Honeywell International Inc.

Kalimulla Khan

Raghu Shamasundar

Ramkumar Rajendran

Kirupakar Janakiraman

Srihari Jayathirtha

Mahesh Sivaratri

Subhransu Sahoo

Phillip Toews

Ryan Weeks

Richard Snyder

Sreenivasan Govindillam K

Chavdar Kirov

Kirupakar J

Kiran Mancheiah Venkataramana

Sreenivasan K Govindillam

Jayasenthilnathan Balasubramanian

Karol Molnar

Bijitha Bg

Dinkar A Mylaraswamy

Yi Chen Zhong

Anil Kumar Songa

Dan Li

Rajeev Mohan

Amit Nishikant Kawalkar

Aloke Roy

Mark Pearson

Sripathi Ramachandra

Byron F Birkedahl

Sue McCullough

Ravish Udupa

Kenneth M Leiphon

Umesh Hosamani

Philip Toews

Susan L McCullough

Ivan Markov

Stanislav Foltan

Nayyar Azam Khan Rao

Karel Mundel

Robert Brownlee

Soumitri Swain

Kantha Chikkegowda

Eva Gelnarova

Nathan Krishna Moorthy

Sushma Bidrupane

Sujith Kalarickal

Sreekumar Thekkuttu Pisharam

Todd Wisner

Yogiraj Dattaram More

Deepavali Dinkarrao Desai

Robert Son

Nithya Vasudevan

Angelo Koutsogiannis

Prasanna M R H

Todd Mathis

Dragomir Kamov

Paulo Da Costa Mello

Jagannadha Rao Poluri

Visakh S

Visakh Sivadasan

John R

Disclosed are methods and systems for bi-directional communication between one or more vehicles and a cloud based computing system. For instance, a method may include processing, by a first digital twin of the cloud based computing system, a first request received from and/or sent to a gateway unit associated with a first vehicle, the request comprising data related to one or more vehicle operations; validating, by an avionics data processing service (ADPS) in communication with the gateway unit, the first request against an operational parameter corresponding to the one or more vehicle operations; upon validating the first request, matching, by the ADPS, the operational parameter with a flight operation; and upon matching the operational parameter with the flight operation, inserting, by the ADPS, a modified flight operation into the flight management system of the vehicle.

Systems and methods for bi-directional communication between one or more vehicles and a cloud based computing system

Embodiments of the present disclosure provide techniques for motion stabilized touch control. Reference data comprising one or more stabilized positions for one or more touch points corresponding to one or more touch zones associated with a touch screen device may be generated using a motion stabilization model. One or more touch zones may be adjusted based on the stabilized positions by transmitting-computer executable-instructions configured to cause the one or more touch zones to be aligned with the one or more stabilized positions. One or more touch detection models associated with the touch screen device may be updated by tuning the one or more touch detection models to learn the stabilized positions. One or more dimensions of the one or more touch zones may be recalibrated by adjusting a size of at least one of the one or more touch zones.

Systems, apparatuses, methods, and computer program products for motion stabilized touch control

A system and method in an aircraft for providing enhanced services is provided. In one example, the method includes: setting up triggering logic to identify a beginning point and ending point for collecting a set of avionics system data during a flight; and systematically retrieving information for use by the triggering logic to identify the beginning point and the ending point. When the beginning point is reached, the method includes systematically repeating: retrieving the set of avionics systems data; and sending, to an off-board application, data from the set of avionics system data that has changed state from prior data sent to the off-board application. When the ending point is reached, the method includes cease sending data from the set of avionics system data to the off-board application.

System and method for providing enhanced services

Embodiments of the present disclosure are directed to a cloud-based vehicle monitoring platform (CVMP) configured to manage events impacting the operation of a plurality of vehicles. An onboard vehicle monitoring system associated with a particular vehicle is communicably coupled to CVMP centralized services and can determine corrective actions to employ to mitigate the events. The corrective actions in some contexts are generated by a rules engine based on a rule set generated by a federated learning model associated with the CVMP centralized services. If the onboard vehicle monitoring system determines that a first set of corrective actions generated based on a first set of rules is unsuccessful at mitigating the events, the onboard vehicle monitoring system can request a secondary set of rules from the CVMP centralized services. Various data recovery operations in some contexts are employed to revert the vehicle from a problem state back into a steady state.

Cloud-based vehicle monitoring platform

Disclosed are methods, systems, and one or more computer-readable mediums for receiving, at an edge device from an external server, a rules database comprising a set of rules; receiving, by the edge device, first data from at least one device; processing, by the edge device, the received first data by comparing the received data to each rule among the set of rules; identifying a first triggering event in response to detecting a match between the received data and a rule of the rules database; and outputting an alert corresponding to the first triggering event.

Systems and methods of situation aware edge analytics framework for avionics IOT gateways

Methods and systems for providing platform agnostic flight management data access for a flight management system (FMS) of an aircraft have been developed. First, a configuration file is loaded to a configuration database. The configuration file is for a data format of an external data source from the aircraft. Upon receiving a data access request from a user for external data from the external data source, downloading the configuration file is downloaded to an FMS data formatter. The configuration file is parsed with a data processor component of the FMS data formatter to update a rule set. The FMS data formatter receives an external data file from an application programing interface (API) of the external data source. The external data file is parsed with a rule engine of the FMS data formatter using the updated rule set. A flight plan file is generated with the FMS data formatter using the parsed external data file and sent to the FMS on the aircraft.

System and method for platform agonistic flight management data access

Disclosed are methods, systems, and one or more computer-readable mediums for performing, by one or more processors located off-board a vehicle, operations including receiving, by the fog based application framework before transit of the vehicle, vehicle operation data from a cloud based database of a cloud based computing system; receiving, by the fog based application framework before and/or in real-time during transit of the vehicle, edge-based vehicle data from one or more edge computing devices of the vehicle; and generating, by the fog based application framework during transit of the vehicle, a plurality of vehicle operation insights based on the vehicle operation data and the edge-based vehicle data.

Systems and methods for a vehicle processing system with a fog-based framework

A system includes avionics line-replaceable units (LRUs); a mission manager including application programming interfaces (API); a processing device; and a memory storing one or more machine readable instructions causing the system to: communicatively couple the mission manager to external avionics services via a data gateway to receive updated mission conditions at the mission manager; register one of the avionics LRUs with one of the mission manager APIs; receive, at the mission manager, updated mission conditions from the external avionics services via the data gateway; provide one or more of the one or more updated mission conditions to the registered avionics LRU based on one or more of an updated mission plan and an unexpected update to the mission condition; and control one or more aircraft systems based on one or more of the updated mission plan and the unexpected update to the mission condition.

Systems and methods for self-contained mission management

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.

System and method for generating configurable optical codes for transferring avionics data

A system for an aircraft configured to: provide one or more of the sensed aircraft characteristics to a flight planning tool for processing by one or more features of the flight planning tool; receive a recommended flight setting from the flight planning tool based on the processing by the flight planning tool; compare a current flight setting as determined based on the one or more sensed aircraft characteristics from the plurality of sensors with the received recommended flight setting; determine a potential operational efficiency based on the comparison between the received recommended flight setting and the current flight setting; and provide the potential operational efficiency to a user based on an identity of the user.

Integrated flight deck

Disclosed are systems, methods, and non-transitory computer-readable medium for providing a safe landing for an aerial vehicle. The method may include: displaying, on one or more displays, an aerial vehicle, an intended landing zone, and a real-time flight path of the vehicle as the vehicle approaches the intended landing zone; receiving data related to one or more of the vehicle, the flight path of the vehicle, the intended landing zone, and an obstacle; determining the proximity of the vehicle relative to the center of the intended landing zone based on the received data; displaying the proximity of the vehicle relative to the center of the intended landing zone; displaying the obstacle when present; displaying an alert when the vehicle deviates in proximity to the center of the intended landing zone and/or approaches the obstacle; and upon determining a failure to respond to the alert computing flight controls to modify landing.

Systems and methods for providing safe landing assistance for an aerial vehicle

Display screen with graphical user interface

Various embodiments described herein relate to performance assurance modeling for a portfolio of assets. In this regard, a request to generate one or more performance assurance insights related to one or more assets is received. The request includes a fault descriptor describing one or more faults associated with the one or more assets. In response to the request, a first risk level associated with the one or more faults is determined based on the fault descriptor and asset data associated with the one or more assets. Additionally, in response to the request, a second risk level associated with the one or more faults is generated based on one or more predetermined relationships between faults and asset performance indicator thresholds. The one or more performance assurance insights are then generated based on a comparison between the first risk level and the second risk level.

Performance metric assurance for asset management

Systems and methods for coordinating with a flight management system (FMS) on-board an aircraft to determine whether a flight plan (FP) change generated by an external device is valid. The method includes generating the FP change, which includes a deviation to the intended FP and a savings parameter associated with a parameter of the intended FP, responsive to weather data and aircraft state data; generating a lateral display showing the intended FP and an alphanumeric window with the FP change; transmitting the FP change to the FMS; receiving, from the FMS, a travel path and a calculated parameter for the travel path, generated by the FMS responsive to the FP change; determining whether the travel path realizes the savings parameter by comparing the calculated parameter to the savings parameter; and, displaying either a selectable graphical user interface (GUI) object to implement the FP change, or a warning based thereon.

Systems and methods to corroborate an externally recommended flight plan change with flight management system

Growing community of inventors

Karnataka, India

Kalimulla Khan