Abstract: A method and system for computing the deceleration performance to a destination point of a vertical takeoff and landing (VTOL) aircraft has been developed. First, predicted performance of the deceleration of the VTOL aircraft is generated and based on pre-determined data for the VTOL aircraft. Sensors of the VTOL aircraft are monitored to capture real-time performance of the deceleration of the VTOL aircraft. A blended display is created of deceleration of the VTOL aircraft by blending the predicted performance and the real-time performance and is shown to the pilot of the VTOL aircraft. The blended display is continuously adjusted by weighting emphasis on the predicted performance based on the degree of correlation to the real-time performance.

Abstract: Systems and methods for presenting a qualitative risk assessment for an aircraft to perform a flight procedure. Methods include determining: a pilot support value that is representative of a human-machine interface (HMI) onboard the aircraft; a crew factors value representative of a number of pilots and respective experience; an equipment state value of the aircraft, representing available and functioning avionic systems; a type of procedure for the flight procedure; a remaining trip length; an airport facilities state value; an Airport facilities state value; a physical environment value; and, an environmental state value. The method calculates the qualitative risk assessment, as a function of the determined values/factors and presents the qualitative risk assessment in a predefined area on an avionic display in the aircraft.

Abstract: Methods and devices are presented for transforming a layout of a densely packed grid of micro-LED light emitters to a layout of a square rectilinear pixel grid to achieve compatibility with hardware and software used in imaging and display technologies. In particular, a pattern of regular hexagonal emitter cells for fabrication on a III-nitride substrate can be transformed to a square pixel array of irregular hexagonal trichrome pixels that are readily addressable. Separation between adjacent trichrome pixels, and between their constituent emitters, can be established for overlay tolerance, while maintaining a cell packing density of about 70% and a pixel pitch of about 4.0 ?m. Wavelength and quantum efficiency properties are shown to depend on optical current density, which can be determined by the emitter area specified in the grid layout.

Abstract: The disclosure describes various aspects of monolithic integration of different light emitting structures on a same substrate. In an aspect, a device for light generation is described having a substrate with one or more buffer layers made a material that includes GaN. The device also includes light emitting structures, which are epitaxially grown on a same surface of a top buffer layer of the substrate, where each light emitting structure has an active area parallel to the surface and laterally terminated, and where the active area of different light emitting structures is configured to directly generate a different color of light. The device also includes a p-doped layer disposed over the active area of each light emitting structure and made of a p-doped material that includes GaN. The device may be part of a light field display and may be connected to a backplane of the light field display.

Abstract: A dual-optical fusion laser rangefinder includes: a square housing, an optical core assembly, a protective lens, a touch control display module and a button control board. The optical core assembly and button control board are disposed in the square housing. The protective lens configured to transmit emitted and received lights is located at a front end of the square housing and corresponds to the optical core assembly. The touch control display module is disposed on the square housing and is connected to the button control board. The button control board is in control connection with the optical core assembly. The optical core assembly includes a phase laser ranging optical path unit and a pulse laser ranging optical path unit. The rangefinder can measure distances from 0.2 m to 5000 m and ensure that accuracy reaches the millimeter level within 200 m by integrating pulse laser ranging and phase laser ranging optics.

Abstract: A microneedle patch for enhancing accumulation of PpIX in a solid tumor and a preparation method therefor. The method includes steps of: dissolving albumin into Dubos medium, taking the albumin as a template, adding CuCl2 and CaCl2 for mineralization to obtain CCP nanoparticles; loading CAT and 5-ALA onto a surface of the CCP nanoparticles by a one-step carbodiimide coupling method and an electrostatic-adsorption method, respectively, to obtain CCPCA nanoparticles; loading the CCPCA nanoparticles and microneedle-matrix solution into a microneedle mold, after vacuum drying and demolding, obtaining the microneedle patch for enhancing accumulation of PpIX in a solid tumor.

Abstract: A method and system for optimizing an aircraft heading for an intercept of a flight plan has been developed. The method includes activating a flight plan intercept advisory function on a flight management system (FMS) for the aircraft when an aircraft deviates from the active flight plan of the aircraft. The flight plan intercept advisory function identifies intercept points of the active flight plan that is based on an aircraft heading that is selected by a pilot of the aircraft. The advisory function calculates predicted compliance with flight performance and operational parameters of the aircraft at each intercept point. The predicted compliance of flight performance and operational parameters of the aircraft at each intercept point are then displayed to the pilot of the aircraft.

Abstract: A display device based on micro light emitting diodes (microLEDs) includes a plurality of chiplets. Each chiplet includes one or more raxels, each raxel including a plurality of microLEDs supported on a substrate. The chiplet also includes a micro integrated circuit (microIC) electronically connected with the one or more raxels. MicroIC includes a plurality of interconnects supported on a backplane such that, when connected with the raxel, microIC may be used to electrically drive each one of the MicroLED of the raxel. In an embodiment, a plurality of chiplets are disposed on a display substrate to for an auto-view horizontal parallax only 3D display.

Abstract: Systems and methods are provided for displaying roll rate on a vertical take-off and landing (VTOL) aircraft display. Aircraft roll data is received from at least one geospatial sensor of the VTOL aircraft. A roll rate scale associated with a desirable roll rate range of the VTOL aircraft is generated. An aircraft roll rate of the VTOL aircraft is determined based on the aircraft roll data. The VTOL aircraft display, including a graphical representation of the roll rate scale and the aircraft roll rate with respect to the roll rate scale, is generated for display on the display device.

Abstract: A method for building a coke own includes steps of building an oven body building three-dimensional control network, and building a coke side or machine side refractory brick receiving platform; based on the three-dimensional control network and the refractory brick receiving platform, marking out a laying position of each layer of refractory bricks layer by layer, arranging the refractory bricks required by laying of each layer by layer, laying the refractory bricks layer by layer according to the marking and the arrangement, jointing the laid refractory bricks layer by layer, cleaning the jointed refractory bricks layer by layer, and checking and accepting the cleaned refractory bricks layer by layer. In this method, quality control is carried out on coke oven body masonry on the whole through six dimensions.

Abstract: Provided are a cyclic peptide compound simulating a natural product structure and a method for preparation thereof. The method is: the compound of formula I, a divalent palladium catalyst, and a silver salt undergoing an intramolecular arylation in a solvent under heating and stirring to construct a cyclic peptide, to generate the compound of formula II, in which the arylation sites are diverse, and can be extended to the side chain ?-position methyl or methylene of the majority hydrophobic amino acids to perform intramolecular arylation, thus overcoming the previous defect of the restriction of the types of selectable amino acids, and effectively constructing a novel aromatic ring-supported cyclic peptide compound. The aromatic ring support structure forms a novel 3D structure similar to a natural product, and provide a very favorable support for the subsequent construction of a cyclic peptide molecular library and high-throughput drug screening.

Abstract: The disclosure describes various aspects of monolithic integration of different light emitting structures on a same substrate. In an aspect, a device for light generation is described having a substrate with one or more buffer layers made a material that includes GaN. The device also includes light emitting structures, which are epitaxially grown on a same surface of a top buffer layer of the substrate, where each light emitting structure has an active area parallel to the surface and laterally terminated, and where the active area of different light emitting structures is configured to directly generate a different color of light. The device also includes a p-doped layer disposed over the active area of each light emitting structure and made of a p-doped material that includes GaN. The device may be part of a light field display and may be connected to a backplane of the light field display.

Abstract: A method and system for dynamically representing the separation for air traffic has been developed. First, air traffic is detected which requires maintenance of a separation distance from an ownship aircraft. The ground speed of the ownship, the ground speed of the air traffic and the current separation distance is determined. A predicted separation distance is calculated following a specific time interval. The predicted separation distance between the air traffic and the ownship is based on a differential in ground speed between the air traffic and the ownship and the specific time interval. The location of the air traffic, the separation distance and the predicted separation distance are all shown on a graphical display onboard the ownship. The separation distance and the predicted separation distance are represented on a non-linear scale on the graphical display.

Abstract: A bidirectional laser rangefinder includes: a housing assembly; and a bracket assembly, a connecting plate, a first laser emitter, and a second laser emitter disposed in the housing assembly; the bracket assembly includes a first bracket and a second bracket disposed in a mirror image manner along a length direction of the bidirectional laser rangefinder; the first and second laser emitters are disposed on the first and second brackets respectively in a mirror image manner along the length direction of the bidirectional laser rangefinder; upper portions of the first and second brackets are connected to the connecting plate; and widths of the first and second brackets as well as the connecting plate are same as an internal diameter of the housing assembly for clamping. Therefore, a split type laser emitter can be coaxial and measurement precision is improved, which is simple to produce and convenient to assemble.

Abstract: A light-emitting diode (LED) structure includes an active region that has at least one aluminum-containing quantum well (QW) stack that emits light from the LED structure when activated. The LED structure exhibits a modified internal quantum efficiency value, which is higher than a LED structure that does not include aluminum within a QW stack. The LED structure also exhibits a modified peak wavelength, which is longer than an unmodified peak wavelength of the unmodified LED structure.

Abstract: A three-laser phase distance measurer is provided. The three-laser phase distance measurer includes a main control device, a laser emitting device, and a laser receiving-processing device. The laser emitting device includes an outer light path focusing device, a visible light path focusing-emitting device, and a first optical filter device. The outer light path focusing device and the visible light path focusing-emitting device are electrically connected to the main control device. The outer light path focusing-emitting device and the visible light path focusing-emitting device are adjacent to each other and arranged side by side. The outer light path focusing-emitting device and the visible light path focusing-emitting device are arranged along a same direction. The laser receiving-processing device includes a second optical filter device, a receiver, an inner light path focusing-emitting device, and a bracket device.

Abstract: A controller for selectively displaying information from raster charts is disclosed. The controller is configured to: retrieve raster data; assign a different priority level to each of a plurality of types of raster data; cause raster data having a predetermined priority level to be displayed with first augmentation information and prevent from being displayed raster data not having the first predetermined priority level, wherein the first augmentation information comprises database data retrieved from a database and is assigned a first predetermined augmentation information priority level; generate a hidden layer of second augmentation information comprising database data from the database that is correlated to a geographical location of the displayed raster data and assigned a second predetermined augmentation information priority level; and cause the hidden layer of second augmentation information to be displayed over a portion of the displayed raster data when the geographical location is selected.

Abstract: Systems and methods are provided for indicating wake turbulence on an avionic display. The system comprises a display device that is onboard an aircraft and a controller in communication with the display device. The controller configured to, by a processor: receive data that includes information relating to a wake turbulence generated by another aircraft, determine a location on a runway of the wake turbulence based on the received data, and render a visual element on a display device onboard the aircraft that is in communication with the controller that is configured to display information relating the determined location on the runway of the wake turbulence, wherein the information is displayed in relation to a takeoff environment of the aircraft.

Abstract: Systems and methods are provided for in-air traffic tracking onboard an ownship. The system includes a display device, a sensor system configured to sense a sensed three-dimensional (3D) position of a target aircraft, a communication system configured to receive in-air traffic position data from an external source that includes a tracked 3D position of the target aircraft, and an in-air traffic tracking system that includes a controller configured to, by a processor: determine a predicted 3D position of the target aircraft by adjusting the tracked 3D position with compensation parameters, wherein the compensation parameters are determined based on a trained machine learning, determine a real-time 3D position of the target aircraft based on the sensed 3D position and/or the predicted 3D position, and render a tracking icon on the display device that indicates the real-time 3D position of the target aircraft.

Abstract: A backplane for controlling a display is disclosed. The backplane includes a plurality of tiles formed into an array. Each of the plurality of tiles includes a plurality of complementary metal-oxide-semiconductor backplane dies. Edges of the backplane dies that form a perimeter of the array include electrical connections that direct electrical signals to at least one of the CMOS backplane dies. A display assembly is also disclosed wherein the display assembly includes a backplane having an array of tiles. Each tile includes a plurality of electrically coupled CMOS backplane dies, where edges of the tiles that form an outer perimeter of the array include electrical connections directing electrical signals to one or more of the plurality of CMOS backplane dies. The display assembly further includes at least one light emitting diode array electrically coupled with at least one tile.