Abstract: Disclosed are methods, systems, and non-transitory computer-readable medium for managing configurations of multiple vehicle displays. For instance, a method may include: obtaining a configurable file for an electronic checklist; generating a graphical user interface (GUI) based on the configurable file; displaying the GUI on one of the multiple vehicle displays; receiving a user input on the GUI; and performing a window configuration setting process based on the user input. The method may also include: in response to the user input being a first user input type in a region associated with a context menu indicator: obtaining a window configuration function and a phase of flight variable; generating a context menu based on the window configuration function and the POF variable; and displaying the context menu on the GUI.

Abstract: A method of displaying information is provided. The method comprises: displaying, on a GUI page that displays a primary function, a plurality of top-level graphical control elements in a row on the GUI page; displaying, on the GUI page responsive to selection of one of the top-level graphical control elements, one or more second-level graphical control elements adjacent to the selected top-level graphical control element and an outline that encompasses the selected top-level graphical control element and the one or more second-level graphical control elements; receiving data entry for affecting the state of a system parameter via a graphical control element while simultaneously providing access to one or more unselected graphical control elements; and transferring the entered data value to appropriate equipment on the vehicle for implementation. The display size of the top-level and second-level graphical control elements allows the display device to continue to display the primary function.

Abstract: A system for displaying the effect of a change in Automatic Terminal Information Service (ATIS) broadcast. The system comprises a receiver module configured to receive at least two ATIS broadcasts and a parsing module operably connected to the receiver module and configured to parse the received at least two ATIS broadcasts into at least two corresponding sets of ATIS messages. The system includes a comparison module operably connected to the parsing module and configured to compare the at least two sets of ATIS messages to determine if a disparity exists between the at least two sets of ATIS messages. The system includes a display module; and a processor module operably connected to the comparison module and the display module, the processor module being configured to cause the display module to display an alert when it is determined that a disparity exists between the at least two sets of ATIS messages.

Abstract: Disclosed are methods, systems, and non-transitory computer-readable medium for managing configurations of multiple vehicle displays. For instance, a method may include: obtaining a configurable file for an electronic checklist; generating a graphical user interface (GUI) based on the configurable file; displaying the GUI on one of the multiple vehicle displays; receiving a user input on the GUI; and performing a window configuration setting process based on the user input. The method may also include: in response to the user input being a first user input type in a region associated with a context menu indicator: obtaining a window configuration function and a phase of flight variable; generating a context menu based on the window configuration function and the POF variable; and displaying the context menu on the GUI.

Abstract: Disclosed are methods, systems, and non-transitory computer-readable medium for managing communications on a vehicle. For instance, the method may include obtaining a configured state of audio systems and communications systems; generating a graphical user interface (GUI) based on the configured state; displaying the GUI, the GUI including a plurality of icons, the plurality of icons corresponding to the communications systems, the plurality of icons indicating which communications systems are being monitored for output and/or receiving an audio input through the audio systems; receiving a user input on the GUI; and performing a communication control process or a communication setting process based on the user input. The method may further include: in response to determining the user input is the first user input type, performing the communication control process; and in response to determining the user input is the second user input type, performing the communication setting process.

Abstract: A practice airspace management system includes a control unit configured to receive user inputs from a first user and to generate a first training plan based on the user inputs. The control unit is further configured to generate display commands representing the first training plan on a navigation map. The practice airspace management system further includes a display device coupled to receive the display commands from the control unit and configured to display a navigation map view that includes the navigation map and a first training plan symbol representing the first training plan on the navigation map.

Abstract: Methods and systems are provided for managing a minimum equipment list (MEL) for an aircraft. The method comprises first generating a MEL that is specific to the aircraft. Next, the performance parameters of the aircraft are monitored. MEL faults are detected by continually comparing the performance to the MEL during operations of the aircraft. A MEL network is notified of the detected MEL faults. The MEL network includes parties affected by the detected MEL faults.

Abstract: A contextual awareness system for an aircraft and a method from controlling the same are provided. The aircraft, for example, may include, but is not limited to, a touch screen display, a memory configured to store rules defining a relationship between a plurality of data fields, and a processor configured to determine when a data field displayed on the touch screen display is selected, determine at least one data field which is related to the selected data field based upon the rules defining the relationship between a plurality of data fields, generate display data for the touch screen display, the display data comprising a virtual keyboard and a contextual awareness display area, the contextual awareness display area displaying the selected field and the at least one data field which is related to the selected data, and update the selected data field based upon input from the virtual keyboard.

Abstract: A system and method provides aircraft autoflight capability feedback to aircraft pilots to thereby prevent, or at least inhibit, latent errors of omission that may result in operational errors. The system and method uses graphics that communicate subtly and in the background, in a manner that naturally fits with how the visual cortex processes graphical information and how the mind makes quick, and subconscious judgments about information. The system may also use auditory and tactile feedback.

Abstract: A flight deck timer management system includes a database storing conditions representing a first monitoring mode defining at least a first rule, a first timing characteristic defining a first time period for compliance with the first rule, and a first advisory value relative to the first time period at which a first advisory is initiated. A control unit is configured to identify input states based on the input data, and to evaluate the input states in view of the first monitoring mode conditions. When the input states trigger the first monitoring mode, the control unit evaluates the input states in view of the first rule, initiates a first timer based on the first timing characteristic, monitors a first timing status of the first timer relative to the first advisory value, and generates display commands representing the first advisory when the first timer status reaches the first advisory value.

Abstract: A flight deck timer management system includes a database storing conditions representing a first monitoring mode defining at least a first rule, a first timing characteristic defining a first time period for compliance with the first rule, and a first advisory value relative to the first time period at which a first advisory is initiated. A control unit is configured to identify input states based on the input data, and to evaluate the input states in view of the first monitoring mode conditions. When the input states trigger the first monitoring mode, the control unit evaluates the input states in view of the first rule, initiates a first timer based on the first timing characteristic, monitors a first timing status of the first timer relative to the first advisory value, and generates display commands representing the first advisory when the first timer status reaches the first advisory value.

Abstract: A practice airspace management system includes a control unit configured to receive user inputs from a first user and to generate a first training plan based on the user inputs. The control unit is further configured to generate display commands representing the first training plan on a navigation map. The practice airspace management system further includes a display device coupled to receive the display commands from the control unit and configured to display a navigation map view that includes the navigation map and a first training plan symbol representing the first training plan on the navigation map.

Abstract: A method in an aircraft computing system for facilitating communication between a flight crew and external communication facility (ECF) such as air traffic control (ATC) or airline operational control (AOC) is provided. The method comprises monitoring aircraft data by an aircraft computing system for a plurality of pre-defined, non-emergency conditions, detecting, by the aircraft computing system, a pre-defined, non-emergency condition requiring communication from the flight crew to the ECF, automatically generating and displaying a computer-generated message on an aircraft cockpit display responsive to detecting the condition requiring communication from the flight crew to the ECF, providing a selection option for transmitting the message to the ECF, and transmitting the message to the ECF in accordance with the option selected.

Abstract: A system method for providing aircraft lateral navigation system capability feedback to a pilot includes determining, in a processor, when a flight plan has been received that includes a flight leg that needs to be captured by the aircraft. A determination is made, in the processor, when an armed signal has been received, where the armed signal indicating that an aircraft autopilot navigation mode (NAV) has been armed. The processor is used to command a display device to render the flight leg using a first display paradigm when the armed signal has not been received, and to render the flight leg using a second display paradigm when the armed signal has been received.

Abstract: A system method for providing aircraft lateral navigation system capability feedback to a pilot includes determining, in a processor, when a flight plan has been received that includes a flight leg that needs to be captured by the aircraft. A determination is made, in the processor, when an armed signal has been received, where the armed signal indicating that an aircraft autopilot navigation mode (NAV) has been armed. The processor is used to command a display device to render the flight leg using a first display paradigm when the armed signal has not been received, and to render the flight leg using a second display paradigm when the armed signal has been received.

Abstract: A system and method provides aircraft autoflight capability feedback to aircraft pilots to thereby prevent, or at least inhibit, latent errors of omission that may result in operational errors. The system and method uses graphics that communicate subtly and in the background, in a manner that naturally fits with how the visual cortex processes graphical information and how the mind makes quick, and subconscious judgments about information. The system may also use auditory and tactile feedback.

Abstract: A method and system are described for enhancing ground situational awareness to an aircrew via an alphanumeric display of an air traffic control ground clearance, including displaying a symbol for each stage of the clearance. A crewmember may accept or change each stage via a graphical user interface within the alphanumeric display.

Abstract: Methods and systems are provided for displaying a taxi clearance for an aircraft at an airport. One exemplary method involves receiving user input indicative of a constraining taxi path of a plurality of taxi paths at the airport, determining a first taxi portion between an initial location for the taxi clearance and the constraining taxi path, determining a second taxi portion between the constraining taxi path and a destination location for the taxi clearance, and displaying, on a display device associated with the aircraft, a taxi route comprising the first taxi portion, the second taxi portion, and the constraining taxi path between the first taxi portion and the second taxi portion.

Abstract: A wearable device to be worn by an operator of an aircraft includes a communication unit configured to receive aircraft parameters from an aircraft system. The wearable device further includes a database configured to store adverse control rules that define at least a first adverse control associated with a first aircraft state. The wearable device further includes a first sensor to collect data associated with movement and/or location of the wearable device. The wearable device includes a processing unit configured to identify the first aircraft state based on the aircraft parameters, evaluate operator intent based on the movement and/or location of the wearable device, and initiate a first alert when the operator intent corresponds to the first adverse control during the first aircraft state. The wearable device includes a haptic unit configured to communicate the first alert to the operator.

Abstract: A dynamic runway indicator is displayed overlying a conformal runway for assisting a pilot in completing an approach to landing on a runway. The dynamic runway indicator includes a polygon, that by changing position with respect to the conformal runway, provides advanced instrumentation cues to the pilot for adjusting the aircraft flight path to a normal, or recommended, path to the runway for landing, thereby assisting the pilot to improve the accuracy and safety of the approach and landing.