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    Display systems and methods
    1.
    发明授权
    Display systems and methods 有权

    公开(公告)号：US12033528B2

    公开(公告)日：2024-07-09

    申请号：US17167861

    申请日：2021-02-04

    Applicant: HONEYWELL INTERNATIONAL INC.

    Inventor： John G. Suddreth ,  Jerry Ball ,  Kenneth Leiphon

    IPC: G06K9/00 ,  B60R11/04 ,  G08G5/06

    CPC classification number: G08G5/065 ,  B60R11/04 ,  B60R2300/105 ,  B60R2300/302 ,  B60R2300/303 ,  B60R2300/607 ,  B60R2300/806

    Abstract: An image processing system for generating a display for a vehicle. The image processing system receives images, respectively, from a plurality of cameras mounted on the vehicle. The field of view of the plurality of cameras at least partially overlaps. The field of view of one or more of the plurality of cameras includes a region underneath the vehicle. The images are transformed to a common reference plane using a perspective transformation algorithm and based on intrinsic and extrinsic parameters of the plurality of cameras, to thereby obtain a projected image. The projected image is projected to the common reference plane. A display is generated based on the projected image. The display includes a synthetic depiction of the vehicle including an outer profile. The display includes an image area within the outer profile that is based on the projected image for the region underneath the vehicle.

    SYSTEMS AND METHODS FOR GENERATING AVIONIC DISPLAYS INCLUDING FORECAST OVERPRESSURE EVENT SYMBOLOGY
    2.
    发明申请
    SYSTEMS AND METHODS FOR GENERATING AVIONIC DISPLAYS INCLUDING FORECAST OVERPRESSURE EVENT SYMBOLOGY 审中-公开

    公开(公告)号：US20200033185A1

    公开(公告)日：2020-01-30

    申请号：US16580626

    申请日：2019-09-24

    Applicant: HONEYWELL INTERNATIONAL INC.

    Inventor： John G. Suddreth ,  Marisela Mendez Tapia ,  Jerry Ball ,  Mark Giddings

    IPC: G01H1/00 ,  G01C23/00 ,  G08G5/00 ,  B64D43/00 ,  B64D45/00 ,  G01H17/00 ,  G01H5/00 ,  B64C30/00

    Abstract: Avionic display systems and methods are provided for generating avionic displays, which include symbology and other graphics pertaining to forecast overpressure events, which are forecast to occur during supersonic aircraft flight. In various embodiments, the avionic display system includes a display device on which an avionic display is produced. A controller architecture is operably coupled to the display device. Storage media contains computer-readable code or instructions that, when executed by the controller architecture, cause the avionic display system to determine whether an overpressure event is forecast to occur due to the predicted future occurrence of a sonic boom, which has a magnitude exceeding a boom tolerance threshold. When the controller architecture determines that an overpressure event is forecast to occur, the avionic display system further generates symbology on the avionic display indicative of or visually signifying the forecast overpressure event.

    SYSTEMS AND METHODS FOR GENERATING AVIONIC DISPLAYS INCLUDING FORECAST BOOM TOLERANCE THRESHOLD EXCEEDANCE SYMBOLOGY
    3.
    发明申请
    SYSTEMS AND METHODS FOR GENERATING AVIONIC DISPLAYS INCLUDING FORECAST BOOM TOLERANCE THRESHOLD EXCEEDANCE SYMBOLOGY 审中-公开

    公开(公告)号：US20190164436A1

    公开(公告)日：2019-05-30

    申请号：US15825916

    申请日：2017-11-29

    Applicant: HONEYWELL INTERNATIONAL INC.

    Inventor： John G. Suddreth ,  Jerry Ball

    IPC: G08G5/00 ,  G06F17/50

    Abstract: Avionic display systems and methods are provided for generating avionic displays including symbology decreasing the likelihood of boom tolerance threshold exceedance (an overpressure events) due to potential constructive interference between pressure waves occurring during supersonic flight. In various embodiments, the avionic display system includes a display device on which an avionic display is generated. A controller architecture is operably coupled to the display device and configured to determine when there exists a possibility for an overpressure event to occur in a future timeframe due to constructive interference between colliding pressure waves, which are forecast to occur during the impending supersonic flight of one or more A/C. When determining that there exists a possibility for an overpressure event to occur in the future timeframe due to constructive interference between pressure waves, the controller architecture further generates symbology or other graphics on the avionic display indicative of the potential occurrence of the overpressure event.

    Systems and methods for generating avionic displays including forecast boom tolerance threshold exceedance symbology
    4.
    发明授权
    Systems and methods for generating avionic displays including forecast boom tolerance threshold exceedance symbology 有权

    公开(公告)号：US10810886B2

    公开(公告)日：2020-10-20

    申请号：US15825916

    申请日：2017-11-29

    Applicant: HONEYWELL INTERNATIONAL INC.

    Inventor： John G. Suddreth ,  Jerry Ball

    IPC: G01C23/00 ,  G08G5/00 ,  B64D43/00 ,  B64D45/00 ,  G06F30/15 ,  B64C23/04 ,  B64C30/00 ,  G06F119/10

    Abstract: Avionic display systems and methods are provided for generating avionic displays including symbology decreasing the likelihood of boom tolerance threshold exceedance (an overpressure events) due to potential constructive interference between pressure waves occurring during supersonic flight. In various embodiments, the avionic display system includes a display device on which an avionic display is generated. A controller architecture is operably coupled to the display device and configured to determine when there exists a possibility for an overpressure event to occur in a future timeframe due to constructive interference between colliding pressure waves, which are forecast to occur during the impending supersonic flight of one or more A/C. When determining that there exists a possibility for an overpressure event to occur in the future timeframe due to constructive interference between pressure waves, the controller architecture further generates symbology or other graphics on the avionic display indicative of the potential occurrence of the overpressure event.

    Systems and methods for generating avionic displays including forecast overpressure event symbology
    5.
    发明授权
    Systems and methods for generating avionic displays including forecast overpressure event symbology 有权

    公开(公告)号：US10720064B2

    公开(公告)日：2020-07-21

    申请号：US16235923

    申请日：2018-12-28

    Applicant: HONEYWELL INTERNATIONAL INC.

    Inventor： John G. Suddreth ,  Marisela Mendez Tapia ,  Jerry Ball ,  Mark Giddings

    IPC: G08G5/00 ,  G01H1/00 ,  G01H5/00 ,  B64C30/00 ,  G01H17/00

    Abstract: Avionic display systems and methods are provided for generating avionic displays, which include symbology and other graphics pertaining to forecast overpressure events, which are forecast to occur during supersonic aircraft flight. In various embodiments, the avionic display system includes a display device on which an avionic display is produced. A controller architecture is operably coupled to the display device. Storage media contains computer-readable code or instructions that, when executed by the controller architecture, cause the avionic display system to determine whether an overpressure event is forecast to occur due to the predicted future occurrence of a sonic boom, which has a magnitude exceeding a boom tolerance threshold. When the controller architecture determines that an overpressure event is forecast to occur, the avionic display system further generates symbology on the avionic display indicative of or visually signifying the forecast overpressure event.

    Systems and methods for sonic boom aware flight planning
    8.
    发明授权
    Systems and methods for sonic boom aware flight planning 有权

    公开(公告)号：US10699584B2

    公开(公告)日：2020-06-30

    申请号：US15910072

    申请日：2018-03-02

    Applicant: HONEYWELL INTERNATIONAL INC.

    Inventor： John G. Suddreth ,  Jerry Ball ,  Troy Nichols ,  Mark A. Giddings

    IPC: G08G5/00 ,  G01C23/00 ,  B64C30/00

    Abstract: Flight planning systems and methods are provided, which augment supersonic flight planning via the integration of sonic boom forecast data. In embodiments, the flight planning system includes a display device, a pilot input interface, and a controller architecture coupled to the display device and to the pilot input interface. During system operation, the controller architecture receives flight plan criteria entered via the pilot input interface. The controller architecture then endeavors to generate or construct a boom-regulated flight plan, which includes at least one supersonic flight plan segment, in accordance with the flight plan criteria. If unable to construct a boom-regulated flight plan, the controller architecture generates a visual notification on the display device. The visual notification can include, for example, a warning that an excessive sonic boom or overpressure event may occur during execution of the flight plan by an aircraft, absent modifications to the flight plan.

    Systems and methods for generating avionic displays including forecast overpressure event symbology
    9.
    发明授权
    Systems and methods for generating avionic displays including forecast overpressure event symbology 有权

    公开(公告)号：US10209122B1

    公开(公告)日：2019-02-19

    申请号：US15798692

    申请日：2017-10-31

    Applicant: HONEYWELL INTERNATIONAL INC.

    Inventor： John G. Suddreth ,  Marisela Mendez Tapia ,  Jerry Ball ,  Mark Giddings

    IPC: G01H1/00 ,  G08G5/00 ,  G01H5/00 ,  B64C30/00

    Abstract: Avionic display systems and methods are provided for generating avionic displays, which include symbology and other graphics pertaining to forecast overpressure events, which are forecast to occur during supersonic aircraft flight. In various embodiments, the avionic display system includes a display device on which an avionic display is produced. A controller architecture is operably coupled to the display device. Storage media contains computer-readable code or instructions that, when executed by the controller architecture, cause the avionic display system to determine whether an overpressure event is forecast to occur due to the predicted future occurrence of a sonic boom, which has a magnitude exceeding a boom tolerance threshold. When the controller architecture determines that an overpressure event is forecast to occur, the avionic display system further generates symbology on the avionic display indicative of or visually signifying the forecast overpressure event.

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