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    Systems and methods for cognitive services of a connected FMS or avionics SaaS platform
    11.
    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 fault injection and ensuring failsafe FMS SaaS platforms
    12.
    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 METHOD FOR PROVIDING ENHANCED SERVICES
    13.
    发明申请
    SYSTEM AND METHOD FOR PROVIDING ENHANCED SERVICES 有权

    公开(公告)号：US20220382299A1

    公开(公告)日：2022-12-01

    申请号：US17660889

    申请日：2022-04-27

    Applicant: HONEYWELL INTERNATIONAL INC.

    Inventor： Raghu Shamasundar ,  Subhransu Sahoo ,  Richard Snyder ,  Kalimulla Khan ,  Ramkumar Rajendran

    IPC: G05D1/10 ,  G08G5/00 ,  G01C21/20

    Abstract: 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.

    FLIGHT SAFETY OPERATIONS OPTIMIZATION
    16.
    发明申请
    FLIGHT SAFETY OPERATIONS OPTIMIZATION 有权

    公开(公告)号：US20250091730A1

    公开(公告)日：2025-03-20

    申请号：US18818803

    申请日：2024-08-29

    Applicant: Honeywell International Inc.

    Inventor： Kirupakar J ,  Kalimulla Khan ,  Ramkumar Rajendran ,  Shirish Katti ,  Mahima Banerjee ,  Rohit Pandita ,  Jyothsna Peram

    IPC: B64F5/60 ,  G06N20/00 ,  G07C5/08

    Abstract: Techniques for optimizing flight safety operations for an aircraft are described. In operation, aircraft operational parameters corresponding to a plurality of flight operations are retrieved. The aircraft operational parameters are then analyzed using a first machine learning model to identify a first flight operation, where the first flight operation comprises at least one aircraft operational parameter with deviation beyond a threshold. At least one potential flight safety incident corresponding to the first flight operation is then identified using the at least one aircraft operational parameter. The at least one potential flight safety incident is then analyzed using a second machine learning model to identify a corrective action for the potential flight safety incident, where the second machine learning model is trained using flight safety artifacts comprising a plurality of flight safety incidents and corrective actions to be initiated in response to the plurality of flight safety incidents. The corrective action is then subjected to an avionics digital twin to ascertain that the corrective action mitigates the at least one potential flight safety incident. The corrective action is then recommended for the at least one potential flight safety incident.

    Display screen with graphical user interface
    18.
    外观设计
    Display screen with graphical user interface 有权

    公开(公告)号：USD1033458S1

    公开(公告)日：2024-07-02

    申请号：US29864211

    申请日：2022-05-13

    Applicant: Honeywell International Inc.

    Designer： Kalimulla Khan ,  Kirupakar Janakiraman ,  Ramkumar Rajendran ,  Ryan Weeks ,  Phillip Toews

    Abstract: FIG. 1 is a front view of a graphical user interface for a display screen or portion thereof showing our new design;
    FIG. 2 is a front view of a second embodiment thereof; and,
    FIG. 3 is a front view of a third embodiment thereof.
    The outer broken line perimeter showing the display screen and the broken lines within showing text and elements of the graphical user interface are provided for the purpose of illustrating portions of the article and form no part of the claimed design. The sections of the graphical user interface that have shading form a part of the claimed design and the shading in the figures forms part of the claimed design as shown.

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