Abstract: Systems and methods for embedding a warning signal in a sensor pulse. When a taxi anticollision system of a host aircraft senses a threat headed for the aircraft, a warning signal is embedded in a sensor pulse to warn the offending vehicle that it is in the field of view of the host aircraft's sensor and is moving on a trajectory that is threatening collision with the host aircraft. Alternately, the radar issues a dedicated pulse for reading and alerting the receiving device.

Abstract: Systems and methods of a security architecture for a connected aircraft are disclosed. In at least one embodiment, an avionics server comprises a plurality of device ports, wherein each of the plurality of device ports is coupled to a respective one of a plurality of device network interface cards and dedicated to a respective one of a plurality of avionics domains which corresponds to the respective device network interface card. Further, at least one processing device is configured to identify one or more signals from a respective user received at one or more of the plurality of device ports and to verify whether the user has access to the respective avionics domains that are dedicated to the one or more device ports over which the one or more signals are received.

Abstract: Systems and methods for embedding a warning signal in a sensor pulse. When a taxi anticollision system of a host aircraft senses a threat headed for the aircraft, a warning signal is embedded in a sensor pulse to warn the offending vehicle that it is in the field of view of the host aircraft's sensor and is moving on a trajectory that is threatening collision with the host aircraft. Alternately, the radar issues a dedicated pulse for reading and alerting the receiving device.

Abstract: Systems and methods for embedding a warning signal in a sensor pulse. When a taxi anticollision system of a host aircraft senses a threat headed for the aircraft, a warning signal is embedded in a sensor pulse to warn the offending vehicle that it is in the field of view of the host aircraft's sensor and is moving on a trajectory that is threatening collision with the host aircraft. Alternately, the radar issues a dedicated pulse for reading and alerting the receiving device.

Abstract: Systems and methods for aiding in pilot awareness of obstacles relative to aircraft features. An exemplary processor receives sensor information from one or more sensors mounted in an aircraft feature (e.g. light modules), determines if at least one obstacle is located within a predefined field of view based on the received sensor or database information and generates an image. The image includes an ownship icon having at least one feature representing wingtips of the aircraft and at least one indicator associated with the determined at least one obstacle. A display device presents the generated image. The display device presents a tip of a first sense coverage area adjacent to one wingtip feature associated with the port wing and a tip of the second sense coverage area adjacent to one wingtip feature associated with the starboard wing. The indicator is presented within at least one of the coverage areas.

Abstract: Systems and methods of a security architecture for a connected aircraft are disclosed. In at least one embodiment, an avionics server comprises a plurality of device ports, wherein each of the plurality of device ports is coupled to a respective one of a plurality of device network interface cards and dedicated to a respective one of a plurality of avionics domains which corresponds to the respective device network interface card. Further, at least one processing device is configured to identify one or more signals from a respective user received at one or more of the plurality of device ports and to verify whether the user has access to the respective avionics domains that are dedicated to the one or more device ports over which the one or more signals are received.

Abstract: Systems and methods for creating a narrow vertical pathway of detection that permits the enforcement of a fixed “exclusion zone” that is narrow and does not widen with range. An advantage to this approach is that the zone or corridor does not widen with range, permitting a fixed exclusion zone that will ignore items that will pass above or below the wing. An exemplary system located on a vehicle includes at least two vertically separated antennas that receive radar reflection signals, a processor, and an output device. The processor receives the radar reflection signals received by the antennas, determines vertical position of any obstacles identified in the radar reflection signals and determines if the obstacles are within a predefined alert zone. The output device outputs an alert if any obstacle is within the alert zone. The predefined alert zone is related to a protruding portion of the vehicle.

Abstract: A system is configured to generate and display information regarding a strike zone of an aircraft. In some examples, a system is configured to generate and display an image of an environment around an aircraft together with a graphical indication of a strike zone of the aircraft, where the indication is scaled to reflect the strike zone at a distance range of one or more detected objects.

Abstract: Systems and methods communicate sensor data pertaining to detected weather between aircraft. An exemplary system has at least one sensor on a transmitting aircraft, wherein the sensor is configured to detect weather and configured to output sensor data. The system has a first transceiver on the transmitting aircraft that is configured to transmit a signal with the sensor data. And the system has a second transceiver on a receiving aircraft that is configured to receive the signal containing the sensor data transmitted by the first transceiver. The sensor data of the transmitting aircraft is fused with sensor data of the receiving aircraft for a geographic region of interest to extend the effective sensor coverage and to resolve at least one of a location conflict and a severity conflict between the sensor data of the transmitting aircraft and the receiving aircraft.

Abstract: Systems and methods for embedding a warning signal in a sensor pulse. When a taxi anticollision system of a host aircraft senses a threat headed for the aircraft, a warning signal is embedded in a sensor pulse to warn the offending vehicle that it is in the field of view of the host aircraft's sensor and is moving on a trajectory that is threatening collision with the host aircraft. Alternately, the radar issues a dedicated pulse for reading and alerting the receiving device.

Abstract: Systems and methods for creating a narrow vertical pathway of detection that permits the enforcement of a fixed “exclusion zone” that is narrow and does not widen with range. An advantage to this approach is that the zone or corridor does not widen with range, permitting a fixed exclusion zone that will ignore items that will pass above or below the wing. An exemplary system located on a vehicle includes at least two vertically separated antennas that receive radar reflection signals, a processor, and an output device. The processor receives the radar reflection signals received by the antennas, determines vertical position of any obstacles identified in the radar reflection signals and determines if the obstacles are within a predefined alert zone. The output device outputs an alert if any obstacle is within the alert zone. The predefined alert zone is related to a protruding portion of the vehicle.

Abstract: Systems and methods for aiding in pilot awareness of obstacles relative to aircraft features. An exemplary processor receives sensor information from one or more sensors mounted in an aircraft feature (e.g. light modules), determines if at least one obstacle is located within a predefined field of view based on the received sensor or database information and generates an image. The image includes an ownship icon having at least one feature representing wingtips of the aircraft and at least one indicator associated with the determined at least one obstacle. A display device presents the generated image. The display device presents a tip of a first sense coverage area adjacent to one wingtip feature associated with the port wing and a tip of the second sense coverage area adjacent to one wingtip feature associated with the starboard wing. The indicator is presented within at least one of the coverage areas.

Abstract: A system comprises a plurality of fixed cameras that each having a field of regard. Each point within an area of interest is covered by the field of regard of at least two of the cameras. Each camera captures an image of its field of regard and a plurality of calibration points within the area of interest. A processor calibrates the imaging system by at least associating the coordinates of each of the plurality of calibration points with a calibration pixel corresponding to an image of the calibration point in the image of each of the cameras. The processor geolocates the object of interest within the area of interest by at least comparing the location an image of the object of interest to the calibration pixels in the images generated by each of the plurality of cameras.

Abstract: Systems and methods communicate sensor data pertaining to detected weather between aircraft. An exemplary system has at least one sensor on a transmitting aircraft that is configured to detect weather and configured to output sensor data, and a transceiver that is configured to receive a query from a requesting aircraft for the sensor data and that is configured to transmit a signal with the sensor data for receipt by the requesting aircraft in response to receiving the query. Upon receipt by the requesting aircraft, the received sensor data of the transmitting aircraft may then be fused with sensor data of the requesting aircraft for a geographic region of interest to extend the effective sensor coverage and to resolve at least one of a location conflict and a severity conflict between the sensor data of the transmitting aircraft and the requesting aircraft.

Abstract: Systems and methods for a target locator device are provided. In one embodiment, a target locator device comprises: a high performance gyroscope; an inertial measurement unit including an accelerometer triad and a gyroscope triad; a rangefinder; a global navigation satellite system (GNSS) receiver; and a processor coupled to the high performance gyroscope, the inertial measurement unit, the rangefinder and the GNSS receiver. The processor derives an alignment heading from a heading measurement provided by the high performance gyroscope. The processor calculates a heading to a target based on a deviation from the alignment heading as measured from a heading and elevation measurement determined from the inertial measurement unit.

Abstract: A system comprises a plurality of fixed cameras that each having a field of regard. Each point within an area of interest is covered by the field of regard of at least two of the cameras. Each camera captures an image of its field of regard and a plurality of calibration points within the area of interest. A processor calibrates the imaging system by at least associating the coordinates of each of the plurality of calibration points with a calibration pixel corresponding to an image of the calibration point in the image of each of the cameras. The processor geolocates the object of interest within the area of interest by at least comparing the location an image of the object of interest to the calibration pixels in the images generated by each of the plurality of cameras.

Abstract: Systems and methods communicate sensor data pertaining to detected weather between aircraft. An exemplary system receives a signal from a remote aircraft that includes at least sensor data acquired from sensors on the remote aircraft. The system fuses the sensor data of the remote aircraft with sensor data of the receiving aircraft to resolve at least one of a location conflict and a severity conflict between the sensor data of the remote aircraft and the receiving aircraft. The system presents weather information on a display corresponding to the fused sensor data of the remote aircraft and the receiving aircraft.

Abstract: Systems and methods communicate sensor data pertaining to detected weather between aircraft. An exemplary system has at least one sensor on a transmitting aircraft that is configured to detect weather and configured to output sensor data, and a transceiver that is configured to receive a query from a requesting aircraft for the sensor data and that is configured to transmit a signal with the sensor data for receipt by the requesting aircraft in response to receiving the query. Upon receipt by the requesting aircraft, the received sensor data of the transmitting aircraft may then be fused with sensor data of the requesting aircraft for a geographic region of interest to extend the effective sensor coverage and to resolve at least one of a location conflict and a severity conflict between the sensor data of the transmitting aircraft and the requesting aircraft.

Abstract: Methods and systems for predicting turbulence. An exemplary system decomposes near-range reflectivity data into multiple adaptive, three-dimensional Gaussian component functions and decomposes turbulence data into multiple adaptive, three-dimensional Gaussian component functions. The multiple adaptive, three-dimensional Gaussian component functions may include parameters, such as center position, amplitude, and dimensional standard deviations that are determined adaptively to maximally match the measured reflectivity. The multiple adaptive, three-dimensional Gaussian component functions may include parameters adjusted to maximally match the measured turbulence data.

Abstract: Systems and methods communicate sensor data pertaining to detected weather between aircraft. An exemplary system has at least one sensor on a transmitting aircraft, wherein the sensor is configured to detect weather and configured to output sensor data. The system has a first transceiver on the transmitting aircraft that is configured to transmit a signal with the sensor data. And the system has a second transceiver on a receiving aircraft that is configured to receive the signal containing the sensor data transmitted by the first transceiver. The sensor data of the transmitting aircraft is fused with sensor data of the receiving aircraft for a geographic region of interest to extend the effective sensor coverage and to resolve at least one of a location conflict and a severity conflict between the sensor data of the transmitting aircraft and the receiving aircraft.