wherein the first and second time rings include a pair of visually spaced apart time rings wherein a visual spacing apart between the first and second time rings is indicative of a range and a separation flight time between each of the time rings; and displaying, about at least the first time ring in the avionic display, a distance marker of a value for a range and a time marker of a value for separation flight time about an ownship's position and airspeed, and to at least one time ring.

公开(公告)号：US20210225180A1

公开(公告)日：2021-07-22

申请号：US17062781

申请日：2020-10-05

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： Anoop S ,  Mohammed Ibrahim Mohideen ,  Gang He

IPC: G08G5/02 ,  B64C29/00 ,  B64D47/08 ,  G06T7/70 ,  G06T11/00 ,  G06T3/40 ,  G06T3/60

Abstract: The present disclosure relates to a vertical takeoff and landing, VTOL, vehicle having a landing aid and associated methods. The landing aid includes at least one processor is configured to: receive image data from an image capture device, receive altitude data from the altimeter, retrieve template landing pad image data for a target landing pad from the database, scale the template landing pad image data based on the altitude data, compare the scaled template landing pad image data and the image data received from the image capture device to locate the target landing pad therein, thereby providing target landing pad localization data, and control a function of the VTOL vehicle based on the target landing pad localization data.

公开(公告)号：US11043130B2

公开(公告)日：2021-06-22

申请号：US16100763

申请日：2018-08-10

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： Sripathi Ramachandra ,  Greg Carlucci ,  Richard Snyder ,  Mohammed Ibrahim Mohideen ,  Mark Pearson ,  Hyden Lopez ,  Christopher Raj Mariadoss

IPC: G08G5/00 ,  B64C13/04 ,  B64D43/00 ,  G06T11/00 ,  G06T11/20

Abstract: An aircraft and a method for operating the same may include, but is not limited to, a flight management system, a vertical situation display, and a processor configured to determine a first variable, a second variable and a third variable, determine flight plan data for the first, second and third variables, generate display data for the vertical situation display, the display data including the scale of the first second and third variables and a vector corresponding to the flight plan data of the first variable and second variable scaled to the first scale and the second scale, wherein the scale of the third variable is non-linear and varies based upon the flight plan data corresponding to the third variable relative to the vector, and output the generated display data to the vertical situation display for display on the vertical situation display.

公开(公告)号：US10311738B2

公开(公告)日：2019-06-04

申请号：US15588944

申请日：2017-05-08

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： Sachin Pratap ,  Jagadeesh Shankar ,  Visvanathan Thanigai Nathan ,  Mohammed Ibrahim Mohideen ,  Shobana Arumugam

IPC: G08G5/00 ,  B64D43/00 ,  G06F3/0484

Abstract: A display system is configured to provide a display to an aircraft flight crew. The system includes an image display device, a data storage device, a flight management system, a processing unit in operable electronic communication with the image display device, the data storage device, and the flight management system. The processing unit includes a computer processor that is configured to receive a time-based requirement to a point of interest associated with operation of the aircraft. Via the image display device, a flight display includes a graphically depicted time tape. The time tape includes a time scale. Also graphically depicted within the time tape is the point of interest using a first symbology and the time-based requirement using a second symbology. Operational parameter data of the aircraft allows determination of the ability of the aircraft to achieve the time-based requirement and graphical depiction within the time tape of the ability of the aircraft to achieve the time-based requirement using a third symbology.

公开(公告)号：US20180312273A1

公开(公告)日：2018-11-01

申请号：US15582216

申请日：2017-04-28

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： Jeevish Glastine Gurumoorthi ,  Mohammed Ibrahim Mohideen ,  Prabhudev Bhuyar

IPC: B64D45/00 ,  B64D47/08 ,  G08G5/00 ,  G06T19/00 ,  G06T7/20

CPC classification number: B64D45/00 ,  B64D47/08 ,  G01C21/20 ,  G01C23/005 ,  G01J5/00 ,  G01S3/781 ,  G05D1/101 ,  G06T7/20 ,  G06T19/003 ,  G06T19/006 ,  G06T2207/10016 ,  G06T2207/10024 ,  G06T2207/10032 ,  G06T2207/10048 ,  G06T2207/20221 ,  G06T2207/30241 ,  G06T2207/30261 ,  G08B17/125 ,  G08B21/12 ,  G08G5/0086

Abstract: A system is provided for generating an alert to the presence of emission vapors for a low altitude in-flight aircraft. An obstacle database and a terrain database provide parameters for obstacles and terrain features to a synthetic vision processor. The processor creates a graphic overlay of the terrain and obstacles that is combined with thermal images of emission vapors by a combined vision processor to create a combined synthetic image. An emissions threat calculator analyzes the synthetic image for the presence of emission vapors. If any emission vapors are detected in proximity to the aircraft, an alert and suggested maneuvers to avoid the emission vapors are sent to the aircraft.