Abstract: A system and method include a phase determination control unit configured to receive position data of an aircraft. The position data includes height of the aircraft, altitude of the aircraft, and distance of the aircraft from one or more locations. The phase determination control unit is further configured to determine variables from messages received from the aircraft. The variables relate to the height of the aircraft, the altitude of the aircraft, and the distance of the aircraft from the one or more locations. The phase determination control unit is further configured to apply fuzzy logic to the variables to determine scores for possible phases of flight of the aircraft, identify a highest score among the possible phases of flight, and determine the highest score as an actual phase of flight of the aircraft.

Abstract: A system and a method include a phase determination control unit configured to receive position data of an aircraft, determine variables from messages received from the aircraft, apply fuzzy logic to the variables to determine scores for possible phases of flight of the aircraft, identify a highest score among the possible phases of flight, and determine the highest score as an actual phase of flight of the aircraft.

Abstract: Certain aspects of the present disclosure provide a method for determining a flight plan for an aircraft, including: determining one or more regions that intersect an initial flight path and comprise at least one terrain feature having an elevation greater than an elevation threshold; for each respective region: determining a flight area based on the initial flight path and an elevation threshold line; determining one or more segments of the initial flight path that comprise one or more terrain features having an elevation greater than the elevation threshold; and determining a modified flight path for each respective segment by: determining a plurality of descent gradients along the respective segment; and moving the respective segment of the initial flight path in the safe descent direction if any of the plurality of descent gradients would collide with any of the one or more terrain features.

Abstract: Certain aspects of the present disclosure provide a method that includes: collecting seat sensor data associated with a plurality of seats in a vehicle; selecting a first subset of data from the collected seat sensor data; providing the first subset of data to a fault detection model; receiving, from the fault detection model, one or more detected seat component faults; and generating, based on the one or more detected seat component faults, a seat condition map associated with the vehicle.

Abstract: Certain aspects of the present disclosure provide a method for determining a flight plan for an aircraft, including: determining one or more regions that intersect an initial flight path and comprise at least one terrain feature having an elevation greater than an elevation threshold; for each respective region: determining a flight area based on the initial flight path and an elevation threshold line; determining one or more segments of the initial flight path that comprise one or more terrain features having an elevation greater than the elevation threshold; and determining a modified flight path for each respective segment by: determining a plurality of descent gradients along the respective segment; and moving the respective segment of the initial flight path in the safe descent direction if any of the plurality of descent gradients would collide with any of the one or more terrain features.

Abstract: A system for taking into account micro wind conditions in a region. The system comprises a plurality of aerial vehicles within the region and a wind speed calculator. Each of the plurality of aerial vehicles has an altitude sensor and a GPS receiver. The wind speed calculator is configured to determine wind vectors within the region using measurements from the plurality of aerial vehicles.

Abstract: A system for redirecting light to a mobile platform includes a satellite and a mobile platform including a first RF antenna that transmits a trajectory data for the mobile platform, and a photovoltaic cell that converts light into electrical energy. The satellite includes a second RF antenna that receives the trajectory data, and a processor coupled to the second RF antenna. The processor computes a target position of the mobile platform based on the trajectory data, and instructs a diffuser system to generate the beam of light and direct the beam to the target position.

Abstract: A method includes determining a first speed value based on a first signal from a first data source. The method also includes determining a second speed value based on a second signal from a second data source. The method further includes determining a first likelihood of icing value based on a third signal from a third data source. The method also includes determining a second likelihood of icing value based on a fourth signal from a fourth data source. The method further includes performing a first comparison between the first speed value and the second speed value and performing a second comparison between the first likelihood of icing value and the second likelihood of icing value. The method also includes generating sensor reliability data based on the first comparison and the second comparison and displaying situational awareness data based on the sensor reliability data.

Abstract: Techniques for updating wake separation distance between aircraft are described. A sensors mesh within a flight path of an aircraft is used to detect when a wake vortex from the aircraft has drifted onto the sensor mesh. A minimum wake separation distance and separation interval for following aircraft are determined based on the various sensor measurements, environmental conditions, and aircraft properties. The minimum wake separation distance and separation interval are used to minimize aircraft separation distances between aircraft that are required due to wake vortex turbulence caused by aircraft during flight.

Abstract: Techniques for updating wake separation distance between aircraft are described. A sensors mesh within a flight path of an aircraft is used to detect when a wake vortex from the aircraft has drifted onto the sensor mesh. A minimum wake separation distance and separation interval for following aircraft are determined based on the various sensor measurements, environmental conditions, and aircraft properties. The minimum wake separation distance and separation interval are used to minimize aircraft separation distances between aircraft that are required due to wake vortex turbulence caused by aircraft during flight.

Abstract: A system for redirecting light to a mobile platform includes a satellite and a mobile platform including a first RF antenna that transmits a trajectory data for the mobile platform, and a photovoltaic cell that converts light into electrical energy. The satellite includes a second RF antenna that receives the trajectory data, and a processor coupled to the second RF antenna. The processor computes a target position of the mobile platform based on the trajectory data, and instructs a diffuser system to generate the beam of light and direct the beam to the target position.

Abstract: A restricted airspace monitoring system and method include a restricted airspace monitoring control unit that is configured to determine if a restricted airspace is active through monitored positions of a plurality of aircraft within an airspace that includes the restricted airspace and/or restriction notice information.

Abstract: Aircraft taxi cost determination systems and methods include a taxi cost determination control unit that determines a total cost of one or more available taxi scenarios for an aircraft at an airport based on fuel cost, engine cost, crew cost, and maintenance cost for the available taxi scenario(s).

Abstract: A wind forecast prediction apparatus includes an historical forecast patterns module configured to generate at least one historical wind forecast pattern and determine a deviation magnitude and a probability of occurrence of the at least one historical wind forecast pattern based on at least one actual wind value; a current wind forecast module; and a wind forecast prediction controller connected to the historical forecast patterns module and current wind forecast module, the wind forecast prediction controller is configured to generate a current wind forecast pattern based on current wind data from the current wind forecast module; and determine a matching historical wind forecast pattern from the at least one historical wind forecast pattern that matches the current wind forecast pattern, where the deviation magnitude and the probability of occurrence of the matching historical wind forecast pattern are combined with the current wind forecast pattern to generate a predicted wind forecast.

Abstract: A method, vehicle, and system for calculating the location of a center of mass of the vehicle and transferring fuel to move the location of the center of mass are provided. The location of the center of mass of the vehicle is determined by measuring or calculating forces acting on the vehicle that counteract the gravitational forces on the vehicle. The location of the center of mass is calculated by determining on a moment arm of the gravitational force that counteracts the moment arms of the other forces acting on the vehicle. Fuel can be transferred among differently-located fuel tanks in the vehicle to move the location of the center of mass to a position in which at least some of the other forces acting on the vehicle are reduced, which may increase the speed and/or efficiency of the vehicle.

Abstract: A system for redirecting sunlight to a mobile platform includes a satellite and a mobile platform including a first RF antenna that transmits a message including a position and velocity of the mobile platform on the path, along with a time of transmission, and a photovoltaic cell that receives and converts light into electrical energy. The satellite includes a second RF antenna that receives the message, an optical channel, a collector system coupled to the optical channel and that gathers sunlight into the optical channel, a diffuser system coupled to the optical channel and that diffuses light therefrom to generate a beam of light, and a processor coupled to the second RF antenna. The processor computes a target position of the mobile platform based on the position, the velocity, and the time of transmission, and instructs the diffuser system to direct the beam to the target position.

Abstract: A restricted airspace monitoring system and method include a restricted airspace monitoring control unit that is configured to determine if a restricted airspace is active through monitored positions of a plurality of aircraft within an airspace that includes the restricted airspace and/or restriction notice information.

Abstract: A method includes determining a first speed value based on a first signal from a first data source. The method also includes determining a second speed value based on a second signal from a second data source. The method further includes determining a first likelihood of icing value based on a third signal from a third data source. The method also includes determining a second likelihood of icing value based on a fourth signal from a fourth data source. The method further includes performing a first comparison between the first speed value and the second speed value and performing a second comparison between the first likelihood of icing value and the second likelihood of icing value. The method also includes generating sensor reliability data based on the first comparison and the second comparison and displaying situational awareness data based on the sensor reliability data.

Abstract: A system for redirecting sunlight to a mobile platform includes a satellite and a mobile platform including a first RF antenna that transmits a message including a position and velocity of the mobile platform on the path, along with a time of transmission, and a photovoltaic cell that receives and converts light into electrical energy. The satellite includes a second RF antenna that receives the message, an optical channel, a collector system coupled to the optical channel and that gathers sunlight into the optical channel, a diffuser system coupled to the optical channel and that diffuses light therefrom to generate a beam of light, and a processor coupled to the second RF antenna. The processor computes a target position of the mobile platform based on the position, the velocity, and the time of transmission, and instructs the diffuser system to direct the beam to the target position.

Abstract: A method includes accessing historical data including timestamped meteorological data and flight path data. The timestamped meteorological data indicates meteorological conditions detected in each of a plurality of geographic regions. The flight path data indicates air traffic volume in each of the plurality of geographic regions during particular time periods. The method also includes, based on the historical data, identifying at least one meteorological condition and at least one time period corresponding to higher than threshold air traffic volume in a particular geographic region of the plurality of geographic regions. The method further includes generating a filter criterion based on the particular geographic region, the at least one meteorological condition, and the at least one time period. The method also includes generating a flight plan based on a portion of the historical data that satisfies the filter criterion.