Abstract: Disclosed herein are systems for routing wireless communications. Some systems may include an apparatus comprising an enclosure configured to attach to an external portion of an aircraft and which may contain: a wireless communications device, and an antenna in communication with the wireless communications device and configured to send or receive signals to and/or from aircraft.

Abstract: Disclosed herein are systems for routing wireless communications. Some systems may include an apparatus comprising an enclosure configured to attach to an external portion of an aircraft and which may contain: a wireless communications device, and an antenna in communication with the wireless communications device and configured to send or receive signals to and/or from aircraft.

Abstract: Disclosed herein are systems for routing wireless communications. Some systems may include an apparatus comprising an enclosure configured to attach to an external portion of an aircraft and which may contain: a wireless communications device, and an antenna in communication with the wireless communications device and configured to send or receive signals to and/or from aircraft.

Abstract: Disclosed herein are systems for routing wireless communications. Some systems may include an apparatus comprising an enclosure configured to attach to an external portion of an aircraft and which may contain: a wireless communications device, and an antenna in communication with the wireless communications device and configured to send or receive signals to and/or from aircraft.

Abstract: A system and related methods for location determination aboard a subject vehicle not equipped with a GNSS-based positioning system receives position signals transmitted by non-satellite atmospheric vehicles and surface objects, which may include precise locations of the transmitting objects or position metrics associated with containment regions within which the transmitting objects should be to a particular certainty level. The received position signals may include ADS-B signals transmitted by proximate aircraft and facilities. The system may determine ownship location via multilateration of received position signals, via processing the received position metrics and corresponding containment regions, or via combining or correlating the two to determine accurate ownship location data of the subject vehicle.

Abstract: A system and related method for regulating the location of an unmanned aircraft system (UAS) determines the current position of the UAS via onboard sensors or via decoding and derivation of ADS-B signals received from other vehicles. The system may operate in inert mode, where the position of the UAS is not broadcast, or alert mode, where the position of the UAS is continually broadcast via ADS-B Out signal. Based on the position of the UAS, the system detects proximate vehicles, restricted airspaces, or other problem statuses of the UAS. If a problem status is detected, the UAS may activate the alert mode. If a problem status is critical, the UAS may execute an auto-landing or correct course to exit a restricted airspace or avoid a detected vehicle.

Abstract: A system, apparatus, and related method for receiving and correlating Manchester encoded data signals includes a receiver for receiving 1090ES/ADS-B or other Manchester encoded signals. A sampler extracts and oversamples data strings from the received signals. Sample correlators compare the oversampled data strings to oversampled versions of each possible pattern for the extracted data string and determine a score indicating how closely the possible pattern (or its oversampled counterpart) matches the extracted data string (or its oversampled version) on a bitwise or symbolwise basis. The system outputs correlated and decoded data string most closely matching the extracted data string based on the set of determined scores.

Abstract: A system for controlling an unmanned aerial vehicle may include a GNSS receiver, a transponder, one or more flight controls, a UAV operation module, a UAV mission module, and a UAV chassis. The system may include an operating area defined within an airspace and an airspace controller, and a transponder key issued to the UAV by the airspace controller. The airspace controller and the UAV may communicate to unlock UAV access of the operating area, including transmitting a transponder ID code for verification to the airspace controller; receiving a read certificate from the airspace controller; transmitting a mission plan to the airspace controller; receiving a mission key from the airspace controller; verifying the mission key via read back transmission to the airspace controller; and receiving a mission plan from the airspace controller in the form of the transponder key, the mission plan unlocking access to the operating area.

Abstract: A gimbal-assisted continuous-wave (CW) Doppler radar detection system mountable to an unmanned aircraft system may be rotated in three degrees of freedom relative to the UAS to provide targeted multidirectional obstacle detection by transmitting CW signals throughout a field of view and analyzing reflected signals from obstacles within the field of view. The radar assembly may be articulated to provide track-ahead detection in anticipation of a heading or altitude change of the UAS, to center on a detected obstacle in order to classify or identify it more clearly. The radar assembly may be rotated below the UAS and its field of view changed to increase breadth and accuracy at a shorter effective range, in order to determine real-time altitude or terrain data while the UAS executes a landing.