Abstract: An electrical interface can include one or more connector devices that facilitate communication between components while they are connected. The connector devices can provide a secure communication and/or power link that resists infiltration by foreign object debris (“FOD”) as well as redundant electrical pathways. The connector devices can further provide mechanisms that are lightweight, are operable in a broad range of temperatures (e.g., low temperatures), accommodate displacement without loss of electrical continuity, and are of low resistance and induction. The connector devices can further provide a kickoff force upon separation of the components.

Abstract: A gradient-index (GRIN) lens comprises an input surface defined by a body configured to receive electromagnetic (EM) waves from an aperture-constrained array; and an output surface defined by the body configured to output phase-aligned EM waves based on the received EM waves from the aperture-constrained array. The GRIN lens can be dimension-constrained in at least one dimension and can have a non-linear permittivity taper in at least a first dimension. The GRIN lens can provide gain for the received EM waves from the aperture-constrained array.

Abstract: Electrochemical cells, such as those present within flow batteries, can include at least one electrode with one face being more hydrophilic than is the other. Such electrodes can lessen the incidence of parasitic reactions by directing convective electrolyte circulation toward a separator in the electrochemical cell. Flow batteries containing the electrochemical cells can include: a first half-cell containing a first electrode with a first face and a second face that are directionally opposite one another, a second half-cell containing a second electrode with a first face and a second face that are directionally opposite one another, and a separator disposed between the first half-cell and the second half-cell. The first face of both the first and second electrodes is disposed adjacent to the separator. The first face of at least one of the first electrode and the second electrode is more hydrophilic than is the second face.

Abstract: A computer-implemented method comprising determining, by the processor, a set of objects of the plurality of objects having the shared coordinates (XS, YS) and at a location along the depth direction (ZS); and prioritizing, by the processor, an object from the set of objects based on at least two of metadata of the set of objects, screen areas of the set of objects, transparency of the set of objects, and opaqueness of at least one object of the set of objects currently displayed to improve the selection of at least one of mutually occluded objects and mutually partially occluded objects in the virtual environment. The method includes associating the prioritized object with the viewer input device for detecting interactions with the prioritized object displayed on the display device by the viewer input device. The prioritized object is updated on the screen of the display device based on the interactions.

Abstract: A pitch beam movable by a pitch change shaft to adjust a pitch of at least one rotor blade of a rotor system via a pitch linkage includes a first surface having a generally planar configuration, a smooth second surface disposed opposite the first surface, and a sidewall extending between the first surface and the second surface. A pitch linkage connection point is disposed at the sidewall to which the pitch linkage is attachable. An interior is defined between the first surface and the second surface and an opening extends through the first and second surface at a rotational axis of the rotor system to which the pitch change shaft is attached. Movement of the pitch change shaft moves the pitch beam and adjusts the pitch of the at least one rotor blade via the pitch linkage attached at the pitch linkage connection point.

Abstract: An airship includes a ballonet, a ballonet tracking system, and a vehicle management system. The ballonet is disposed within the airship and includes a ballonet surface. The ballonet tracking system includes one or more light emitters disposed within the ballonet at one or more fixed locations and one or more light detectors disposed within the ballonet at the one or more fixed locations. The ballonet tracking system measures a plurality of distances between one or more fixed locations and one or more locations on the ballonet surface. The ballonet tracking system also calculates differences between a predetermined set of expected distances and the plurality of measured distances. Based on the calculated differences, the ballonet tracking system calculates a volume of the ballonet. The vehicle management system is communicatively coupled to the ballonet tracking system and controls the operation of the airship using the calculated volume of the ballonet.

Abstract: A printed circuit board (PCB) device including one or more insulating layers and one or more conducting layers arranged to form a layer stack; and one or more blind holes disposed along a side edge of the layer stack and parallel to a plane of the layer stack. Each of the one or more blind holes along the side edge of the layer stack is configured to receive a pin. Each pin can make an electrical connection with a corresponding blind hole.

Abstract: An apparatus for precision shaving is provided. In one embodiment, the apparatus includes an endmill cutter, a base frame, and a motor adjacent to the base frame and having a shaft on one end. A coupler is positioned between the shaft and the endmill cutter. A positioning slide is housed within the base frame and a coupler frame and a first gear are fastened to the positioning slide. A second gear is adjacent to the first gear, the second gear having a set of first teeth and a set of second teeth positioned opposite the set of first teeth. The set of first teeth and the set of second teeth are separated by a gap.

Abstract: A system for determining airborne light detection and ranging (lidar) installation angles includes an airborne platform, a light detection and ranging (lidar) apparatus, a navigation system and a processor. The airborne platform performs a calibration flight in an orbit. The lidar apparatus is installed on the airborne platform for wind-velocity measurement. The navigation system is on board the airborne platform and measures motion data associated with movements of the airborne platform and generates a navigation signal. The processor determines in real time one or more installation angles of the lidar apparatus on the airborne platform to improve accuracy of the wind-velocity measurement.

Abstract: A technique relates to route planning. Points associated with a start location and a destination location are received. It is determined whether the points comprise one or more hard points, one or more soft points, or both. At least one obstruction to avoid is determined. A route is autonomously generated comprising the points and segments associated with the points, the segments comprising rhumb lines, great-circle arcs, or both. Responsive to the points comprising the one or more soft points, the at least one obstruction is avoided by permitting a distance associated with the one or more soft points to be reached and adding at least one free waypoint. Responsive to the points comprising the one or more hard points, the at least one obstruction is avoided by requiring the one or more hard points to be reached and adding the at least one free waypoint.

Abstract: A reflector antenna includes a reflector, a feed, and a beamforming network. The feed is spaced apart at a focal distance from the reflector. The feed includes an array of dual linear polarized elements. The beamforming network is operatively coupled to the feed. The beamforming network is configured to generate a Sigma pattern and a Delta pattern in a plane orthogonal to the reflector plane of symmetry.

Abstract: A rover can include a spherical shall and an avionics hub. The spherical shell defines a spherical volume and having an inner surface and an outer surface. The avionics hub is disposed within the spherical volume. The avionics hub includes an avionics shell, a data acquisition unit, and a plurality of motortrain assemblies. The avionics shell is disposed with the spherical volume of the spherical shell. The data acquisition unit is disposed within the avionics shell. Each motortrain assembly includes a motorized wheel extending at least partially through the avionics shell and in contact with the inner surface of the spherical shell, the plurality of motortrain assemblies configured to rotate the spherical shell relative to the avionics shell to move the rover.

Abstract: Provided herein are various improvements to communication systems and satellite-carried communications. In one example, a method provides communication coverage for at least an endpoint device within a cell. The method includes detecting access preamble communications transferred by the endpoint device during a random access slot of a base station by at least applying a selected quantity of successive sets of processing windows in accordance with a round-trip minimum communication delay expected between the base station and the cell, with each of the successive sets shifted in time by a selected duration.

Abstract: According to certain embodiments, reducing data signal bandwidth comprises receiving a multi-resolution image having a plurality of concentric regions that each have a different level of resolution, where the regions closer to the center having greater levels of resolution. Generating a representative image comprising first rasterizing the multi-resolution image into a pixel representation of pixel data with an array of pixel values. A ring of pixels for each region results from discarding duplicate pixels from each region such that only the interior pixels from each region are preserved. In a first circular direction, duplicate pixels along each ring are discarded, the preserved unique pixels resulting in ring fragments. The ring fragments are then moved towards the center so that there are no gaps between the ring fragments for each level of resolution.

Abstract: A technique relates to evaluating autonomous landing of an aircraft. An autonomous vehicle receives cellular metadata and determines whether a landing site is suitable for the autonomous vehicle based on the cellular metadata.

Abstract: A system includes a mandrel having an exterior surface configured to receive composite material, a first end, and a second end opposite the first end, an end support coupled to the first end of the mandrel such that the mandrel is rotatable about an axis of rotation, and an intermediate support configured to support the mandrel between the first end and the second end such that at least a portion of the exterior surface is exposed while the mandrel is supported by the intermediate support, a vertical distance between the intermediate support and the axis of rotation defining a support distance, and the intermediate support being adjustable between a first position having a first support distance and a second position having a second support distance greater than the first support distance.

Abstract: A system for secure processor virtualization including a secure initialization memory and one or more processors coupled to the secure initialization memory is disclosed. The secure initialization memory includes initialization instructions for launching a security runtime environment before operating systems and cryptographic keying for security handoffs. The processors are configured to retrieve the initialization instructions from the secure initialization memory at startup, execute the initialization instructions to launch the security runtime environment and retrieve at least a portion of the cryptographic keying, and generate specific keying for chip-level resources the processors by combining instruction sets of the chip-level resources and the cryptographic keying.

Abstract: In one embodiment, a system includes a ground layer, a first layer, a second layer, and a plurality of vias. The first layer includes a first insulating material and a plurality of first metallic strips. The second layer includes a second insulating material and a plurality of second metallic strips. The plurality of vias electrically connect one or more of the plurality of first metallic strips of the first layer to one or more of the plurality of second metallic strips of the second layer. The plurality of first metallic strips of the first layer and the plurality of second metallic strips of the second layer form a plurality of capacitors and a plurality of conductors. Each capacitor is located in the first layer. Each conductor is partially located in the first layer and partially located in the second layer.

Abstract: A hosted multi-reflector antenna system includes a primary reflector, a subreflector, an aperture, a feed structure and an anti-jam housing. The feed structure includes an electronically steered antenna (ESA). The subreflector directs a reflected beam between a primary reflector and an ESA, and the anti-jam housing encloses the subreflector and the ESA. The antenna system is thermo-elastically decoupled and thermally self-sufficient, accommodates thermal dissipation of the feed structure, and can maintain a precise antenna alignment.

Abstract: A hybrid propulsion system extracts electrical power using a combined heat engine and electrical generator. The propulsion system includes a gas generator, an electrical power generator disposed upstream of the gas generator and configured to be driven by a power turbine, an output power shaft mated to the power turbine and extending through a central axis of the gas generator and power generator unit, an engine enclosure circumferentially surrounding the power generator, and a shroud disposed between the power generator and the engine enclosure. The electrical power generator includes at least one rotating member and a stationary conductive member. The at least one rotating member includes a magnetic portion, and rotation of the at least one rotating member relative to stationary conductive member generates a current transmissible by one or more coupled power output cables.