Abstract: In one embodiment, a method is provided. The method comprises: obtaining data; generating complete travel plan; determining at least one of: one or more current travel conditions and one or more future travel conditions; automatically generating at least one proposed message based upon the at least one of one or more current travel conditions and one or more future travel conditions; rendering one icon, for each of the at least one proposed message, on a grid having a first axis specifying altitude and a second axis specifying one of distance and time; and wherein each of the at least one proposed message is configured to be at least one of selectable, reviewable, printable, editable, and sendable.

Abstract: Systems and methods for enhanced subnetwork preference logic are herein provided. In certain implementations, a method for transmitting messages over a datalink communication system includes identifying a location of a first communication unit; and identifying an altitude of the first communication unit. Further, the method includes selecting a sub-network preference for the first communication unit for communicating between the first communication unit and one or more other communication units, wherein the sub-network preference is selected based on the location and the altitude of the first communication unit, wherein the sub-network preference identifies one or more sub-networks in order of preference; and transmitting one or more messages to the one or more other communication units through a sub-network that is a most preferred sub-network as indicated by the selected sub-network preference and available for communications.

Abstract: Systems and methods for providing air traffic control center data to aircraft is provided. In certain embodiments an avionics system includes a communication device configured to communicate with a data center and an air traffic control center; and a processing unit configured to execute machine readable instructions. In at least one embodiments, the machine readable instructions cause the processing unit to manage communications associated with the flight of an aircraft, wherein the communications are communicated through the communication device with the data center; distinguish identifying information received through the communication device, wherein the identifying information identifies at least one of the air traffic control center and associated aeronautical telecommunications network address; and establish a communication session with the air traffic control center using the identifying information received through the communication device.

Abstract: An apparatus is provided. The apparatus comprises a processing system comprising: an ARINC 429 converter system; an Internet protocol (IP) suite; and an Ethernet driver; wherein the processing system is configured to be coupled to a communications management system and at least one IP radio; wherein the processing system converts data, from the communications management system, from an ARINC 429 protocol into a transport layer protocol, an IP and a Ethernet protocol; and wherein the processing system converts data, from the IP radio, from the Ethernet protocol, IP, and transport layer protocol to the ARINC 429 protocol.

Abstract: In one embodiment, a method is provided. The method comprises: selecting, with a communications management system configured to be installed on a vehicle, at least one primary channel on a multichannel transceiver; transmitting and/or receiving data over the at least one primary channel; searching, with the multichannel transceiver for other viable communications links; and selecting a new at least one primary channel.

Abstract: A method and system for formatting datalink messages is disclosed. The method comprises providing a format style of parameters and/or portions of free text for a datalink message; sending the datalink message to a destination; decoding the datalink message at the destination for both content and format style information; sending the content and format style information to a display processor; and generating parameter or free text highlighting information on a display screen corresponding to the content and format style information.

Abstract: Systems and methods for a non-integrated CPDLC solution are provided. In one embodiment, the system includes: a first and second computing system for respectively executing a first and second CPDLC application; a Human Machine Interface coupled to the first and second computing systems, the Human Machine Interface providing access to display screens generated by both the first and second CPDLC applications; and a data authority function that determines a data authority application from the first and second CPDLC applications based on which of the first and second CPDLC applications has a current data authority (CDA) session. The data authority function prevents the first CPDLC application from establishing a concurrent current data authority session when the second CPDLC application is the data authority application. The data authority function prevents the second CPDLC application from establishing a concurrent current data authority session when the first CPDLC application is the data authority application.

Abstract: Systems and methods for modifying multiple element request datalink messages in avionics system are provided. A method includes generating a plurality of downlink message element information at a verify screen displayed by a display. The method further allows for the changing of at least one downlink message element information of the plurality of downlink message element information within the verify screen. Moreover, the method concatenates the plurality of downlink message element information after the changing of the at least one element information in preparation of generating a concatenating downlink message element information message to be downlinked.

Abstract: A method for processing Aircraft Communications Addressing and Reporting System (ACARS) messages at a Communications Management Unit (CMU) on an aircraft is provided. The method includes, for an ACARS downlink message, receiving a message at the CMU from an application on a computer external to the CMU onboard the aircraft, reading a field in the message that indicates a message type for that application, determining an ACARS label associated with the message type, using the determined ACARS label instead of the industry standard ACARS label/sublabel associated with the onboard application external to the CMU, and sending the ACARS downlink message encoded with the determined ACARS label to a ground system to be delivered to a peer ground application.

Abstract: In one embodiment, a method is provided. The method comprises: obtaining data; generating complete travel plan; determining at least one of: one or more current travel conditions and one or more future travel conditions; automatically generating at least one proposed message based upon the at least one of one or more current travel conditions and one or more future travel conditions; rendering one icon, for each of the at least one proposed message, on a grid having a first axis specifying altitude and a second axis specifying one of distance and time; and wherein each of the at least one proposed message is configured to be at least one of selectable, reviewable, printable, editable, and sendable.

Abstract: In one embodiment, a method for implementing a non-integrated CPDLC solution is provided. The method includes monitoring a datalink router for messages from a first CPDLC application in a first one or more execution partitions, wherein the first one or more execution partitions are configured to implement a first CPDLC application and wherein messages from the first CPDLC application and a second CPDLC application in a second one or more execution partitions use the datalink router to interface with one or more radio transceivers. The method also includes when the second CPDLC application has an active current data authority (CDA) air traffic control (ATC) connection, inhibiting communication between the first CPDLC application and an ATC ground station by discarding downlink messages of the first CPDLC application from the datalink router.

Abstract: A method of compressing messages into a message block is provided. The method includes monitoring a router queue of a first communication hub for short messages that are waiting to be transmitted to the same second communication hub. A short message is a message that contains less characters than a maximum number of characters allowed in a user data block of the message block. At least two short messages monitored in the router queue waiting to be transmitted to the same second communication hub are combined when a combined message character number is less than the maximum number of characters allowed in the user data block of the message block. The message block with the combined at least two messages is then transmitted.

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: 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: In one embodiment, a method for processing vehicle messages is provided. The method comprises: receiving a vehicle message for transmission; determining whether a condition exists to expedite transmission of the vehicle message; determining if a preferential sub-network is available; determining if at least one less preferential sub-network is available; and when the condition exists, when the preferential sub-network is not available for use, and the less preferential sub-network is available, expediting the transmission of the vehicle message over a less preferential sub-network.

Abstract: A system for dynamic flight tracking of an aircraft comprises a ground center configured to communicate with a flight tracking application onboard an aircraft, wherein the flight tracking application is preloaded with default flight tracking preferences comprising a normal time rate interval for sending normal condition position reports to the ground center when a flight condition is normal; abnormal time rate intervals for sending abnormal condition position reports to the ground center when abnormal flight conditions are detected, with the abnormal time rate intervals less than the normal time rate interval; and abnormal flight condition criteria to determine which aircraft conditions to monitor for detecting abnormal flight conditions.

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: 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: Systems and methods for secure communications over broadband datalinks are provided. In certain implementations, a system for providing secure communications through a communication link includes a first communication unit that includes a processing unit that is configured to execute code that causes the first communication unit to verify messages with a firewall as they are received by the first communication unit; remove encapsulation data that encapsulates a message received from a second communication unit; check a digital signature appended to the message received from a second communication unit through a non-secure communication link; perform an integrity check on the message; and when the message is verified through the digital signature and the integrity check, process the message; wherein removal of the encapsulation data and implementation of the firewall is in a first partition and performance of the integrity check and verification of the digital signature is in a second partition.

Abstract: A system to distribute an Aircraft Operations Communication (AOC) application is provided. The system includes communication components in a vehicle, and an AOC database. The communication components include one of: a Communication Management Unit (CMU); or a Communication Management Function (CMF); and at least one of: at least one electronic flight bag (EFB); and at least one cabin terminal. The AOC database includes an operational configuration for aircraft operations communication for the communication components in the vehicle. The AOC database is loaded into at least one of: the CMU, the CMF, the at least one EFB; the at least one cabin terminal; and a database device. The AOC database configures the operation of the communication components in the vehicle.