A method for integrating an application into a flight deck includes receiving, by the flight deck, an identification of the application for integrating into the flight deck, wherein the application is running on a portable electronic device (PED) separate from the flight deck. The method also includes transmitting, by the flight deck, the identification of the application to the PED. The method additionally includes locating an application window corresponding to the application on a display of the PED and reading pixel data corresponding to the application window on the display of the PED. The method further includes transmitting the pixel data from the PED to the flight deck and integrating the application into the flight deck using the pixel data.

This disclosure relates to methods and devices for detecting configurations of aircraft. A sound is recorded from an interior of an aircraft. A transform is calculated of the sound. The transform is compared with a calibration transform of a known configuration. A closeness parameter is determined based on the comparison. A detected configuration is indicated if the closeness parameter is above a threshold.

Disclosed are systems, methods, and non-transitory computer-readable medium for automatically capturing and recording anomalies and vehicle operator interaction data. For example, a method may comprise receiving external operational data associated with operation of a vehicle, detecting loading of one or more applications associated with the operation of the vehicle, capturing one or more interactions between an operator of the vehicle and the one or more applications at the vehicle, logging anomalies data associated with the operation of the vehicle, based on any anomaly identified from the received external operational data, the detected loading of the one or more applications, or the captured one or more interactions, recording the received external operational data, the detected loading of the one or more applications, the captured one or more interactions, and/or the logged anomalies data, to generate recorder data, storing the generated recorder data in one or more vehicle data recorder databases.

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.

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.

An addressable display system configured for use in a mounting adapter configured to mount a personal electronic device (PED) on an aircraft includes a transparent surface configured to overlay the display surface of a PED when the PED is mounted in the mounting adapter wherein the transparent surface includes a region that is uniformly coated with a coating layer that when activated with a select excitation wavelength is configured to emit visible light to annunciate a message indicating a problem with an image displayed on a PED display; a lighting source configured to provide light in at an excitation wavelength; a MEMS (microelectromechanical systems) scanner module that is controllable to write desired symbology for annunciation at different addressable locations on the transparent surface; and an imaging device configured to capture an image of the PED display for an integrity check of data displayed on the PED display.

A method is provided. The method comprises receiving a travel plan for a vehicle including a travel path information; determining a vehicle trajectory using the travel path information; obtaining forecasts of at least one of weather and vehicles proximate in time and location to the vehicle along the vehicle trajectory; determining, based upon at least one of the weather forecast and the other vehicles forecast, if at least one optional function would be beneficial to enable during vehicle travel along the vehicle trajectory; and generating at least one enablement code corresponding to the determined at least one optional function.

An automatic, autonomous predictive aircraft surface state event track (ASSET) system, includes a mobile device onboard an aircraft and a remote service in communication with the mobile device. The mobile device includes a processor, and an application that in turn includes machine instructions encoded on a non-transitory computer-readable storage medium. The processor executes the machine instructions to receive sensor data from aircraft onboard sensors, the sensor data indicating an operational state of the aircraft; and transmit the sensor data. The remote service receives the sensor data and includes a remote processor that executes machine instructions to compute an operational state of the aircraft; identify an aircraft event associated the aircraft; and using the aircraft operational data, the sensor data, and the event, predict that the aircraft will meet a next scheduled aircraft event within a specified time window.

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.

An aircrew automation system that provides a pilot with high-fidelity knowledge of the aircraft's physical state, and notifies that pilot of any deviations in expected state based on predictive models. The aircrew automation may be provided as a non-invasive ride-along aircrew automation system that perceives the state of the aircraft through visual techniques, derives the aircraft state vector and other aircraft information, and communicates any deviations from expected aircraft state to the pilot.