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    SYSTEMS, APPARATUSES, METHODS, AND COMPUTER PROGRAM PRODUCTS FOR A STABILIZED VEHICLE RELATED INTERFACE COMPONENT
    21.
    发明申请
    SYSTEMS, APPARATUSES, METHODS, AND COMPUTER PROGRAM PRODUCTS FOR A STABILIZED VEHICLE RELATED INTERFACE COMPONENT 有权

    公开(公告)号：US20250138847A1

    公开(公告)日：2025-05-01

    申请号：US18921880

    申请日：2024-10-21

    Applicant: Honeywell International Inc.

    Inventor： Kenneth M Leiphon ,  Kirupakar J ,  Kalimulla Khan ,  Ramkumar Rajendran

    IPC: G06F9/451 ,  G02B27/00 ,  G02B27/01 ,  G06F3/01 ,  G06F3/04845

    Abstract: Systems, apparatuses, methods, and computer program products are provided herein. For example, a method may include receiving, from a wearable device, head motion data. In some embodiments, the method includes generating eye motion data by applying the head motion data to an eye motion determination model. In some embodiments, the method includes detecting device motion data associated with a device. In some embodiments, the method includes generating vehicle related stabilization data by applying the eye motion data and the device motion data to a vehicle related stabilization model. In some embodiments, the method includes generating a stabilized vehicle related interface component based on the vehicle related stabilization data and vehicle related device display data. In some embodiments, the method includes causing the stabilized vehicle related interface component to be rendered to an interface of the device.

    SYSTEMS, APPARATUSES, METHODS, AND COMPUTER PROGRAM PRODUCTS FOR A STABILIZED AVIATION OPERATIONS INTERFACE COMPONENT
    22.
    发明申请
    SYSTEMS, APPARATUSES, METHODS, AND COMPUTER PROGRAM PRODUCTS FOR A STABILIZED AVIATION OPERATIONS INTERFACE COMPONENT 有权

    公开(公告)号：US20250138714A1

    公开(公告)日：2025-05-01

    申请号：US18921887

    申请日：2024-10-21

    Applicant: Honeywell International Inc.

    Inventor： Kalimulla Khan ,  Kirupakar J ,  Kenneth M. Leiphon ,  Mythili Belle Kamath ,  Ramkumar Rajendran

    IPC: G06F3/04845 ,  B64D45/00

    Abstract: Systems, apparatuses, methods, and computer program products are provided herein. For example, a method may include receiving aviation operations display data associated with an aircraft. In some embodiments, the method includes capturing aviation operations impact data using one or more aircraft components of the aircraft. In some embodiments, the aviation operations impact data is indicative of an aviation instability event. In some embodiments, the method includes generating aviation stability adjustment data by applying the aviation operations impact data to an aviation stability adjustment model. In some embodiments, the method includes generating a stabilized aviation operations interface component based on the aviation stability adjustment data and the aviation operations display data. In some embodiments, the method includes causing the stabilized aviation operations interface component to be rendered to an aviation operations interface of a device.

    INTELLIGENT SOFTWARE DEVELOPMENT KIT FRAMEWORK FOR ADVANCED MOTION STABILIZATION
    23.
    发明申请
    INTELLIGENT SOFTWARE DEVELOPMENT KIT FRAMEWORK FOR ADVANCED MOTION STABILIZATION 有权

    公开(公告)号：US20250138629A1

    公开(公告)日：2025-05-01

    申请号：US18922093

    申请日：2024-10-21

    Applicant: Honeywell International Inc.

    Inventor： Kirupakar J ,  Kalimulla Khan ,  Ramkumar Rajendran ,  Kenneth M. Leiphon ,  Mythili Belle Kamath

    IPC: G06F3/01 ,  B60K35/28 ,  B60K35/29 ,  G06F3/14 ,  G06F9/54

    Abstract: Embodiments of the present disclosure provide motion stabilization software development kit and framework. An example motion stabilization software development kit may include a hardware layer that includes a first set of one or more sensors configured for generating device motion data for a display device within a vehicle and a second set of one or more sensors configured for generating vehicle motion data for the vehicle. The example motion stabilization software development kit may include an API layer that includes one or more APIs and an application layer that includes one or more applications communicatively coupled to the first and second set of one or more sensors. The example motion stabilization software development kit may include a software development kit abstraction layer that includes a motion stabilization model configured to adjust a position of an object on a screen of the display device.

    FLIGHT SAFETY OPERATIONS OPTIMIZATION
    24.
    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
    26.
    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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