A device includes a transceiver, a receiver, and a processor. The transceiver is configured to receive feedback data from an unmanned aerial vehicle (UAV) and transmit control data to the UAV via a first communication link. The receiver is configured to receive the control data from a controlling terminal via a second communication link. The second communication link does not interfere with the first communication link. The processor is configured to determine whether the feedback data and the control data are being simultaneously transmitted via the first communication link.

Provided is an unmanned aerial vehicle that broadcasts a route and future location information of the unmanned aerial vehicle within preset coverage based on sensing data and current location information of the unmanned aerial vehicle. The unmanned aerial vehicle includes a calculator configured to calculate a predicted route and second location information of the unmanned aerial vehicle corresponding to a preset period of time based on first location information and sensing data; and a transmitter configured to periodically broadcast a first notification signal that includes the first location information, the predicted route, and the second location information.

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.

A computer-implemented method for prioritized flight data transmission includes receiving a frame of flight data from one or more aircraft data sensors, the frame of flight data comprising a plurality of parameters collected from one or more avionics systems, associating each parameter of the plurality of parameters with a respective priority level, decomposing the frame of flight data into a plurality of flight data frame layers, wherein each flight data frame layer of the plurality of flight data frame layers comprises a subset of the plurality of parameters having respective priority levels that are equivalent, and transmitting, to a ground station, a first flight data frame layer of the plurality of flight data frame layers comprising parameters having a highest respective priority level.

A system and method for autonomous distress tracking of an aircraft. An automatic dependent surveillance-broadcast transceiver is configured to transmit an automatic distress transmission. A system controller comprises a distress identifier that is configured to determine when the aircraft is in a distress condition. The system controller is configured to control the automatic dependent surveillance-broadcast transceiver to transmit the automatic distress transmission in response to a determination that the aircraft is in the distress condition. The automatic dependent surveillance-broadcast transceiver and the system controller are contained within a housing attached to the aircraft on an outside of the aircraft.

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.

A method 140 of assessing an operator emotional state 131 and sending an alert 144 based on the emotional state 131. The method 140 includes tracking 141 during a time period, using at least one sensor 103, 105, 106, 112, 117, one of an image sensor data, voice data or a biometric parameter of an operator. Determining 142, using a controller 120 that is operatively connected to at least one sensor 103, 105, 106, 112, 117, a probability of a likely emotional state 131 from a list of emotional states 131 of an operator based on one of the image sensor data, voice data or the biometric parameter. Comparing 143, using a processor, the probability of one of the likely emotional states 131 of the operator with a baseline emotional state 131 of the operator. Sending 144, using the controller 120, an alert if most likely emotional state deviates from the baseline emotional state by a predetermined threshold.

The aim of the invention is to optimise the monitoring and security of at least one enclosure, allowing a constant and complete view of the enclosure, and a modulated assessment of the state of security of same. For this purpose, the invention proposes to transmit images of the enclosure wirelessly to a mobile medium for helping the flight crew assess the situation and the measures to take in case of a sensitive security situation. According to one embodiment, the optimised system for monitoring and securing an enclosure, a cockpit (3), a cabin (2) and/or a luggage hold (4) of an aircraft (1), comprises video cameras (21a to 23a, 21b to 23b, 24 to 28) distributed so as to define a field of view inside or outside the enclosure (2 to 4), mobile (2T) or fixed (3A) display media dedicated to members of the crew of the enclosure capable, via suitable wireless transmission/reception means (20A), of receiving image streams transmitted by the video cameras (21a to 23a, 21b to 23b, 24 to 28) and of connecting to auxiliary data sources and to means for locking/unlocking (7 to 10, 41) the enclosure (2 to 4) arranged in areas sensitive with respect to security.

A monitoring terminal includes a transceiver, a receiver, and a processor. The transceiver provides a two-way communication with an unmanned aerial vehicle (UAV) via a first communication link and is configured to receive feedback data and a feedback data indication from the UAV and transmit control data to the UAV. The receiver is configured to receive the control data and a control data indication from a controlling terminal via a second communication link. The second communication link does not interfere with the first communication link. The processor is configured to determine whether the feedback data and the control data are being simultaneously transmitted via the first communication link based on the feedback data indication and the control data indication.