A system includes an aircraft avionics system and a portable computing device. The aircraft avionics system is configured to run one or more embedded avionics applications. The portable computing device is in operable communication with the aircraft avionics system and is configured to run one or more portable device applications. Each portable device application has resident therein a software development kit having libraries and utilities that enables the portable device application to: establish a secure connection with the aircraft avionics system, establish and maintain a required protocol with the embedded avionics application, and communicate with the embedded avionics application as specified by an application programming interface definition.

A portable computerized device for an aircraft control system includes an input system for inputting commands, a device display for displaying information on the computerized device, a processor, a wireless communication module, and a non-transitory computer readable medium comprising computer executable instructions, the computer executable instructions configured to cause the processor to perform a method. The method can include detecting whether the portable computerized device is in a cockpit state such that the portable computerized device is in and/or docked to an aircraft cockpit or if the portable computerized device is in a remote state such that the portable computerized device is not in an aircraft cockpit or is not docked to an aircraft cockpit. If the portable computerized device is determined to be in a remote state, the method includes operating the remote device in a remote mode. If the portable computerized device is determined to be in a cockpit state, the method includes operating the device in a local mode.

A system for incorporating predictive health data into a mission timeline receives a predictive health event, identifies a time frame for the event, and incorporates the event into a mission timeline. The event may define a probability window with weighted probabilities overlaid onto the mission timeline. The event may define an uncorrected outcome. The uncorrected outcome is rendered onto the mission timeline at a point when the uncorrected outcome will likely occur if no remedial action is taken.

Methods and systems provide a visual user interface on a display device associated with an aircraft. A Flight Information System (FIS) broadcast report; and an Air Traffic Control (ATC) broadcast message are received. The FIS broadcast report and the ATC broadcast message are transcribed. Ownship data for the aircraft is received. The ownship data concerns at least one of: a state of the aircraft, a flight plan for the aircraft and a state of components of the aircraft. The transcribed FIS broadcast report is analyzed with respect to the ownship data to determine filtered FIS information that is relevant to the ownship. A visual user interface (UI) is rendered to be displayed on the display device. The visual UI includes the transcribed ATC broadcast message and the filtered FIS information.

Systems and methods for detection and display of marine objects for an aircraft. One example system includes a transceiver configured to communicate with an Automatic Identification System (AIS) server and an electronic controller located within an aircraft. The electronic controller is configured to provide on a display an interface comprising a map representing a travel area. The electronic controller is configured to provide, on the map, a first graphical representation of the aircraft within the travel area. The electronic controller is configured to receive, via the transceiver, marine object data from the AIS server. The electronic controller is configured to periodically update, on the map, a second graphical representation of a first marine object within the travel area based on the marine object data.

A portable flight navigation tool has a tablet computer with GPS, and memory with an aviation database with international operating rules including transoceanic flight rules, a moving-map database with tracks, coastal airport identifiers and locations, and predefined reporting point locations for transoceanic operations. The navigation tool includes machine readable code for displaying the operating rules, reading locations from the GPS while indicating them on a moving map display, and a trip database with a planned transoceanic route for an individual flight configured by entry of waypoints or names and selection of predefined tracks. The tool has a checklist database and displays checklists for pre-departure, coast-out flight phase, waypoint-reached, and a coast-in flight phases; and may provide a heading and next-waypoint timing for rhumb-line routes from GPS failure locations to the next waypoint of the active route. The tool links as a master/secondary pair with another like tool.

Systems and methods for suggesting, on an avionic display in an aircraft, a communication frequency that is relevant to a context of the aircraft. The method includes determining a location and orientation of the aircraft and referencing an intended flight path to determine, based thereon, the context of the aircraft. The method uses the context to reference an on-board source of a plurality of stored navigation communication frequencies. The method identifies one or more relevant navigation communication frequencies for the context and presents the relevant navigation communication frequencies in a predefined area on an avionic display.

Provided is a flight optimization system and a method of flight optimization that includes generating flight data via an onboard aircraft system, performing a pre-flight cycle by determining an updated tail assignment plan before departure based on the flight data received in real-time from the onboard aircraft system, performing an in-flight cycle by collating and processing in-flight data and external data via an onboard network server, and transmitting the processed data to an electronic flight bag in real-time and performing flight path optimization via a path optimizer application of the electronic flight bag to be accessed by flight personnel, and performing a post-flight cycle by transmitting post-flight data to an event measurement system along with operational data to be processed and sent to a fleet support system and a maintenance system for generating updated flight plans and maintenance plans which are data-driven.

Systems and methods for harvesting data for an electronic flight bag (EFB) device. The system includes an electronic communication device located in the aircraft and configured to receive aircraft state information transmitted in a first communication protocol via an electronic transponder located in the aircraft, decode the aircraft state information, repackage the aircraft state information as decoded in a second communication protocol, and transmit the aircraft state information as repackaged. The system also includes an electronic flight bag device communicatively coupled to the electronic communication device. The electronic flight bag device includes a transceiver configured to receive the aircraft state information as repackaged and transmitted via the electronic communication device. The system also includes an electronic processor configured to process the aircraft state information from the electronic communication device and perform flight performance planning based on the processed aircraft state information.

A method, system, and computer program product for providing an indication that a received vehicle operation instruction can be performed is provided. During operation of a vehicle a vehicle operation instruction is received and at least one vehicle performance parameter to perform the vehicle operation instruction is calculated. Then, a determination is made as to whether the calculated at least one vehicle performance parameter exceeds performance limitations of the vehicle. If at least one performance parameter exceeds a performance limitation, then a first alert is generated and output.