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    METHOD AND SYSTEM FOR INTEGRATING OFFBOARD GENERATED PARAMETERS INTO A FLIGHT MANAGEMENT SYSTEM
    13.
    发明申请
    METHOD AND SYSTEM FOR INTEGRATING OFFBOARD GENERATED PARAMETERS INTO A FLIGHT MANAGEMENT SYSTEM 审中-公开

    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.

    METHODS AND APPARATUS FOR DISPLAYING FLIGHT INTERVAL MANAGEMENT DATA FOR SELECTING APPROPRIATE FLIGHT MANAGEMENT SETTINGS
    14.
    发明申请
    METHODS AND APPARATUS FOR DISPLAYING FLIGHT INTERVAL MANAGEMENT DATA FOR SELECTING APPROPRIATE FLIGHT MANAGEMENT SETTINGS 审中-公开

    公开(公告)号：US20190049268A1

    公开(公告)日：2019-02-14

    申请号：US15675256

    申请日：2017-08-11

    Applicant: HONEYWELL INTERNATIONAL INC.

    Inventor： Rajeev Mohan ,  Ravish Udupa ,  Ruben Carrillo ,  Shashi Kumar Namde

    IPC: G01C23/00 ,  B64D43/00 ,  G08G5/00

    Abstract: A method and system for aircraft management for selecting a speeding profile mode for phases of a flight plan including: retrieving assigned space goals (ASG) corresponding to a plurality of achieve by point (ABP) designations for a target flight path of the aircraft wherein the target flight path is associated with a target aircraft; determining a target air speed and applicable speed profile modes by retrieving prior information of traffic history and flight plans of the target aircraft to achieve the ABP designations corresponding to an ASG retrieved; selecting from a plurality of applicable speed profile modes, at least one applicable speed profile mode for a phase of the target flight plan for the aircraft; and comparing statuses of the aircraft of at least a status of fuel remaining for a combination of the selection of the applicable speed profile mode and the phase of the target flight plan.

    Systems and methods for cognitive services of a connected FMS or avionics SaaS platform
    17.
    发明授权
    Systems and methods for cognitive services of a connected FMS or avionics SaaS platform 有权

    公开(公告)号：US11488063B2

    公开(公告)日：2022-11-01

    申请号：US16805101

    申请日：2020-02-28

    Applicant: Honeywell International Inc.

    Inventor： Kirupakar Janakiraman ,  Rajeev Mohan ,  Ramkumar Rajendran

    IPC: G06N20/00 ,  B64D43/00 ,  G06N7/00

    Abstract: Disclosed are methods, systems, and non-transitory computer-readable medium for cognitive services for a FMS SaaS platform. For instance, the method may include obtaining training data; training reinforcement learning model(s) using the obtained training data; in response to receiving a request for cognitive services from a user device, analyzing a query of the request for cognitive services using at least one reinforcement learning model of the trained reinforcement learning model(s); determining intent, entity(s), emotion, and/or context of the query based on an output of the at least one reinforcement learning model to form a cognitive services request; applying a second at least one reinforcement learning model of the trained reinforcement learning model(s) to the cognitive services request to determine one or more services to invoke; and transmitting a result to the user device based on an output of the one of more invoked services.

    SYSTEMS AND METHODS FOR IDENTIFYING A NUMBER OF FEASIBLE TARGET TRAFFIC FOR A PAIRED APPROACH
    18.
    发明申请
    SYSTEMS AND METHODS FOR IDENTIFYING A NUMBER OF FEASIBLE TARGET TRAFFIC FOR A PAIRED APPROACH 有权

    公开(公告)号：US20220066479A1

    公开(公告)日：2022-03-03

    申请号：US17065683

    申请日：2020-10-08

    Applicant: HONEYWELL INTERNATIONAL INC.

    Inventor： Rajeev Mohan ,  Ravish Udupa ,  Ruben Carrillo ,  Bhalakrishnan Janardhanan

    IPC: G05D1/10 ,  G06F3/0481 ,  G08G5/00 ,  B64D43/00

    Abstract: Methods and systems for an aircraft entering a terminal radar approach control (TRACON) airspace to identify a number of feasible target traffic for a paired approach for the aircraft. Traffic data is filtered to identify a plurality of neighbor traffic that are entering the TRACON airspace or within the TRACON airspace when the aircraft is entering the TRACON airspace and estimating, concurrently, for each neighbor traffic of the plurality of neighbor traffic: a trajectory, a traffic arrival time at an ideal location for a respective paired approach with the aircraft, a spacing interval between the neighbor traffic and the aircraft for the respective paired approach, and a respective target location for the aircraft to begin the respective paired approach, as a function of the spacing interval. Based on the estimations, the method identifies feasible, marginally feasible, and infeasible targets, and displays this information in an intuitive lateral display.

    Systems and methods for fault injection and ensuring failsafe FMS SaaS platforms
    19.
    发明授权
    Systems and methods for fault injection and ensuring failsafe FMS SaaS platforms 有权

    公开(公告)号：US11204861B2

    公开(公告)日：2021-12-21

    申请号：US16804970

    申请日：2020-02-28

    Applicant: HONEYWELL INTERNATIONAL INC.

    Inventor： Rajeev Mohan ,  Ramkumar Rajendran ,  Kirupakar Janakiraman

    IPC: G06F9/44 ,  G06F11/36

    Abstract: Disclosed are methods, systems, and non-transitory computer-readable medium for fault injection and ensuring failsafe FMS SaaS platforms. For instance, the method may include observing a behavior of a platform; building a hypothesis about a steady state behavior based on the observing the behavior of the platform; determining whether a request for fault injection has been received; in response to receiving the request for the fault injection, performing the fault injection; observing a response of the platform to the fault injection; determining whether the fault injection is at an end; and in response to determining that the fault injection is at the end, collect and analyze data of observed response(s).

    SYSTEM AND METHODS ENABLING AIRCRAFT ENERGY DISSIPATION FOR RAPID DECISION MAKING
    20.
    发明申请
    SYSTEM AND METHODS ENABLING AIRCRAFT ENERGY DISSIPATION FOR RAPID DECISION MAKING 有权

    公开(公告)号：US20210319708A1

    公开(公告)日：2021-10-14

    申请号：US16890614

    申请日：2020-06-02

    Applicant: HONEYWELL INTERNATIONAL INC.

    Inventor： Rajesh Chaubey ,  Rajeev Mohan ,  Daniel E. Lewis

    IPC: G08G5/02 ,  G06F3/0482 ,  B64D43/02

    Abstract: A method in an aircraft for energy reduction is disclosed. The method includes: determining a starting point location, altitude and airspeed for a stable approach for landing at a diversion airport; and determining a vertical strategy for achieving the starting point altitude and airspeed by identifying a region of opportunity for adjusting the speed and altitude and identifying a plurality of energy reduction strategies for achieving the starting point altitude and airspeed while in the region of opportunity based on a speed mode during the stable approach. The method further comprises causing a graphic display to be displayed that lists for selection each of the plurality of identified strategies, detailed maneuver information for strategy implementation, and costs for implementing each identified strategy; and causing to be displayed, responsive to flight crew selection, a lateral view and vertical view of a proposed trajectory based on a selected identified strategy.

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