Honeywell International Inc.

Susan L McCullough

Mark Pearson

Todd Wisner

Raghu Shamasundar

Kalimulla Khan

William Ray Hancock

Srihari Jayathirtha

Mahesh Sivaratri

Philip Toews

Paul A Fisher

Dave Bibby

David McGloughlin

Sushma Bidrupane

Steven L Smith

Disclosed are methods, systems, and non-transitory computer-readable medium for managing vehicle guidance using a GUI. One method may include: obtaining flight management system (FMS) data; updating an aircraft configuration state based on the FMS data; obtaining a current mode, active command, and a second command for a guidance panel based on the configuration state; and generating a guidance panel GUI based on the current mode, the active command, and the second command. Another method may include: obtaining vehicle data; updating a vehicle configuration state based on the vehicle data if the vehicle data has updated information; obtaining a current mode, active command, and a second command for a guidance panel of the vehicle based on the vehicle configuration state; generating a guidance panel GUI based on the current mode, the active command, and the second command; and displaying the guidance panel GUI on the guidance panel.

Systems and methods for managing graphical user interfaces for vehicle guidance

A system for integrating flight crew decision aid applications in an aircraft cockpit includes a touch screen controller (TSC) that comprises a data mining engine configured to mine aircraft data from the already existing avionics interface and a flight plan and trajectory generating engine (FPTGE) configured to retrieve a trajectory request from a requesting flight crew decision aid application, compute one or more theoretical trajectories using the mined aircraft data, and transmit the one or more theoretical trajectories to the requesting flight crew decision aid application. The TSC also comprises a flight crew decision aid application configured to receive a flight crew request for simulated data from a touch screen user interface, generate and transmit one or more requested trajectory requests to the FPTGE, receive data from the one or more theoretical trajectories from the FPTGE, and display the requested simulated data on the touch screen user interface.

System and method for integration of smart trajectory generation and decision aid applications in legacy cockpits

A keyboard module configured for use in an avionics touchscreen system is disclosed. The keyboard module is configured to display, via a visual display in the avionics touchscreen system and responsive to a selection of an application program generated widget for focus via a touchscreen surface in the avionics touchscreen system, a virtual keyboard. The virtual keyboard includes a text box widget configured to display clip data stored in clipboard memory provided by the avionics touchscreen system, a copy widget configured to cause data in a first widget provided by the application program that is in focus to be copied to the clipboard memory, and a paste widget configured to cause the clip data in the clipboard memory and displayed in the text box widget to be pasted to a second widget provided by the application program that is in focus.

System and method of providing clipboard cut and paste operations in an avionics touchscreen system

An aircraft system includes a visual display system; a printer; and a flight management system coupled to the visual display system and the printer. The flight management system includes a processor and a plurality of data sources coupled to the processor. The processor includes a crew interface module coupled to the plurality of data sources, a display driver coupled to the crew interface module and the visual display system, and a printer driver coupled to the crew interface module and the printer. The crew interface module is configured to generate a report from data from the data sources and to send the report to the visual display system via the display driver. The visual display system is configured to receive the report and to display the report.

Aircraft systems with flight management systems that display reports

A visual display system includes a monitor for displaying a visual display; a memory having a user application definition file containing information related to the visual display; and a processor coupled to the monitor and the memory, the processor configured to receive runtime parameters from a flight management system and provide the visual display to the monitor based on the runtime parameters and the user application definition file. The visual display includes at least one hotkey.

Visual display system for an aircraft

A rendering technique for generating a three dimensional (3D) image is provided. The technique includes the steps of collecting 3D data, writing the 3D data into texture memory as two dimensional (2D) slices, and texturizing a first set of overlapping polygons utilizing the 2D slices. The technique further includes the step of displaying the first set of overlapping texturized polygons to produce a 3D image.

Method and aircraft display system for generating three dimensional image

A radar display system ( ) according to the present invention generates textured radar display data by utilizing a direct memory access receiver ( ) to receive radially scanned radar data, to convert the radially scanned radar data into range bin data sets, and to store the range bin data sets. A graphics renderer ( ) stores the set of range bin data sets in a texture memory ( ) as a plurality of rectangular textures, and bit maps the rectangular textures to a series of display triangles in a frame buffer ( ). The graphics renderer ( ) colors the display triangles in accordance with the rectangular textures by performing a bi-linear interpolation of the color and warps the display triangles in accordance with the size of a display ( ).

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Glendale, AZ, United States of America

Susan L McCullough