Abstract:
A system and method is disclosed for providing dynamic tactile feedback. A tactile feedback generator is mounted in each vehicle in a group of vehicles and is coupled to provide a controllable tactile feedback signal to an operator of each vehicle in the group of vehicles upon receipt of an activation signal. A tactile feedback control device is mounted in each vehicle in the group of vehicles and is coupled to the tactile feedback generator for selectively providing an activation signal and a tactile feedback characteristic signal thereto. An accelerometer is positioned within each vehicle in the group of vehicles. A turbulence processing unit is coupled to receive accelerometer data from each accelerometer. The turbulence processing unit processes the accelerometer data to identify characteristics of a current level of turbulence-induced vibration, and, based thereon, selects and provides updated tactile feedback characteristics to each tactile feedback control device.
Abstract:
A flight range-restricting system is configured to control a flight range of an unmanned aerial vehicle (UAV). The flight range-restricting system includes a database including a UAV capabilities storage area that stores UAV capabilities data indicative of technical specifications of the UAV, and a restricted airspace storage area that stores restricted airspace data indicative of a restricted airspace. A range-restricting control unit is communicatively coupled to the database. The range-restricting control unit controls the flight range of the UAV based on a current location of the UAV, the UAV capabilities data, and the restricted airspace data.
Abstract:
The present disclosure provides for informed de-icing by identifying a travel time range for an aircraft from a de-icing station to a runway; identifying a holdover window based on predicted weather conditions during the travel time range; estimating a takeoff time for the aircraft based on a takeoff queue for the runway and the travel time range; and in response to the holdover window expiring before the estimated takeoff time, delaying the aircraft from de-icing. In some aspects, informed de-icing includes, in response to identifying an aircraft scheduled for de-icing within a caution threshold of a scheduled takeoff time and to determining that a push time cannot be delayed: evaluating an effect of repeating a de-icing operation for the aircraft on flight operations; and in response to the effect exceeding an impact threshold: rescheduling the de-icing operation for the aircraft based on a new takeoff time.
Abstract:
A system and a method include at least one control unit that determines a de-icing time for an aircraft within a de-icing area of an airport, predicts a de-icing time for an aircraft within a de-icing area of an airport, schedules de-icing times for a plurality of aircraft within a de-icing area of an airport, and/or predicts demand for future de-icing operations of aircraft within a de-icing area of an airport.
Abstract:
A system and method is disclosed for providing dynamic tactile feedback. A tactile feedback generator is mounted in each vehicle in a group of vehicles and is coupled to provide a controllable tactile feedback signal to an operator of each vehicle in the group of vehicles upon receipt of an activation signal. A tactile feedback control device is mounted in each vehicle in the group of vehicles and is coupled to the tactile feedback generator for selectively providing an activation signal and a tactile feedback characteristic signal thereto. An accelerometer is positioned within each vehicle in the group of vehicles. A turbulence processing unit is coupled to receive accelerometer data from each accelerometer. The turbulence processing unit processes the accelerometer data to identify characteristics of a current level of turbulence-induced vibration, and, based thereon, selects and provides updated tactile feedback characteristics to each tactile feedback control device.
Abstract:
A wearable electronic display system detects aircraft flight related conditions, compares the detected flight related conditions with rules or procedures, retrieves flight condition information relating to phase of flight, and displays small amounts of contextually relevant flight condition information on a display screen.
Abstract:
A wearable electronic display system detects aircraft flight related conditions, compares the detected flight related conditions with rules or procedures, retrieves flight condition information relating to phase of flight, and displays small amounts of contextually relevant flight condition information on a display screen.
Abstract:
A wearable electronic display system detects aircraft flight related conditions, compares the detected flight related conditions with rules or procedures, retrieves flight condition information relating to phase of flight, and displays small amounts of contextually relevant flight condition information on a display screen.
Abstract:
A method and apparatus for managing a touch screen system. Data generated by an acceleration detector about acceleration of the touch screen system is received. The acceleration detector is located within the touch screen system. An action is initiated by an input manager when the acceleration of the touch screen system reduces usability of the touch screen system.