Abstract: A system and method are disclosed for design of a suite of multispectral (MS) sensors and processing of enhanced data streams produced by the sensors for autonomous aircraft flight. The onboard suite of MS sensors is specifically configured to sense and use a MS variety of sensor-tuned objects, either strategically placed objects and/or surveyed and sensor significant existing objects to determine a position and verify position accuracy. The received MS sensor data enables an autonomous aircraft object identification and positioning system to correlate MS sensor data output with a-priori information stored onboard to determine and verify position and trajectory of the autonomous aircraft. Once position and trajectory are known, the object identification and positioning system commands the autonomous aircraft flight management system and autopilot control of the autonomous aircraft.

Abstract: An integrity monitoring system for a first image sensor includes an electronic processor configured to receive sensor data for the provision of image data associated with an environment of the avionic sensor. The electronic processor is configured to monitor the avionic sensor for integrity. The electronic processor is configured to perform at least one of: determining a presence of an optical feature associated with optics of the first image sensor, comparing overlap information derived from the sensor data and other sensor data, comparing characteristics of a digital output stream of the sensor data to expected characteristics, or comparing a first motion derived from the image data and a second motion derived from avionic position equipment.

Abstract: A bezel for overhead panels provides a grip or hand rest so the pilot is not required to maintain a hand at a specific overhead location in space to interactive with a touchscreen display device. Gripping mechanisms take the strain off the arm and allow for more precise inputs during turbulence. In a further aspect, the bezel includes features at known locations to tactilely identify the location. Such features may include indentations or protrusions.

Abstract: A helmet mounted display is embedded in a visor assembly. The visor assembly comprises two molded sections that define portions for receiving waveguides. The optical components are disposed in a portion of the visor assembly and the entire assembly is attached by a hinge to the helmet. The visor assembly includes lateral clips to secure the visor assembly to the helmet, and a night-vision goggle attachment point.

Abstract: A non-uniform sampling pADC is disclosed. The pADC may include an optical pulse source configured to generate uniform optic pulses. The pADC may include a non-uniform sampling system. The non-uniform sampling system may include an inter-pulse timing modulation sub-system configured to convert the uniform optic pulses into non-uniform optic pulses. The non-uniform sampling system may include a timing control sub-system configured to control the timing of the optical pulse source. The pADC may include an optical modulator configured to modulate the non-uniform optical pulses. The pADC may include a photodetector configured to convert the modulated non-uniform optic pulses into electronic pulses. The pADC may include a pulse capture assembly configured to capture a pulse amplitude of the electronic pulses and generate sampled radio frequency output pulses. The pADC may include a quantizer configured to quantize the sampled radio frequency output pulses and generate digital radio frequency output signals.

Abstract: A system and method for dynamic mesh network discovery is disclosed. In embodiments, the system assigns each network asset (e.g., unmanned or manned aircraft or like mobile nodes) a unique asset number. Each asset has a controller coupled to a datalink including antenna elements and a memory for storing an asset table. Each asset periodically broadcasts an asset status message including the asset number. When a status message is received, the receiving asset compares the received asset number to its own asset number. If the received asset number is higher (e.g., of lower priority) than its own asset number, the receiving asset establishes a bidirectional mesh network connection to the broadcasting asset. Assets on the receiving end of a network connection interrogate the establishing asset for its asset number, such that assets on both sides of the connection know the identity of the other and update their asset tables accordingly.

Abstract: A wireless aircraft cabin control panel is disclosed. In embodiments, the wireless aircraft cabin control panel includes a user interface device disposed on a first surface of a bulkhead of an aircraft cabin. In embodiments, the user interface includes a display device, a user input device, wireless communication circuitry, and a controller. The controller may be configured to: generate control signals configured to cause the wireless communication circuitry to transmit wireless control signals to wireless communication circuitry of a control unit disposed on a second surface of the bulkhead; receive power via wireless charging signals received from the wireless communication circuitry of the control unit; distribute power from the wireless charging signals to the display device; extract data signals encoded within the wireless charging signals; and cause the display device to display at least one of an indicator or an image in response to the extracted data signals.

Abstract: Systems and methods of heading determination with global navigation satellite system (GNSS) signal measurements are provided herein. A pair of antennas may be separated by a known baseline length and mounted on a vehicle. A GNSS receiver may obtain pseudorange and carrier phase measurements for GNSS satellites within view. An LRU may estimate carrier phase ambiguities and a two-dimensional vector, using the known baseline length and a linearized measurement model. The LRU may determine integer ambiguities using the estimated carrier phase ambiguities. The LRU may determine assumed wrong fixes of the integer ambiguities and a probability of almost fixed value. The LRU may store the set of integer ambiguities. The LRU may determine, from accumulated data over measurement epochs, updated integer ambiguities. The LRU may correct the carrier phase measurements using the updated integer ambiguities. The LRU may compute the heading using the corrected carrier phase measurements.

Abstract: A multicore processing environment (MCPE) is disclosed. In embodiments, the MCPE includes multiple processing cores hosting multiple user applications configured for simultaneous execution. The cores and user applications share system resources including main memory and input/output (I/O) domains, each I/O domain including multiple I/O devices capable of requesting inbound access to main memory through an I/O memory management unit (IOMMU). For example, the IOMMU cache associates unique cache tags to each I/O device based on device identifiers or settings determined by the system registers, caching the configuration data for each I/O device under the appropriate cache tag. When each I/O device requests main memory access, the IOMMU cache refers to the appropriate configuration data under the corresponding unique cache tag. This prevents contention in the IOMMU cache caused by one device evicting the cache entry of another, minimizing interference channels by reducing the need for main memory access.

Abstract: A system may include a manifold. The manifold may include a body and a rupture disc. The body may include first connector connected to a pressurized source, a second connector, and a third connector. The body may include hollow pathway network including a first path portion extending from the pressurized source to a pathway junction, a second path portion extending from the pathway junction to the second connector, and a third path portion extending from the pathway junction to the third connector. The first path portion may include a bend. The rupture disc may be positioned between the bend and the pathway junction. When the rupture disc is in an unruptured state, the rupture disc may seal the first path portion from the other path portions. When the rupture disc is in a ruptured state, the rupture disc may allow a flow from the pressurized source to the third connector.

Abstract: Combined taxi signage may be generated from taxi signage for a first origination node and taxi signage for a second origination node, the first origination node and the second origination node being of a select proximity and orientation relative to an aircraft. The taxi signage for the first origination node may be generated from the first origination node and at least a first termination node stored within an airport surface routing network data, and a first turning angle determined based on a comparison between the first origination node and the at least the first termination node. The taxi signage for the second origination node may be generated from the second origination node and at least a second termination node stored within the airport surface routing network data, and a second turning angle determined based on a comparison between the second origination node and the at least the second termination node.

Abstract: A system and method. The system may include an integrated circuit (IC) die having two faces and sides. The system may further include mold material surrounding at least the sides of the IC die. The system may further include a redistribution layer and signal pads. The redistribution layer may be positioned between (a) the signal pads and (b) the mold material and the IC die. The redistribution layer may have conductive paths at least connecting the IC die and at least some of the signal pads. A surface of the mold material may abut the redistribution layer. The surface of the mold material may include at least one recessed area having at least one conductive feature connected to at least one of the conductive paths or the IC die.

Abstract: A system may include a computing device including a processor. The processor may be configured to: for correlation threads having populated queues, execute at least some of the correlation threads in parallel, wherein execution of each of the at least some of the correlation threads results in at least one of: at least one new radar track or at least one updated existing radar track; and output each new radar track and each updated existing radar track.

Abstract: A system and method for analog estimation of a spectral correlation function (SCF) provides a photonic carrier to generate a signal comb and offset comb, each comprising N comb tones separated by respective repetition rates ?F and ?F+?F. The signal and offset combs are amplitude-modulated according to an inbound RF signal of interest and filtered via periodic optical filters to produce a sequence of N Fourier components of the signal comb and N Fourier components of the offset comb, each filtered signal comb component overlapping with a filtered offset comb component. In-phase/quadrature (I/Q) components of the products of each component of the complex conjugate of the filtered offset comb and the overlapping counterpart of the filtered signal comb are generated in an optical receiver and digitized into slices of the SCF at a fixed time instance and center frequency, correlated at various cyclic separations ?.

Abstract: A dual or quad aperture radar array switches between states in between radiation cycles to acquire both sum and difference beams. The beams are then processed together to produce a central lobe enhanced beam and a side lobe enhanced beam via difference computations. During interleaved cycles, beams may be processed by Taylor weighting, split Taylor weighting, or Bayliss weighting. Multiple sets of switching cycles may be processed together to refine results.

Abstract: A facemask-mounted augmented reality (AR) display device is disclosed. In embodiments, the display device is hard-mounted to a breathing apparatus (e.g., oxygen mask, smoke mask) fitted to a user's nose and mouth behind a partially or fully covering external face shield. The AR display system includes display surfaces aligned with the eyes of the user and capable of providing the user with a forward field of view that moves with the user's head. The AR display system synthesizes streaming images with additional overlay sources (e.g., mission data, position data) to generate augmented reality content presented to the user within the field of view of the display surfaces.

Abstract: A system and a method of determining an absolute position of a first vehicle can be used in restricted areas. The system performs operations of or the method includes receiving image data from a vision system mounted on a second vehicle, determining a first location of the second vehicle using at least positions of stars in the image data, providing the first location to the first vehicle, determining a first relative position between the first vehicle and the second vehicle using at least one signal communicated between the first vehicle and the second vehicle, and determining the absolute position using at least the relative location data and the first location.

Abstract: A display system includes an interface unit, a head worn display in wireless communication with the interface unit, and a first tracker sensor remote from a head of a user and configured to wirelessly sense a head pose and provide first head tracking data to the interface unit. The interface unit is remote from the head worn display. The display system also includes a second tracker sensor associated with the head of the user and configured to provide second head tracking data associated with the head pose to the head worn display. The interface unit is configured to receive the second head tracking data from the head worn display via at least one wireless link and provide video information for display on the head worn display via the at least one wireless link.

Abstract: A system may include a display installed in an aircraft, a hardware button installed in the aircraft, and a processor installed in the aircraft, wherein the processor may be communicatively coupled to the display and to the hardware button. The processor may be configured to: output at least one view to the display; receive a user input from the hardware button; and based at least on the user input, cause a cursor to move to a default position on one of the at least one view.

Abstract: A semiconductor package system is disclosed. The system includes a first interposer and a first integrated circuit die electrically coupled and thermally coupled to a first side of the first interposer. The system further includes a second integrated circuit die electrically coupled and thermally coupled to a second side of the first interposer. The system further includes a ring carrier electrically coupled and thermally coupled to the first interposer. The ring carrier is configured to transmit an input to the first interposer. In some embodiments, the system further includes at least one thermal spreader thermally coupled to the ring carrier and at least one of the first integrated circuit, the second integrated circuit, or the first interposer.