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 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: Methods and devices for growing plants in non-native environments and/or protecting crops from adverse weather conditions are disclosed in which sub-surface growing wells are used. The sub-surface growing wells extend below ground-level and include an opening that is exposed to above-ground conditions. The growing wells are outfitted with a well cap positioned above the well opening and the well cap can be moved either down to seal off the well from above-ground conditions or up to expose the well to above-ground conditions. The growing wells can be enhanced with a variety of control and monitoring systems to provide optimal growing conditions for plants contained in the wells.

Abstract: Methods for transmitting data between parties or locations using temporary markings that are affixed to a human or animal body are disclosed, along with related devices. These markings, or tattoos, are intended to be temporary, where the lifespan of the marking is dictated by the marking material used and the material's interaction with the dermis of the wearer. The markings can be visible, invisible or a combination thereof, placed in predetermined or random locations. The markings can also be affixed in visible or hidden locations, depending on privacy concerns.

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 runway exiting system is configured to determine a suitable exit off of a runway for an aircraft. The runway exiting system includes a housing, and one or more processors within the housing that are configured to determine a current position of the aircraft on the runway, determine a current rate of deceleration of the aircraft on the runway, and determine the suitable exit off of the runway for the aircraft based, at least in part, on the current position of the aircraft on the runway and the current rate of deceleration of the aircraft on the runway.

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 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: 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 runway exiting system is configured to determine a suitable exit off of a runway for an aircraft. The runway exiting system includes a housing, and one or more processors within the housing that are configured to determine a current position of the aircraft on the runway, determine a current rate of deceleration of the aircraft on the runway, and determine the suitable exit off of the runway for the aircraft based, at least in part, on the current position of the aircraft on the runway and the current rate of deceleration of the aircraft on the runway.

Abstract: A flight plan analysis system is configured to determine a flight plan decision regarding a proposed flight plan for an unmanned aerial vehicle (UAV). The flight plan analysis system includes a flight plan database that stores risk factor data, and a flight plan analysis unit communicatively coupled to the flight plan database. The flight plan analysis unit receives a proposed flight plan for the UAV and determines the flight plan decision based on an analysis of the proposed flight plan and the risk factor data.

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: 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: An instrument panel is identified based on a captured image such as a photograph. A target configuration of the instrument panel is compared with a current configuration of the instrument panel based on the image data. An indication of differences between the target configuration and the current configuration is provided.

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 for providing a minimum safe altitude indication on an aircraft display is described. The method includes utilizing current aircraft heading and position data to generate a location and orientation for an own-ship depiction with respect to an aircraft display, utilizing the current position data, along with terrain data, to generate minimum safe altitude data for an area surrounding the aircraft, and displaying on the aircraft display, about the location for own-ship depiction, the minimum safe altitudes surrounding the aircraft.