Abstract: A system comprises a physical display unit and an aircraft system component. The aircraft system component is configured to output a first signal for display according to a first display format. The system also includes an abstraction component configured to generate a virtual display page according to the first protocol based on the signal received from the aircraft system component and to map the virtual display page into two or more modified pages. Each of the modified pages is configured according to a second display format and corresponds to a respective portion of the virtual display page. The abstraction component is further configured to output a second signal comprising a first of the two or more modified pages to the physical display unit for display according to the second display format. The abstraction component is configured to output a signal comprising a second modified page based on user input.

Abstract: A method for minimizing propagation time of at least one queued-up datalink TPDU comprises determining whether a current TPDU ready for transmission requires acknowledgement; transmitting the current TPDU, starting a retry timer, and setting a transmission count to one, when acknowledgement required; determining whether acknowledgement received after transmitting the current TPDU; determining whether a pending TPDU is awaiting transmission when acknowledgement is not received; when a pending TPDU is awaiting transmission, determining whether elapsed wait time of the current TPDU is greater than a preselected minimum; incrementing the transmission count by one when elapsed wait time is greater than the preselected minimum; determining again whether there is a pending TPDU awaiting transmission when the transmission count is less than a predetermined maximum and an inactivity timer has not expired; and when there is still at least one pending TPDU awaiting transmission, retransmitting the current TPDU and resta

Abstract: An avionics system comprising a human machine interface configured to display a user interface and a control device is provided. The control device coupled to the human machine interface, wherein the control device is configured to send and receive controller/pilot data link communications (CPDLC) messages and adjust the user interface based on a first CPDLC version of an established first CPDLC session.

Abstract: A system and method for dynamically validating uplink messages during flight are provided. The system comprises at least one processing unit in an aircraft, and at least one communication device in the aircraft that is operatively connected to the processing unit. The communication device is configured to receive uplink messages from a ground air traffic control (ATC) center, and transmit downlink messages to the ground ATC center. The system also includes a human machine interface (HMI) in the aircraft that is operatively connected to the processing unit. The HMI is configured to receive input from a user and display information to the user. One or more data sources that provide dynamic information are in operative communication with the processing unit. The processing unit is configured to determine whether an ATC uplink message is acceptable based on analysis of the dynamic information from the one or more data sources.

Abstract: A graphical in-flight message representation system comprises a sensor configured to measure a characteristic of a flight of an aircraft and a communication device configured to send and receive in-flight messages. An in-flight message is a message communicated during the flight of the aircraft. The system also comprises a display unit configured to display a graphical flight progress indicator and one or more message icons, each of the one or more message icons corresponding to a respective in-flight message. The graphical flight progress indicator is representative of the characteristic of the flight measured by the sensor. Each of the one or more message icons are displayed in location relative to the graphical flight progress indicator based on the measured characteristic of the flight when the respective in-flight message was communicated.

Abstract: An avionics display system is provided that modifies the appearance of an uplink message when the uplink message is affected by a flight information message. The avionics display system comprises a display device; and a processing device configured to: determine whether a flight information message affects an uplink message; and modify the displayed appearance of the uplink message on a display device when the uplink message is affected by the flight information message; wherein the display device is communicatively coupled to the processing device and located onboard an aircraft.

Abstract: Embodiments of the present invention provide improved systems and methods for a programmable portable electronic device for airborne operational communications. In one embodiment, a system for preventing unauthorized access to operational aircraft data comprises a personal electronic device and a plurality of aircraft systems that produce avionic operational data. The system further comprises an airborne server in network communication with the personal electronic device and the plurality of aircraft systems, wherein the airborne server implements security measures to prevent unauthorized electronic devices from accessing the avionic operational data, wherein the airborne server controls the dissemination of avionic operational data to electronic devices.

Abstract: An aerospace communication system comprises a communication management unit; a first communication device configured to transmit and receive data over a first communication network; and a second communication device configured to transmit and receive data over a second communication network. The first communication device is coupled to a corresponding interface of the communication management unit. The second communication device is communicatively separated from the communication management unit by the first communication device such that the communication management unit is unaware of the second communication device. The first communication device includes routing logic configured to determine whether to send each message received from the communication management unit over the first communication network or to the second communication device for transmission over the second communication network.

Abstract: Systems and methods for displaying position sensitive datalink messages on avionics displays are provided. In one embodiment, a flight deck instrument display system for an aircraft comprises: a flight plan display screen that displays a graphical representation of at least a part of an aircraft's planned flight path together with symbology representing a position of the aircraft with respect to the aircraft's planned flight path; wherein the flight plan display screen further displays at least one symbol positioned along the graphical representation of at least a part of the aircraft's planned flight path that indicates a point of applicability for a received uplink datalink message.

Abstract: A method for minimizing propagation time of at least one queued-up datalink TPDU comprises determining whether a current TPDU ready for transmission requires acknowledgement; transmitting the current TPDU, starting a retry timer, and setting a transmission count to one, when acknowledgement required; determining whether acknowledgement received after transmitting the current TPDU; determining whether a pending TPDU is awaiting transmission when acknowledgement is not received; when a pending TPDU is awaiting transmission, determining whether elapsed wait time of the current TPDU is greater than a preselected minimum; incrementing the transmission count by one when elapsed wait time is greater than the preselected minimum; determining again whether there is a pending TPDU awaiting transmission when the transmission count is less than a predetermined maximum and an inactivity timer has not expired; and when there is still at least one pending TPDU awaiting transmission, retransmitting the current TPDU and resta

Abstract: A method for minimizing datalink message propagation time comprises determining whether a datalink TPDU ready for transmission requires an acknowledgement; transmitting the TPDU, starting a transport retry timer, and setting a transmission count to one, when acknowledgement is required; determining whether acknowledgement is received after transmitting the TPDU; determining whether the retry timer has expired if acknowledgement not received; determining whether a hold mode is in effect when the retry timer has expired; determining whether a transport inactivity timer has expired when the hold mode is in effect; determining whether the hold mode is still in effect when the inactivity timer has not expired; when the hold mode is no longer in effect, incrementing the transmission count by one; and retransmitting the datalink TPDU and restarting the retry timer, when the transmission count is less than a predetermined maximum value and the inactivity timer has not expired.

Abstract: Systems and methods for enhanced adoptive validation of ATC clearance requests are provided. In certain implementations, a system comprises a processor executing a controller pilot data link communication application, and at least one source of dynamic information coupled to the processor, wherein the dynamic information comprises data relevant to possible flight paths of an aircraft, the dynamic information being changeable during the flight of the aircraft, wherein the processor processes at least one clearance request that identifies a deviation from the present flight path and validates the at least one clearance request against the dynamic information.

Abstract: An avionics system includes a human-machine interface (HMI), wherein the HMI includes a display device that displays information to an operator and an input device that receives input from an operator; a storage device that stores master air traffic control (ATC) center data; a memory device that stores separately loaded ATC center data and hard-coded ATC center data, and a processing device communicatively coupled to the HMI, the storage device and the memory device. The processing device compares the separately loaded ATC center data with the hard-coded ATC center data; requests operator validation of changes between the separately loaded ATC center data and the hard-coded ATC center data using the HMI; and updates the master ATC center data when the operator validates the changes between the separately loaded ATC center data and the hard-coded ATC center data.

Abstract: In one embodiment, an aerospace system is provided. The aerospace system comprises at least one display unit configured to display flight data and a memory configured to store one or more flight plan associations. Each flight plan association is an association between a data link message and a respective waypoint in a flight plan. The aerospace system also comprises a processing unit configured to determine when each respective waypoint in the flight plan is reached based on a comparison of current location data to the flight plan. When each respective waypoint is reached, the processing unit is configured to identify any data link messages associated with the respective waypoint based on the flight plan associations and to direct the at least one display unit to display a respective notification for each identified data link message associated with the respective waypoint.

Abstract: A system comprises a physical display unit and an aircraft system component. The aircraft system component is configured to output a first signal for display according to a first display format. The system also includes an abstraction component configured to generate a virtual display page according to the first protocol based on the signal received from the aircraft system component and to map the virtual display page into two or more modified pages. Each of the modified pages is configured according to a second display format and corresponds to a respective portion of the virtual display page. The abstraction component is further configured to output a second signal comprising a first of the two or more modified pages to the physical display unit for display according to the second display format. The abstraction component is configured to output a signal comprising a second modified page based on user input.

Abstract: A method to provide access to air traffic control centers to a crew member for context management (CM) logon is provided. The method includes accessing a flight plan for an aircraft at a processor; accessing a listing of air traffic control centers; generating a subset of the air traffic control centers at the processor; and displaying the subset of the air traffic control centers as at least a part of a prioritized listing of the air traffic control centers on a display for the crew member. The generating is based on at least one of: an ATC-center authority coverage area overlapping a flight path associated with the flight plan; and a pre-selected distance from the flight path.

Abstract: An aerospace communication system comprises a communication management unit; a first communication device configured to transmit and receive data over a first communication network; and a second communication device configured to transmit and receive data over a second communication network. The first communication device is coupled to a corresponding interface of the communication management unit. The second communication device is communicatively separated from the communication management unit by the first communication device such that the communication management unit is unaware of the second communication device. The first communication device includes routing logic configured to determine whether to send each message received from the communication management unit over the first communication network or to the second communication device for transmission over the second communication network.

Abstract: An avionics system includes a human-machine interface (HMI), wherein the HMI includes a display device that displays information to an operator and an input device that receives input from an operator; a storage device that stores master air traffic control (ATC) center data; a memory device that stores separately loaded ATC center data and hard-coded ATC center data, and a processing device communicatively coupled to the HMI, the storage device and the memory device. The processing device compares the separately loaded ATC center data with the hard-coded ATC center data; requests operator validation of changes between the separately loaded ATC center data and the hard-coded ATC center data using the HMI; and updates the master ATC center data when the operator validates the changes between the separately loaded ATC center data and the hard-coded ATC center data.

Abstract: A method of ensuring secure and cost effective communication of aeronautical data to and from an aircraft is provided. The method includes uplinking air-ground aircraft data communications via an aeronautical safety data link and downlinking air-ground aircraft data communications via a consumer data link separated from the aeronautical safety data link by a one-way firewall.

Abstract: A data messaging system is provided. The data messaging system includes means for displaying a message log on a human-machine-interface (HMI) device; means for selecting at least one message identified for quick retrieval at a later time; means for storing the at least one selected message identified for quick retrieval in at least one save-selected-message log in one of a functional module and a computer, wherein a number of messages in the at least one save-selected-message log is much less than a number of messages in the message log by an end of a trip; means for displaying titles of the messages in the at least one save-selected-message log on the HMI device in place of the message log; and means for displaying a selected message associated with a title selected from the displayed titles of the messages in the at least one save-selected-message log.