Honeywell International Inc.

Rakshit R

Thea Lynn Feyereisen

Gang He

Pavan Kumar Desai

Pramod Kumar Malviya

Emmanuel Letsu-Dake

Zuowei He

Brock Graham

Atmacharan Ajjavara

Bincicil Mathew

Roshini Mehboob

Methods and systems are provided for propagating a free-form user input across different displays. One method involves receiving a free-form user input on a navigational map display, assigning a geographic location to the free-form user input based on a position of the free-form user input on the navigational map display, and generating a graphical indication influenced by the free-form user input on a second display at a respective position on the second display corresponding to the geographic location assigned to the free-form user input.

Methods and systems for propagating user inputs to different displays

A controller for selectively displaying information from raster charts is disclosed. The controller is configured to: retrieve raster data; assign a different priority level to each of a plurality of types of raster data; cause raster data having a predetermined priority level to be displayed with first augmentation information and prevent from being displayed raster data not having the first predetermined priority level, wherein the first augmentation information comprises database data retrieved from a database and is assigned a first predetermined augmentation information priority level; generate a hidden layer of second augmentation information comprising database data from the database that is correlated to a geographical location of the displayed raster data and assigned a second predetermined augmentation information priority level; and cause the hidden layer of second augmentation information to be displayed over a portion of the displayed raster data when the geographical location is selected.

System and method for dynamically augmenting raster charts displayed on a cockpit display

Methods and systems for low visibility surface movement guidance for an aircraft navigating an airport environment. The system includes an avionic display module on an aircraft, configured to receive ownship data and generate an avionic display on a display device, and to respond to display commands. The system also includes a low voltage (LV) conditions module, configured to: receive weather data and determine when low voltage LV conditions are occurring; and, responsive to determining that LV conditions are occurring, (i) generate display commands to reconfigure the avionic display to present the LVO plan, rendered in accordance with a preprogrammed visualization scheme for rendering LV features in the LVO plan, and (ii) calculate an optimized taxi route for the aircraft to a target airport point of interest, as a function of the LVO plan. The system generates display commands to render the optimized taxi route on the reconfigured avionic display.

Systems and methods for low visibility guidance and taxi routing

Methods and systems are provided for resolving a selected graphical element corresponding to a tactile user input associated with a graphical user interface display on a display device associated with a vehicle, such as an aircraft. The tactile user input is classified based on its temporal duration, and the classification of the tactile user input influences the identification of the selected graphical element or other response to the tactile user input.

Methods and systems for resolving tactile user input selections

Methods and systems are provided for guiding or otherwise assisting operation of an aircraft when diverting from a flight plan. One method involves determining a gliding trajectory for the aircraft based at least in part on a current altitude of the aircraft, providing a graphical representation of the gliding trajectory for the aircraft, identifying a plurality of landing locations within a range defined by the gliding trajectory from the aircraft, and for each landing location of the plurality of landing locations, providing a graphical representation of a respective landing location with respect to the gliding trajectory at a respective altitude associated with the respective landing location and at a respective distance with respect to a graphical representation of the aircraft corresponding to a respective geographic distance between a current location of the aircraft and the respective landing location.

Composite vertical profile display systems and methods

Methods and systems are provided for generating a user and phase of flight dependent cockpit display. The methods and systems generate a display for a display device using display settings included in a user profile and a current phase of flight. The display settings include preferences defining a range of a map to be displayed that are different for different phases of flight, and preferences defining a level of declutter of a map to be displayed that are different for different phases of flight.

Growing community of inventors

Bengaluru, India

Rakshit R