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公开(公告)号:US20190012921A1
公开(公告)日:2019-01-10
申请号:US15644501
申请日:2017-07-07
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor: Mark Pearson , Susan McCullough , Phillip Toews , Todd Wisner , Charles Dairman
IPC: G08G5/00
Abstract: Aircraft systems and related methods are provided for extensible flight management capabilities. One exemplary system includes a multifunction computing module including a user interface, a first processing system, and a first communications interface supporting a first data characteristic, and a flight management computing module. The flight management computing module includes at least one avionics interface to receive operational data from an avionics system onboard an aircraft and having a second data characteristic different from the first data characteristic, a second communications interface communicatively coupled to the first communications interface to the multifunction computing module, and a second processing system coupled to the avionics interface and the second communications interface to convert the operational data to input data having the first data characteristic and provide the input data to the multifunction computing module.
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公开(公告)号:US10957206B2
公开(公告)日:2021-03-23
申请号:US15787077
申请日:2017-10-18
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor: Susan McCullough , Mahesh Sivaratri , Raghu Shamasundar , Kalimulla Khan , Srihari Jayathirtha , Sushma Bidrupane , Mark Pearson , Todd Wisner
IPC: G05D1/10 , G08G5/00 , G06F16/951
Abstract: 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.
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公开(公告)号:US20190114927A1
公开(公告)日:2019-04-18
申请号:US15787077
申请日:2017-10-18
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor: Susan McCullough , Mahesh Sivaratri , Raghu Shamasundar , Kalimulla Khan , Srihari Jayathirtha , Sushma Bidrupane , Mark Pearson , Todd Wisner
Abstract: 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.
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公开(公告)号:US11762543B2
公开(公告)日:2023-09-19
申请号:US16697968
申请日:2019-11-27
Applicant: Honeywell International Inc.
Inventor: Steven Smith , Susan McCullough , David McGloughlin
IPC: G06F3/04847
CPC classification number: G06F3/04847
Abstract: 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.
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公开(公告)号:US20200372813A1
公开(公告)日:2020-11-26
申请号:US16417235
申请日:2019-05-20
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor: Steven L. Smith , Susan McCullough , Keshav Rao
IPC: G08G5/00
Abstract: Methods and systems are provided for recovering flight plan data for a bypassed segment of a flight plan aircraft. The method comprises loading an initial flight plan onto a Flight Management System (FMS) that is located on board the aircraft. The active flight plan includes multiple waypoints located along the active flight plan. A modified flight plan is created and executed that bypasses at least one of the waypoints located along the initial flight plan. The bypassed flight data is stored in the memory of the FMS. A restored flight plan is created later by retrieving the bypassed flight data from the FMS memory and loaded onto the FMS. The restored flight plan is then executed by the FMS.
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6.
公开(公告)号:US10131444B1
公开(公告)日:2018-11-20
申请号:US15689171
申请日:2017-08-29
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor: Philip Toews , Todd Wisner , Mark Pearson , Susan McCullough
IPC: B64D43/00 , G06F3/0488 , G06F3/041 , G06F3/0482
Abstract: 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.
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