A method of operating an aircraft during a flight is provided. An onboard monitoring subsystem of the aircraft detects that a flight crew member is fatigued, and an automated flight crew training exercise is activated in response to detecting that the flight crew member is fatigued. The flight crew member is then engaged with the automated flight crew training exercise, including instructions intended to alleviate flight crew fatigue.

A method, apparatus, and aircraft tracker system for reporting state information for an aircraft. A state of the aircraft is identified using sensor data received from an aircraft sensor system in the aircraft. The state information is transmitted at a reporting rate set using the state of the aircraft identified from the sensor data, at least one of a crew command or a ground command when at least one of the crew command is received from a crew interface or the ground command is received from a ground source, and a policy defining priorities for reporting that are based on at least one of the crew command, the ground command, or the state of the aircraft identified from the sensor data.

An automated aircraft flight data and delivery management system and method operates in a normal state and a demand state. The demand state may be self-initiated or manually-initiated, and may be triggered during situations which include but are not limited to situations when the aircraft is in a potential or confirmed emergency situation. Data transmission increases in intensity when the system is in a demand state.

A system for an aircraft and method of determining intrusion of an avionics component or system in an aircraft having multiple avionics components and systems communicating over an aircraft communications network monitored by a system, including monitoring, by the system, data communication over the aircraft communications network for at least some of the avionics components or system and comparing, by the system, the monitored communications for the at least some of the avionics components to corresponding operational profiles.

In one or more embodiments, the method for a streaming flight data from an aircraft involves transmitting, from a flight data unit(s), the flight data to a flight data recorder streaming (FDRS) server. The method further involves determining, by the FDRS server, at least one antenna to use for streaming the flight data by analyzing the flight data. Also, the method involves generating, by the FDRS server, an antenna selection signal according to the antenna(s) to use for streaming. In addition, the method involves transmitting, by the FDRS server, an antenna selection signal to an antenna switch unit. Additionally, the method involves selecting, by the antenna switch unit, the antenna(s) to use for streaming according to the antenna selection signal. Further, the method involves streaming, by the antenna(s) to use for streaming, the flight data to a satellite(s).

Methods and systems for detecting an anomaly with a communication service provided to a transportation vessel along a travel route are disclosed. In some aspects, performance metrics are obtained for a monitored vessel while the travel is in progress. Historical travel routes are identified having characteristics similar to those of the monitored vessel's travel route. Corresponding performance metrics of the historical travel routes may be aggregated via mean or median operations, and the results compared to equivalent metrics of the monitored vessel. If accumulated negative variances between the monitored vessel's performance and the historical travel route's performance exceed a threshold, an anomaly may be determined to exist. In this case, the systems and methods may generate an alert in various forms, including email, text, or selective network commands to various networking components, including, for example, instructing networking equipment on board the monitored vessel to perform a power cycle operation.

An apparatus and method of delivering an alert from an aircraft to a search and rescue system. An alert from an aircraft is received via a communications satellite. The alert comprises identification information identifying the aircraft and position information identifying the position of the aircraft. In response to receiving the alert, an emulated distress radio beacon signal is generated. The emulated distress radio beacon signal comprises the identification information and the position information in a standard format of a signal generated by a distress radio beacon. The emulated distress radio beacon signal is broadcast from a location other than the aircraft as an emulated distress radio beacon transmission that is configured to be received and processed by the search and rescue system.

The invention is a service for sending and/or receiving messages in a first format intended for a recipient or authority, where the service identifies for the intended recipient a second format for receiving messages, and where the service formats a communication for delivery to the intended recipient, where the message is prepared to be presented to the recipient in the first and/or the second format.

Methods and systems are provided for preventing interference from simultaneous data transmissions in a remote control system. A controlled terminal is typically configured to receive control data from a controlling terminal and to transmit feedback data to a monitoring terminal. To prevent interference caused by the simultaneous transmissions of control data and feedback data. The controlling terminal can transmit the control data to the monitoring terminal, which then transmits the control data to the controlled terminal. Such transmission of the control data may be carried out in a way that does not interfere with the transmission of the feedback data.

A system includes a first terminal and a second terminal. The first terminal is configured to communicate with a controlled terminal via a first communication link. The second terminal is configured to communicate with the controlled terminal via a second communication link and communicate with the first terminal via a third communication link. The second terminal is further configured to relay data between the first terminal and the controlled terminal via the second communication link and the third communication link.