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 passenger cabin monitoring system includes infrared cameras disposed in respective passenger rest compartments, a flight attendant information system including at least one display and at least one speaker, and a computing device in communication with the infrared cameras and the flight attendant information system. The computing device is configured to detect a temperature of a portion of passenger rest compartment based on one or more thermal images generated by a respective infrared camera of the passenger rest compartment. The computing device is further configured to compare the temperature of the portion of the passenger rest compartment with a predetermined critical temperature and provide an audible alert and/or a visual alert via the flight attendant information system to indicate a critical status of the passenger rest compartment when the temperature of the portion of the passenger rest compartment is above the predetermined critical temperature.

The present disclosure provides a radio and method for automatically adjusting, in response to ambient noise, the volume setting of a radio. The radio comprises a microphone for receiving ambient audio and generating a microphone signal; a codec for receiving the microphone signal and generating a processor signal representative of the ambient audio; and processor circuitry operable to receive the processor signal, determine an ambient audio level in response to the processor signal, and determine an adjusted radio volume to generate a radio volume control signal, wherein the adjusted radio volume is determined by calculating a difference between a baseline volume level and ambient audio level and adding a current volume level setting, wherein the codec is also operable to receive the radio volume control signal and generate an output signal to adjust the radio volume setting to maintain a net difference between the adjusted radio volume and ambient audio.

A system and method for emergency manual flight direction to a non-pilot enables the non-pilot an ability to safely land an aircraft after an event causing a single pilot of the aircraft to become unable to perform pilot tasks. The emergency flight director (EFD) receives inputs from a plurality of sources and displays information, maneuver, configuration and communication commands to the non-pilot on a flight deck display. Inputs to the system include aircraft state data as well as airport and current weather information associated with each available airport. The EFD determines an appropriate emergency landing runway and presents simplified commands coupled with animated aircraft specific graphics to the non-pilot to manually fly the aircraft to a safe landing.

An unmanned aerial vehicle (UAV) includes a first communication module, a second communication module, and one or more processors. The first communication module is configured to directly receive control data from a controlling terminal via a first communication link and the control data is used to control operations of the UAV. The second communication module is configured to transmit feedback data to a monitoring terminal via a second communication link. The monitoring terminal is located remotely from the UAV. The one or more processors are, individually or collectively, configured to terminate and reactivate the first wireless communication link based on one or more predetermined criteria.

The present disclosure provides a radio and method for automatically adjusting, in response to ambient noise, the volume setting of a radio. The radio comprises a microphone for receiving ambient audio and generating a microphone signal; a codec for receiving the microphone signal and generating a processor signal representative of the ambient audio; and processor circuitry operable to receive the processor signal, determine an ambient audio level in response to the processor signal, and determine an adjusted radio volume to generate a radio volume control signal, wherein the adjusted radio volume is determined by calculating a difference between a baseline volume level and ambient audio level and adding a current volume level setting, wherein the codec is also operable to receive the radio volume control signal and generate an output signal to adjust the radio volume setting to maintain a net difference between the adjusted radio volume and ambient audio.

Aircraft tracking and emergency location avionics architectures that integrate existing fixed Emergency Locator Transmitter (ELT) installations, their associated aircraft avionics systems and existing flight deck interfaces with an Autonomous Distress Tracker (ADT) transceiver unit in a coupled configuration. Some of the architectures allow the ADT unit and its advanced distress detecting and reporting capabilities to monitor the activation control path for the ELT and the associated ELT activation outputs. Other architectures place the ADT unit and its advanced distress detection capabilities and ground-controlled capabilities in the activation control path for the ELT. Additional architectures entail the connection of an ADT unit to an ELT remote panel on the flight deck of an aircraft.

Various methods enable a robotic vehicle to determine that it has been stolen, determine an appropriate opportunity to perform a recovery operation, and perform the recovery operation at the appropriate opportunity. Examples of recovery operations include traveling to a predetermined location, identifying and traveling to a safe location to await recovery, and crashing to self-destruct when the predetermined location cannot be reached and a safe location cannot be identified.

Pilot health monitoring systems, methods, and apparatuses are provided. A pilot health monitoring system is configured to collect information regarding the pilot's physiological and/or physical characteristics, and information regarding a state of the aircraft; analyze the information; determine a health condition of the pilot and/or a state of the aircraft; and/or provide warnings and/or commands as a function of the information.

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. The ground center receives flight tracking communications from the aircraft for monitoring flight conditions to determine if the aircraft is encountering abnormal flight conditions, and is operative to send an uplink request to the aircraft to change the default flight tracking preferences.