A collision avoidance system for aggregating and processing data when an aircraft is on or near the ground. The collision avoidance system includes a data input module configured to obtain object data and contextual data from a plurality of aircraft systems. The collision avoidance system further includes a processor configured to combine the object data into an aggregated list of detected objects, and label the aggregated list of detected objects using the contextual data to form a contextualised list of detected objects for use in determining collision avoidance. The collision avoidance system further includes a data output module configured to output the contextualised list of detected objects to a set of output systems.
An aircraft-based system for providing forward-looking terrain profiling and downward-looking altimetry via a single active electronically scanned array (AESA) orients the AESA through a sequence of desired directions, e.g., according to a predetermined scan pattern. At each desired direction, the AESA scans for ground-based targets, determining a range and Doppler velocity to each detected target. The AESA additionally orients downward, e.g., during a dedicated altimetry frame and with the assistance of inertial sensors to determine the orientation of the AESA, to scan terrain directly below the aircraft and provide a precise estimate of the altitude of the aircraft. Based on the determined ranges and velocities, the radar system determines a pointing angle and vertical/horizontal distances between the aircraft and each identified ground-based target.
G01S 13/935 - Radar ou systèmes analogues, spécialement adaptés pour des applications spécifiques pour prévenir les collisions d'aéronefs ou d'engins spatiaux pour éviter les impacts avec le sol
An ESA includes radiating elements having a normal mode radiating element and a superimposed end-fire mode radiating element. The combined normal mode radiating element and and-fire mode radiating element attenuators or variable gain amplifiers for amplitude adjustment, phase shifting, and time delay circuitry and algorithms to drive the normal mode radiating element and end-fire mode radiating element simultaneously to produce radiation patterns that constructively interfere. Alternatively, the radiating elements are fed by a radio frequency (RF) feed and switching integrated circuitry timed to drive the normal mode radiating element and end-fire mode radiating element to effectively produce hemispherical radiation patterns as a function or time/scan angle.
H01Q 5/30 - Dispositions permettant un fonctionnement sur différentes gammes d’ondes
H01Q 3/24 - Dispositifs pour changer ou faire varier l'orientation ou la forme du diagramme de directivité des ondes rayonnées par une antenne ou un système d'antenne faisant varier l'orientation, par commutation de l'énergie fournie, d'un élément actif rayonnant à un autre, p. ex. pour commutation du lobe
A computer implemented method for detecting timing faults during execution of a task having an estimated worst case execution time (WCET). The method includes, in response to a monitoring interrupt occurring, determining the progress of the task at the interrupt and the executed time of the task up until the interrupt, determining the remaining worst case execution time (rWCET) for the task to finish its execution from the progress of the task at the point of interrupt, and if the sum of the rWCET and the run time of the task exceed the estimated WCET of the task, then detecting that a timing fault will occur.
Neutron single effect events are mitigated using gadolinium. Layers of gadolinium are fully encapsulated as part of an airborne electronic hardware, in circuit boards, in heat sinks, and as part of the device packaging. The gadolinium layers are designed to shield semiconductor chips from neutrons. Shielding the semiconductor chips from the neutrons reduces the upset rate of device packages using the semiconductor ships.
H01L 23/552 - Protection contre les radiations, p. ex. la lumière
H01L 23/367 - Refroidissement facilité par la forme du dispositif
H01L 23/498 - Connexions électriques sur des substrats isolants
H01L 25/065 - Ensembles consistant en une pluralité de dispositifs à semi-conducteurs ou d'autres dispositifs à l'état solide les dispositifs étant tous d'un type prévu dans une seule des sous-classes , , , , ou , p. ex. ensembles de diodes redresseuses les dispositifs n'ayant pas de conteneurs séparés les dispositifs étant d'un type prévu dans le groupe
H05K 1/18 - Circuits imprimés associés structurellement à des composants électriques non imprimés
6.
System and method for monitoring head-up display (HUD) for malfunction
A system includes a head-up display (HUD) system including a display; a combiner; and at least one processor communicatively coupled to at least one image sensor of at least one tracking system and to the display. The at least one processor configured to: receive image data from one or more of the at least one image sensor, wherein the image data is (i) for performing eye tracking and/or head tracking operations and (ii) for monitoring the displayed images; and detect the at least one malfunction of the HUD system.
A system and method for validating navigational aids includes a navigation solution monitor that receives sensor inputs from a plurality of onboard sensors and produces a trustworthiness metric. The navigation solution monitor updates inertial navigation units (INU) based on the sensor with the highest trustworthiness metric. The navigation solution monitor may measure the trustworthiness of each sensor against every other sensor such that the trustworthiness metric represents a deviation from other sensors.
G01C 21/16 - NavigationInstruments de navigation non prévus dans les groupes en utilisant des mesures de la vitesse ou de l'accélération exécutées à bord de l'objet navigantNavigation à l'estime en intégrant l'accélération ou la vitesse, c.-à-d. navigation par inertie
An HF mesh network node includes an Electric Field Rydberg sensor as a compact broadband HF antenna. The Electric Field Rydberg sensor ensures that the receiver has visibility of a large band of HF spectrum and can therefore receive all propagating frequencies in that band simultaneously. The system may receive control information via the Rydberg sensor to establish a direct connection with a distant node via a traditional coupler and antenna on a specific frequency. The system may include a plurality of Rydberg sensors, each specifically tuned to cover a 10 MHz range of an extended spectrum.
A supply glider is disclosed herein. The supply glider includes a body having a first end and a second end, the body being configured to be coupled to a host aircraft, a container disposed between the first end and the second end of the body, wings coupled to the body between the first end and the second end, and stabilators coupled to the body adjacent the second end.
An aircraft radar system includes an antenna, a processor, and a data storage element. The data storage element includes geolocation data of ground-based structures that are likely to produce ground clutter. Based on the location and orientation of the aircraft, the processor determines where to produce a null in the antenna beam to exclude the ground clutter. Sensors on the aircraft provide data to geolocate ground clutter inducing targets in real-time. Sensor data is collated, and potentially correlated to stored maps or other databases. A trained machine learning algorithm may receive sensor data and other inputs to identify ground clutter inducing targets, and potentially generate nulls to exclude such targets.
G01S 13/524 - Discrimination entre objets fixes et mobiles ou entre objets se déplaçant à différentes vitesses utilisant la transmission de trains discontinus d'ondes modulées par impulsions basée sur le décalage de phase ou de fréquence résultant du mouvement des objets, avec référence aux signaux transmis, p. ex. MTI cohérent
G01S 13/933 - Radar ou systèmes analogues, spécialement adaptés pour des applications spécifiques pour prévenir les collisions d'aéronefs ou d'engins spatiaux
A system is disclosed for thermal coupling and fastening of circuit card assemblies of line-replaceable units (LRUs). The LRU may include a chassis configured to house one or more circuit card assemblies. The chassis may include external coupling features configured to receive fasteners. The circuit card assembly may include a heat sink with corresponding coupling features configured to align with the external coupling features and to receive the fasteners. The chassis may include a mateable surface. The circuit card assembly may include a corresponding mateable surface configured to mate to and thermally couple with the mateable surface of the chassis. The chassis may include an electrically conducting surface and the circuit card assembly may include a corresponding electrically conducting surface.
A method for determining performance of an imaging device in real-time is disclosed. The method may include, but is not limited to, receiving a first set of images of a first calibration target positioned at a first position from one or more imaging devices, determining a first environmental condition external to the aircraft at the first position based on the received first set of images using a machine learning algorithm; receiving additional set of images of an additional calibration target positioned at an additional position from the one or more imaging devices; determining an additional environmental condition external to the aircraft at the additional position based on the received additional set of images; and determining one or more real-time calibration parameters for the one or more imaging devices based on at least one of the determined first environmental condition and the determined additional environment condition.
H04N 23/13 - Caméras ou modules de caméras comprenant des capteurs d'images électroniquesLeur commande pour générer des signaux d'image à partir de différentes longueurs d'onde avec plusieurs capteurs
G01W 1/18 - Test ou étalonnage des appareils météorologiques
H04N 23/60 - Commande des caméras ou des modules de caméras
H04N 23/90 - Agencement de caméras ou de modules de caméras, p. ex. de plusieurs caméras dans des studios de télévision ou des stades de sport
H04N 23/951 - Systèmes de photographie numérique, p. ex. systèmes d'imagerie par champ lumineux en utilisant plusieurs images pour influencer la résolution, la fréquence d'images ou le rapport de cadre
13.
PASSIVE HEAD AND NECK PROTECTION PULL HANDLE INITIATION
An ejection system is disclosed herein. The ejection system includes a seat having a seat bucket and a seat back, a passive head and neck protection device coupled to the seat back, and an ejection initiation system. The ejection initiation system includes a pull handle coupled to the seat bucket, a first connector having a first end coupled to the pull handle, an ejection sequence initiation device configured to initiate an ejection sequence, a passive head and neck protection mechanism configured to activate the passive head and neck protection device, and an ejection pull connector having a first end and a second end, the second end coupled to the ejection sequence initiation device and to the passive head and neck protection mechanism.
A method (20) for calculating lateral avoidance trajectories for an aircraft (11). The method includes: obtaining data indicative of current aircraft position, current track, current roll, current airspeed, current vertical speed, current altitude, and maximum achievable roll of the aircraft; calculating a current trajectory of the aircraft; and calculating a left trajectory and right trajectory of the aircraft corresponding to the aircraft turning left/right at the maximum achievable roll from the current aircraft position. The method also includes obtaining local terrain elevation grid data; determining intersections between the local terrain elevation grid, and each of the current trajectory, left trajectory, and right trajectory; and providing an indication, of any intersections between the local terrain elevation grid, and each of the trajectories.
A system for controlling operation of unmanned assets. The system includes a graphical user interface displaying a map. The graphical user interface accepts graphical inputs drawn on the map. The system also includes a calculation unit having an input interpretation module that recognizes the graphical inputs and translates the graphical inputs into tasks and/or commands. The calculation unit also includes an operation planning module that generates operation instructions based on the tasks and/or commands; and a journey planning module that generates a journey plan for the unmanned assets based on the operation instructions. The system also includes a communications module that communicates with the unmanned assets to instruct the unmanned assets to operate according to the generated journey plan.
A printed circuit board “PCB” comprising a coaxial-like connection (210) is described herein. The coaxial-like connection (210) is configured to transmit a radio frequency signal or signals. The PCB can be used in combination with an antenna.
A system may include at least one processor configured to: obtain a trained neural network (NN); obtain or calculate at least one average feature information associated with the trained NN, each of the at least one average feature information including a given average feature information summarizing in-class statistics that each layer of the trained NN uses for a given class; receive an incoming observation influencing a given layer; calculate a corresponding feature information of the incoming observation, the corresponding feature information summarizing statistics of the incoming observation for the given layer; classify the incoming observation as being in the given class; calculate a distance score associated with a distance between the corresponding feature information of the incoming observation and the given average feature information; determine the incoming observation is an out-of-distribution (OOD) sample; and output an alert indicating the incoming observation is OOD and/or discard the incoming observation's classification.
G06V 10/82 - Dispositions pour la reconnaissance ou la compréhension d’images ou de vidéos utilisant la reconnaissance de formes ou l’apprentissage automatique utilisant les réseaux neuronaux
G06V 10/72 - Préparation de données, p. ex. prétraitement statistique des caractéristiques d’images ou de vidéos
G06V 10/764 - Dispositions pour la reconnaissance ou la compréhension d’images ou de vidéos utilisant la reconnaissance de formes ou l’apprentissage automatique utilisant la classification, p. ex. des objets vidéo
18.
AIR GROUND COMMUNICATION METHOD FOR TRANSMITTING SAFETY MESSAGES OVER NON SAFETY INFRASTRUCTURE
There is provided a method for transmitting safety-critical data from an aircraft control domain, ACD, router to a ground system via a Virtual Safety Radio, VSR, provided by a cross-router, X-router, interface between the ACD router and one or more non-safety communication domain routers, the method comprising: determining, by the VSR, that at least one non-safety media link of at least one non-safety communication medias of the one or more non-safety communication domain routers is available for conveying safety traffic from the ACD, responsive to the determination that at least one non-safety media link is available, receiving, by a communication stack of the ACD router, an application message; and sending, via the VSR, the application message to the ground system through the at least one available non-safety media link.
H04L 67/12 - Protocoles spécialement adaptés aux environnements propriétaires ou de mise en réseau pour un usage spécial, p. ex. les réseaux médicaux, les réseaux de capteurs, les réseaux dans les véhicules ou les réseaux de mesure à distance
A hybrid cooling approach uses both conduction and convection cooling for circuit cards. The hybrid cooling approach also isolates sensitive circuitry in the circuit cards from the ambient environment. The hybrid cooling approach uses an electronic module with a heat spreader. The heat spreader is coupled to the circuit card. The heat spreader defines openings disposed at an opposite end of a connector. The openings permit a fluid to flow within a cavity defined by the heat spreader.
A system and method for projecting a scene using sub-elemental control of antenna phase center locations is disclosed. The system and method may include an antenna array configured to transmit the projected scene including a plurality of antenna phase center locations. The system and method may include a controller operatively coupled to the antenna array. The controller may be configured to determine antenna phase center location weightings corresponding to the plurality of antennas based on distances between perceived/desired lateral positions of particular antenna phase center locations and an actual lateral position of the particular antenna. The antenna phase center location weightings may be configured to shift the projected scene a shift distance that is less than an antenna pitch between the plurality of antennas.
H01Q 3/36 - Dispositifs pour changer ou faire varier l'orientation ou la forme du diagramme de directivité des ondes rayonnées par une antenne ou un système d'antenne faisant varier la phase relative ou l’amplitude relative et l’énergie d’excitation entre plusieurs éléments rayonnants actifsDispositifs pour changer ou faire varier l'orientation ou la forme du diagramme de directivité des ondes rayonnées par une antenne ou un système d'antenne faisant varier la distribution de l’énergie à travers une ouverture rayonnante faisant varier la phase par des moyens électriques avec des déphaseurs variables
In a system for establishing connectivity in a HF ALE cellular network, stations are organized to sound each channel, synchronized to every other station in the network. All stations make identical sounding transmissions using a single address, synchronized such that the differential timing within the coverage area remains within the mobile radios' delay spread capability. Synchronized soundings allow the mobile radio to consistently connect to the best available channel. The stations may be synchronized via a central control function. Alternatively, the stations may perform soundings based on a predetermined schedule. Where the propagation time to the mobile radio is known, or determinable within some threshold, the stations may apply a delay to the sounding transmissions to ensure that the sounding transmissions from each of the stations reaches the mobile radio at the same time within some acceptable margin.
An operational planning system and method for optimal assignment of resources to the completion of tasks includes a combination of software modules and customizable plugins. A resource manager assesses known resources to determine which resources are assignable to a set of tasks to be completed, and a task manager determines which tasks are available for completion and prioritizes the valid tasks by resolving task dependencies. Customizable plugins determine cost factors for assigning each valid resource to each valid task, whether valid resources should continue their current task assignments and receive new assignments. Based on the assignment cost data, the customizable plugins ultimately determine an optimal assignment of valid resources to valid tasks (e.g., optimal in the sense of lowest cost and/or other desirable factors).
A system and method for correlating a received signal is disclosed. The system may include an antenna configured to receive the received signal. The system may also include a controller. The controller may include a field programmable gate array (FPGA) including a plurality of look-up tables (LUTs). The controller may also include a plurality of registers for storing and manipulating data. The plurality of registers may be coupled to the plurality of LUTs. The plurality of registers may include a known reference register, a secondary reference register, an in-phase register, and a quadrature register. Each LUT may be configured to receive Boolean inputs from the known reference register, the secondary reference register, the in-phase register, and the quadrature register and to output correlation results based on the Boolean inputs.
A method of reconstructing an image. The method includes performing panoptic segmentation of the image and performing instance segmentation of the image. The method further includes performing recurring image inpainting of the image. The recurring image inpainting of the image includes applying a first mask corresponding to the first object to the image, inpainting the first mask to form a partially reconstructed image, applying a second mask corresponding to the second object to the partially reconstructed image, and inpainting the second mask.
G06V 10/26 - Segmentation de formes dans le champ d’imageDécoupage ou fusion d’éléments d’image visant à établir la région de motif, p. ex. techniques de regroupementDétection d’occlusion
G06T 5/77 - RetoucheRestaurationSuppression des rayures
G06V 10/764 - Dispositions pour la reconnaissance ou la compréhension d’images ou de vidéos utilisant la reconnaissance de formes ou l’apprentissage automatique utilisant la classification, p. ex. des objets vidéo
G06V 10/82 - Dispositions pour la reconnaissance ou la compréhension d’images ou de vidéos utilisant la reconnaissance de formes ou l’apprentissage automatique utilisant les réseaux neuronaux
G06V 20/17 - Scènes terrestres transmises par des avions ou des drones
A system is disclosed herein, including a cushion including a plurality of tactors and a plurality of air bladders disposed adjacent the plurality of tactors, a pump assembly operably connected to the plurality of bladders, a processor, and a memory operatively coupled to the processor. The memory includes instructions stored thereon that, when executed by the processor, cause the processor to determine an inflation sequence for the plurality of air bladders, determine a deflation sequence for the plurality of air bladders, output commands to the pump assembly corresponding to the inflation sequence and the deflation sequence, and output vibrate commands to the plurality of tactors.
An enhanced vision system (EVS) is integrated with a heads-up display (HUD). The EVS generates image of an external scene. The EVS generates the images without repeatedly generating the images when a mode of the HUD changes. The EVS includes an expanded interface, where inputs from the HUD are used in the internal processing of the EVS. The HUD then displays information in a graphical and alphanumeric format. The information can include an enhanced vision image from the EVS and/or a synthetic vision image from a synthetic vision system (SVS). The enhanced vision image can be merged with a synthetic vision image to provide a combined vision image.
G06T 5/50 - Amélioration ou restauration d'image utilisant plusieurs images, p. ex. moyenne ou soustraction
B64D 43/00 - Aménagements ou adaptations des instruments
G06T 5/10 - Amélioration ou restauration d'image utilisant le filtrage dans le domaine non spatial
H04N 23/80 - Chaînes de traitement de la caméraLeurs composants
27.
SYSTEM AND METHOD TO GENERATE AND DISPLAY RUNWAY OVERRUN AWARENESS AND ALERTING SYSTEM (ROAAS) IMAGE DEPICTING CURRENT RUNWAY DISPLACED THRESHOLD VALUE AND CURRENT LANDING DISTANCE AVAILABLE VALUE
A system may include a display and at least one processor. The at least one processor may be configured to: obtain a Notice to Air Mission (NOTAM); extract information from the NOTAM, the information including information of a runway displaced threshold of the runway and/or a landing distance available on the runway; generate a NOTAM file including the information; update runway overrun awareness and alerting system (ROAAS) data to include a current runway displaced threshold value and a current landing distance available value based on the information of the NOTAM file; generate a ROAAS image, wherein the ROAAS image graphically and/or textually depicts a view indicative of the current runway displaced threshold value and the current landing distance available value; and output the ROAAS image to the display.
G08G 5/02 - Aides pour l'atterrissage automatique, c. à d. systèmes dans lesquels les données des vols d'avions arrivant sont traitées de façon à fournir les données d'atterrissage
A system may be configured to display a view of an airport moving map (AMM) depicting a location of an aircraft relative to a runway, the runway, a maximum runway overrun awareness and alerting system (ROAAS) model distance (RMD) indicator on the runway, a nominal model distance (NMD) indicator on the runway, and a ROAAS runway end indicator.
G08G 5/02 - Aides pour l'atterrissage automatique, c. à d. systèmes dans lesquels les données des vols d'avions arrivant sont traitées de façon à fournir les données d'atterrissage
A system may include at least one processor configured to: obtain data of an aircraft, the data including and/or associated a flight path vector (FPV) and/or a flight path predictor (FPP); obtain image sensor data output; identify features associated with a runway; determine that the identified features are indicative of the runway; determine a touch down zone on the runway; determine whether the FPV and/or the FPP is in the touch down zone when the aircraft is at a decision altitude and/or is predicted to be in the touch down zone when the aircraft will be at the decision altitude; and (i) output a notification to proceed with a landing procedure, (ii) perform an operation configured to cause the aircraft to proceed with the landing procedure, (iii) output a notification to perform a go-around procedure, and/or (iv) perform an operation configured to cause the aircraft to perform the go-around procedure.
A control head for a modular control unit of a urinary relief system is disclosed herein. The control head includes a pressurized gas source input, a toggle configured to activate a pressurized gas source coupled to the pressurized gas source input, a first connector fluidly coupled to the pressurized gas source input and configured to allow a first gas from the pressurized gas source input to flow through the control head, and a second connector fluidly coupled to the first connector and configured to allow a second gas to pass through the control head.
A61F 5/453 - Réceptacles génitaux pour recueillir l'urine ou d'autres sécrétions des organes masculins
A61F 5/44 - Dispositifs portés par le patient pour recueillir l'urine, les selles, les menstrues ou d'autres sécrétionsDispositifs de colostomie
A61M 1/00 - Dispositifs de succion ou de pompage à usage médicalDispositifs pour retirer, traiter ou transporter les liquides du corpsSystèmes de drainage
Autonomous systems increase the robustness and safety of current aircraft and to support simplified vehicle, reduced crew, and single pilot operations. The autonomous systems aid air crews in their handling of non-normal, high workload, aircraft upset scenarios. The upset scenarios include the recovery from attitudes outside of the normal operating envelope that even the most robust automatic flight control systems currently in service today do not support.
A method for provisioning a microelectronic (ME) component or device for non-bypassable, unclonable electronic device fingerprinting includes receiving an initialization vector from a provisioning device. A physically unclonable function (PUF) incorporated into the ME device (and unique to that ME device) provides a unique device bitstream. The device bitstream and initialization vector are cryptographically hashed to generate an electronic device fingerprint recordable to non-volatile memory onboard the ME device, which can be used for subsequent verification that the ME device is not counterfeited or compromised.
G06F 21/73 - Protection de composants spécifiques internes ou périphériques, où la protection d'un composant mène à la protection de tout le calculateur pour assurer la sécurité du calcul ou du traitement de l’information par création ou détermination de l’identification de la machine, p. ex. numéros de série
H04L 9/06 - Dispositions pour les communications secrètes ou protégéesProtocoles réseaux de sécurité l'appareil de chiffrement utilisant des registres à décalage ou des mémoires pour le codage par blocs, p. ex. système DES
H04L 9/32 - Dispositions pour les communications secrètes ou protégéesProtocoles réseaux de sécurité comprenant des moyens pour vérifier l'identité ou l'autorisation d'un utilisateur du système
33.
SYSTEM FOR GESTURE RECOGNITION BY A REMOTE TOUCH-SENSITIVE DISPLAY
A remote avionics display device connected to a source graphics generator device receives image data from the source device and presents an avionics display via a touch-sensitive display surface. The avionics display includes a set of display windows, each display window having a size and function defined by window context data. Touch sensors detect user contact points on the display surface. The remote ADD translates the sensed contact points into potential command/control gestures by correlating the contact points with window context data to determine which display window each contact is located and to which gesture each contact or set of contacts corresponds based on the window context data and current touch data structures for the appropriate display window. The remote ADD sends sensed contact points and the corresponding potential gesture data back to the source graphics generator.
G06F 3/04883 - Techniques d’interaction fondées sur les interfaces utilisateur graphiques [GUI] utilisant des caractéristiques spécifiques fournies par le périphérique d’entrée, p. ex. des fonctions commandées par la rotation d’une souris à deux capteurs, ou par la nature du périphérique d’entrée, p. ex. des gestes en fonction de la pression exercée enregistrée par une tablette numérique utilisant un écran tactile ou une tablette numérique, p. ex. entrée de commandes par des tracés gestuels pour l’entrée de données par calligraphie, p. ex. sous forme de gestes ou de texte
34.
Attention redirection within AR/XR immersive environments
A system and method for attention redirection is disclosed. The system may include a display, an environment imaging sensor configured to receive environment images comprising elements of an environment, a user state sensor configured to receive user images comprising a user gaze, and a controller. The controller may be configured to execute program instructions to receive environment images, identify elements and their identities and locations, receive user images comprising the user gaze, track the user gaze direction, determine salience values associated with the elements, and direct a focus adjustment of at least one region of the display based on the salience values.
G09G 5/00 - Dispositions ou circuits de commande de l'affichage communs à l'affichage utilisant des tubes à rayons cathodiques et à l'affichage utilisant d'autres moyens de visualisation
G06F 3/01 - Dispositions d'entrée ou dispositions d'entrée et de sortie combinées pour l'interaction entre l'utilisateur et le calculateur
G06V 10/46 - Descripteurs pour la forme, descripteurs liés au contour ou aux points, p. ex. transformation de caractéristiques visuelles invariante à l’échelle [SIFT] ou sacs de mots [BoW]Caractéristiques régionales saillantes
G09B 9/30 - Simulation de vue à partir d'un aéronef
35.
SYSTEM AND METHOD FOR ROUTING AIRCRAT SENSOR TREND DATA TO OFFBOARD DATACENTER FOR ANALYTICS
A system may include an aircraft sensor and a processor onboard the aircraft. The processor may be configured to: obtain sensor data; obtain a model; based at least on the sensor data and the model, infer trend associated with the sensor data; determine that the trend is to be communicated to an offboard destination; packetize the trend as a packet; tag the packet with information associated with one of at least two priority levels; determine at least part of a route that said tagged packet is to be communicated along based at least on a priority level associated with said tagged packet; and output said tagged packet to an electromagnetic (EM) emitter for communication along said determined at least part of the route.
A system may include a circular parasitic array assembly. The circular parasitic array assembly may include a first circular parasitic array configured to at least one of transmit or receive over a first bandwidth, the first circular parasitic array defined by a physical cylindrical volume. The circular parasitic array assembly may further include at least one positioned circular parasitic array including a first positioned circular parasitic array, each of the at least one positioned circular parasitic array positioned at least one of within the physical cylindrical volume of the first circular parasitic array or above the physical cylindrical volume of the first circular parasitic array, wherein the first positioned circular parasitic array is configured to at least one of transmit or receive over a second bandwidth, the second bandwidth being a higher frequency bandwidth than the first bandwidth.
H01Q 5/378 - Combinaison d’éléments alimentés et d’éléments passifs
H01Q 3/24 - Dispositifs pour changer ou faire varier l'orientation ou la forme du diagramme de directivité des ondes rayonnées par une antenne ou un système d'antenne faisant varier l'orientation, par commutation de l'énergie fournie, d'un élément actif rayonnant à un autre, p. ex. pour commutation du lobe
37.
SYSTEM AND METHOD FOR CALIBRATING TRANSMIT ANTENNA ARRAY
A system may include a digital beam forming (DBF) antenna array including antenna radiating elements including a first and second antenna radiating elements. The DBF antenna array may be configured to: simultaneously transmit a set of calibration signals on multiple antenna radiating elements, the multiple antenna radiating elements including the first and second antenna radiating elements, each calibration signal of the set of calibration signals comprising a given timing acquisition sequence and a given second sequence, the given second sequence used to measure a phase and a gain of a given antenna radiating element; transmit a first calibration signal of the set by the first antenna radiating element; transmit a second calibration signal of the set by the second antenna radiating element; and calibrate the multiple antenna radiating elements by using an estimated relative phase and an estimated relative gain for each of the multiple antenna radiating elements.
H04B 17/12 - SurveillanceTests d’émetteurs pour l’étalonnage d’antennes d’émission, p. ex. de l’amplitude ou de la phase
H01Q 3/26 - Dispositifs pour changer ou faire varier l'orientation ou la forme du diagramme de directivité des ondes rayonnées par une antenne ou un système d'antenne faisant varier la phase relative ou l’amplitude relative et l’énergie d’excitation entre plusieurs éléments rayonnants actifsDispositifs pour changer ou faire varier l'orientation ou la forme du diagramme de directivité des ondes rayonnées par une antenne ou un système d'antenne faisant varier la distribution de l’énergie à travers une ouverture rayonnante
H04B 17/21 - SurveillanceTests de récepteurs pour l’étalonnageSurveillanceTests de récepteurs pour la correction des mesures
A system may include a circular parasitic array (CPA) assembly including: a first CPA configured to at least one of transmit or receive; and a second CPA configured to at least one of transmit or receive; wherein the first CPA is configured to one of transmit or receive over a first bandwidth while the second CPA is configured to another of transmit or receive over the first bandwidth or a second bandwidth, wherein the first CPA and the second CPA are physically separated by a distance so as to provide on-frequency isolation.
An antenna includes multiple pillbox antenna structures arranged in a circle to cover the horizon. Each pillbox antenna structures includes a reflector configured to widen the resulting beam so that neighboring pillbox antenna structures produce beams that interact to more fully cover the horizon. A feed layer may include transmit/receive modules that are configured to apply amplitude and phase modulations to input signals for each pillbox antenna structure. Amplitude and phase modulations enable constructive and destructive interference between neighboring pillbox antenna structures to enhance the resulting beam or create nulls to exclude interfering signals. Sets of pillbox antenna structures may be stacked and angularly offset to correct crossover sectors. Alternatively, or in addition, sets of pillbox antenna structures may be adapted to operate in different, distinct frequency bands.
H01Q 19/13 - Combinaisons d'éléments actifs primaires d'antennes avec des dispositifs secondaires, p. ex. avec des dispositifs quasi optiques, pour donner à une antenne une caractéristique directionnelle désirée utilisant des surfaces réfléchissantes où les surfaces sont concaves la source rayonnante primaire étant un élément rayonnant unique, p. ex. un dipôle, une fente, une terminaison de guide d'onde
H01Q 3/20 - Dispositifs pour changer ou faire varier l'orientation ou la forme du diagramme de directivité des ondes rayonnées par une antenne ou un système d'antenne utilisant un mouvement mécanique relatif entre des éléments actifs primaires et des dispositifs secondaires des antennes ou systèmes d'antennes pour faire varier la position relative d'un élément primaire actif vis-à-vis d'un dispositif réfléchissant où l'élément primaire actif est fixe et l'élément réfléchissant est mobile
09 - Appareils et instruments scientifiques et électriques
Produits et services
computer hardware; computer hardware for displaying moving maps; electronic display interface with recorded software for electronic video informational and entertainment display and generation units for the aviation industry; computer software; computer software for displaying moving maps; computer software recorded for displaying moving maps; downloadable application for phone or tablet providing an interactive moving maps system.
A rotating plating fixture changes an orientation of the substrate throughout a plating cycle. The plating fixture changes the orientation by precisely controlling a rotation speed and position of the substrate. A stepper motor changes the orientation in response to control signals from a controller. The plating fixture includes a stepper motor fixed to a hanger, a shaft coupled to the stepper motor, a pinion gear coupled to the shaft such that rotation of the shaft by the stepper motor causes rotation of the pinion gear, and a bevel gear meshing with the pinion gear.
C25D 17/00 - Éléments structurels, ou leurs assemblages, des cellules pour revêtement électrolytique
F16H 1/14 - Transmissions à engrenages pour transmettre un mouvement rotatif sans engrenages à mouvement orbital comportant uniquement deux organes engrenés dont les axes ne sont pas parallèles comportant uniquement des engrenages coniques
F16H 57/021 - Structures de support d'arbres, p. ex. parois de séparation, orifices de logement de paliers, parois de carter ou couvercles avec paliers
F16H 57/032 - Boîtes de vitessesMontage de la transmission à l'intérieur caractérisés par les matériaux utilisés
42.
EYE TRACKING, FACIAL EXPRESSIONS, SPEECH, AND INTONATION FOR COLLECTIVE ENGAGEMENT ASSESSMENT
A team monitoring system receives data for determining user engagement for each team member. A team engagement metric is determined for the entire team based on individual user engagement correlated to discreet portions of a task. User engagement may be determined based on arm/hand positions, gaze and pupil dynamics, and voice intonation. Individual user engagement is weighted according to a task priority for that individual user at the time. The system determines a team composition based on individual user engagement during a task and team engagement during the task; even where the users have not engaged as a team during the task.
G06Q 10/0639 - Analyse des performances des employésAnalyse des performances des opérations d’une entreprise ou d’une organisation
G06V 10/82 - Dispositions pour la reconnaissance ou la compréhension d’images ou de vidéos utilisant la reconnaissance de formes ou l’apprentissage automatique utilisant les réseaux neuronaux
G06V 20/40 - ScènesÉléments spécifiques à la scène dans le contenu vidéo
43.
GROUND CLUTTER SUPPRESSION AND RUNWAY IMAGING VIA RADAR GROUND MAPPING
A radar system includes an AESA and at least one ground mapping linear array that operate on a separate receive channel and send I/Q digital terrain mapping data to a radar processing unit. The linear arrays provide constant ground mapping. The AESA may have more than one panel. Panels may be arranged as a chevron with the linear arrays disposed at the periphery. The AESA and linear arrays may be configured as a radar interferometer for track location and/or geolocation. The linear arrays may be configured as near field probes for insitu calibration.
G01S 13/90 - Radar ou systèmes analogues, spécialement adaptés pour des applications spécifiques pour la cartographie ou la représentation utilisant des techniques d'antenne synthétique
G01S 7/03 - Détails de sous-ensembles HF spécialement adaptés à ceux-ci, p. ex. communs à l'émetteur et au récepteur
44.
NARX ARCHITECTURE FOR TASK CONTENTION MODELS USING TIME-SERIES AND FINE-GRAIN INSTRUMENTATION FOR MPSoCs
There is provided a computer-implemented method of predicting a timeseries of time delays resulting from contention between tasks running in parallel on a multi-processor system using a trained Machine Learning based Task Contention Model, ML based TCM. The method comprises: executing a plurality of actual execution tasks on the multi-processor system in isolation, and for each task and during execution of the respective task, capturing a timeseries comprising a plurality of uWindows by capturing a plurality of snapshots, each snapshot comprising an array of performance monitoring counters, PMCs, since the previous snapshot, and the time since the previous snapshot. The method also includes inferring, from a time-agnostic ML based regressor, a predicted contention delay for the first uWindow of the timeseries when two or more of the plurality of actual execution tasks are executed on parallel on the multi-processor system given the first captured snapshot for each of the tasks to be completed in parallel. The method further includes inferring, from a Non-linear AutoRegressor with exogenous inputs, NARX, predicted contention delays for each subsequent uWindow of the timeseries based on the respective captured snapshot, and the predicted values for the previous time periods fed back into the NARX.
A pilot monitoring system receives data of a pilot's pose such as arm/hand positions and eyes to detect their gaze and pupil dynamics, coupled with knowledge about their current task to detect what a pilot is paying attention to, and temporally predict what they may do next. The system may use interactions between the pilot and the instrumentation to estimate a probability distribution of the next intention of the pilot. Such probability distribution may be used subsequently to evaluate the performance or training effectiveness and readiness of the pilot. The system determine data that will be necessary for a later pilot action based on the probability distribution, and compile that data from avionics systems for later display.
An ESA antenna includes a layer of filters between the layer of radiating elements and the ground layer. The filter layer obviates certain post processing steps. The filters define a passband at the operating range of the antenna and a stopband defined to prevent crosstalk or reduce known external interference. Each filter includes alternating cells of a resonator cell formed by two split ring resonators and a resonator cell formed by a complementary split ring resonator and a complementary patch/stub. A particular implementation of the filter defines an operating range around 23 gigahertz with a passband to stopband transition of less than 500 megahertz. Vias may connect the filter layer to a surface component layer with beamforming integrated circuits, bypassing the routing layer.
H01Q 3/34 - Dispositifs pour changer ou faire varier l'orientation ou la forme du diagramme de directivité des ondes rayonnées par une antenne ou un système d'antenne faisant varier la phase relative ou l’amplitude relative et l’énergie d’excitation entre plusieurs éléments rayonnants actifsDispositifs pour changer ou faire varier l'orientation ou la forme du diagramme de directivité des ondes rayonnées par une antenne ou un système d'antenne faisant varier la distribution de l’énergie à travers une ouverture rayonnante faisant varier la phase par des moyens électriques
H03H 1/00 - Détails de réalisation des réseaux d'impédances dont le mode de fonctionnement électrique n'est pas spécifié ou est applicable à plus d'un type de réseau
A display includes a split night visions imaging system (NVIS) filter, including a first and second interference filter. The first interference filter is disposed between a backlight and a diffuser of the display. The second interference filter is disposed between the diffuser and an LCD stack of the display. A cutoff wavelength of the second interference filter is between cutoff wavelengths of the first interference filter.
A network is described. The network is a peer-to-peer network of nodes. The nodes maintain a distributed ledger. The distributed ledger includes a list of transactions. The list of transactions includes various transactions for maintaining a decentralized root store between the nodes. The decentralized root store includes a list of certificate authorities which are trusted by the nodes in the network. The root certificates may be retrieved from the distributed ledger, validated, and then used to access the certificate authorities.
H04L 29/06 - Commande de la communication; Traitement de la communication caractérisés par un protocole
H04L 9/30 - Clé publique, c.-à-d. l'algorithme de chiffrement étant impossible à inverser par ordinateur et les clés de chiffrement des utilisateurs n'exigeant pas le secret
An optical device includes an electrochromic layer including a single electrochromic region and electronic drivers. The optical device includes a controller for controlling the electronic drivers to change the light transmission of the electrochromic region by applying different voltages to electrodes contacting the electrochromic region. The optical device includes a light intensity sensor for detecting light intensity of regions of a two-dimensional scene, the regions of the scene corresponding to regions of the electrochromic region. The electronic drivers are caused by the controller to apply different voltages to the electrodes to set the light transmission of the regions of the electrochromic region based on detected light intensity of the regions of the scene.
A method is disclosed herein. The method includes receiving, by a processor, an ejection command for ejecting an ejection seat from an aircraft; determining, by the processor, an airspeed and an altitude of the ejection seat; responsive to the altitude of the ejection seat indicating a second mode of operation, determining, by the processor, whether the airspeed of the ejection seat is at or above a first threshold and below a second threshold; and responsive to the airspeed of the ejection seat being at or above the first threshold and below the second threshold: sending, by the processor, a command to deploy a drogue parachute; and, responsive to a first predetermined time period expiring, sending, by the processor, a command to deploy a main parachute and sever the drogue parachute based on a variable drogue severance delay.
An anti-fuse apparatus for enabling or disabling features associated with one or more integrated circuits (IC) set into a substrate includes a layer of low melting point dielectric material deposited above and/or between two conductive pads set into the substrate and not otherwise electrically coupled. A layer of a low melting point conductive alloy is deposited above the dielectric layer, and a layer of an energetic material deposited above the conductive alloy layer. The energetic material is connected to an ignition circuit for triggering a thermal reaction within the energetic material, removing the dielectric layer and melting the conductive alloy to electrically bridge the conductive pads, enabling or disabling features associated with the ICs (or providing tamper-proof identification strapping) without otherwise fracturing or damaging the underlying substrate or ICs set thereinto.
H01L 23/525 - Dispositions pour conduire le courant électrique à l'intérieur du dispositif pendant son fonctionnement, d'un composant à un autre comprenant des interconnexions externes formées d'une structure multicouche de couches conductrices et isolantes inséparables du corps semi-conducteur sur lequel elles ont été déposées avec des interconnexions modifiables
52.
SYSTEM AND METHOD FOR EFFICIENT DIRECTIONAL DISCOVERY OF COMMUNICATIONS TERMINALS VIA BEAM INTERLEAVING
A node of a multi-node network includes a communications interface incorporating one or more paired antenna elements wherein a transmitter (Tx) element and receiver (Rx) element are oriented in opposing directions. The node discovers and/or links to other nodes of the network by orienting each paired antenna element to transmit to other nodes in one direction and receive in the opposing direction (e.g., through a transmit and receive region, the transmit region opposite the receive region). At subsequent time intervals (e.g., alternating with the first time interval or set thereof), the Tx antenna elements transmit in directions through the initial receive region, each transmit direction interleaved between two prior receive directions, while the Rx antenna elements simultaneously attempt to receive in opposing directions through the initial transmit region, each receive direction interleaved between two prior transmit directions.
G01S 3/40 - Systèmes pour déterminer une direction ou une déviation par rapport à une direction prédéterminée utilisant le réglage d'une orientation réelle ou effective d'une caractéristique de directivité d'une antenne ou d'un système d'antenne afin d'obtenir une valeur désirée du signal venu de cette antenne ou système d'antenne, p. ex. donner un signal maximal ou minimal réglant l'orientation d'une caractéristique de directivité unique afin de produire un signal maximal ou minimal, p. ex. cadre rotatif ou système goniométrique équivalent
G01S 3/04 - Radiogoniomètres pour déterminer la direction d'où proviennent des ondes infrasonores, sonores, ultrasonores ou électromagnétiques ou des émissions de particules sans caractéristiques de direction utilisant des ondes radio Détails
The mixer-first topology of receivers do not include low-noise amplifiers (LNA) preceding the mixer. The Mixer-First topology of radio receivers utilizes a direct-conversion quadrature mixer to down convert an RF signal to baseband, where a Hilbert Transform filter is used for sideband selection. When a switching mixer is used, the mixer-first receiver is capable of extremely high dynamic range and linearity. The downfall of the mixer-first topology is poor out-of-band signal rejection. A mixer-first receiver is described which achieves third-harmonic rejection without bandpass filtering proceeding the mixer.
A system for providing maneuvering behaviors to a vehicle is disclosed. The system may include one or more controllers communicatively coupled to one or more vehicles. The one or more controllers may include one or more processors configured to execute one or more program instructions causing the one or more processors to: initiate one or more maneuver primitives in response to decision engine selection; receive a plurality of input parameters for the one or more maneuver primitives, the plurality of input parameters including one or more initialization definition input parameters, one or more goal definition input parameters, one or more navigation state input parameters, one or more design input parameters, and one or more vehicle performance envelope input parameters; and generate one or more control signals at one or more predetermined intervals of time to maneuver the one or more vehicles based on the decision engine selection.
G05D 1/00 - Commande de la position, du cap, de l'altitude ou de l'attitude des véhicules terrestres, aquatiques, aériens ou spatiaux, p. ex. utilisant des pilotes automatiques
A pitot tube restraint system is disclosed herein. The pitot tube restrain system includes an outer shaft, a pitot tube coupled to a first end of the outer shaft and extending outward from the outer shaft, a torsion spring disposed around the outer shaft, a stop pad coupled to the first end of the outer shaft, a base disposed adjacent the second end of the outer shaft, an inner shaft having disposed through the outer shaft, a first end of the inner shaft rotationally coupled to the stop pad and a second end of the inner shaft rotationally coupled to the base, a pawl disposed around the inner shaft and adjacent the second end of the outer shaft, the pawl configured to engage the second end of the outer shaft to prevent the pitot tube from rotating in a first direction, and a pawl spring disposed around the inner shaft.
Disclosed are embodiments of antenna assemblies for integration with aircraft lighting systems. The antenna assemblies in some embodiments include a ground plane, a patch antenna positioned on the ground plane, and a radome covering the patch antenna. The patch antenna and radome are configured as an annular ring for positioning around a light fixture received through a center opening through each of the ground plane, patch antenna, and radome such that the antenna assembly can mount and connect to the aircraft utilizing the light fixture aperture without the need for a separate antenna aperture.
An integrated circuit may include two processing cores. Each processing core may include: a core controller operable to execute instructions to perform processing tasks; a memory resource connected to the core controller; and a hardware accelerator module connected to the core controller. The integrated circuit may further include: a shared bus connected to the respective hardware accelerator modules of the two processing cores; and a shared memory resource connected to the shared bus; where the only communication path between the two processing cores is via the hardware accelerator modules and the shared bus.
A method for managing software application tasks being performed in a multi-core processing system, the system comprising: a management core configured to manage the allocation of processing tasks in the system; a plurality of processing cores configured to execute instructions for performing processing tasks; at least one shared resource, wherein the at least one shared resource is connected to each of the processing cores; a contention assessment module configured to monitor the amount of contention in the system; and a processing suspension module configured to cause the suspension of processing on at least one of the processing cores; wherein the method comprises: determining a criticality level of each task to be performed; allocating each task to a respective processing core of the plurality of processing cores based on the determined criticality level; assigning a contention threshold to at least one processing core of the plurality of processing cores; monitoring the amount of contention caused by the at least one processing core that has been assigned a contention threshold; and if the amount of contention caused by the at least one processing core that has been assigned a contention threshold reaches the assigned contention threshold, suspending processing on that processing core.
A communication system applies impedance matching to an antenna specific to individual samples of a transmit signal. The system samples a signal and identifies the peak frequency content of each sample. Based on the peak frequency content, the system identifies an impedance match for a given antenna that provides the greatest energy transmission. The sampled portion of the signal is delayed to accommodate processing time to determine the impedance match and control settings. Control settings may be applied via discrete digital circuitry or continuous analog circuitry.
H01Q 5/335 - Éléments rayonnants individuels ou couplés, chaque élément étant alimenté d’une façon non précisée utilisant des circuits ou des composants dont la réponse dépend de la fréquence, p. ex. des circuits bouchon ou des condensateurs au point d’alimentation, p. ex. aux fins d’adaptation d’impédance
A system-on-chip comprises a first core having a first processor architecture and a second core having a different second processor architecture. A shared bus is communicatively coupled to the cores. A shared memory is communicatively coupled to the shared bus, for storing shared data accessible by cores. A hardware comparison module is configured to compare first data, determined by one or more operations of the first core, and second data, determined by one or more operations of the second core, to detect an inconsistency between the first data and the second data, and to signal when an inconsistency is detected. A first comparison-data bus is communicatively coupled to the first core and to the comparison module, and arranged to provide the first data to the hardware comparison module. A second comparison-data bus is communicatively coupled to the second core and to the comparison module, and arranged to provide the second data to the comparison module. The first and second comparison-data buses are isolated from each other and from the shared bus.
A direct dry film (DDF) lamination method includes providing a chamber including a bladder, positioning a frame in the chamber, positioning a compound curve substrate in an interior space within the frame, and suspending, by the frame, an optically clear adhesive (OCA) sheet over the compound curve substrate. In embodiments, a top liner of the OCA sheet is scored or cut to introduce weakness imparting flexibility in the sheet corresponding to the curvature of the compound curve substrate. The method continues with evacuating the chamber, deploying the bladder, retracting the bladder, and venting the chamber. Additional steps prepare the product for further boding with a flexible film or rigid part having a matched curvature profile.
B32B 37/12 - Procédés ou dispositifs pour la stratification, p. ex. par polymérisation ou par liaison à l'aide d'ultrasons caractérisés par l'usage d'adhésifs
B32B 1/00 - Produits stratifiés ayant une forme non plane
B32B 7/12 - Liaison entre couches utilisant des adhésifs interposés ou des matériaux interposés ayant des propriétés adhésives
B32B 37/10 - Procédés ou dispositifs pour la stratification, p. ex. par polymérisation ou par liaison à l'aide d'ultrasons caractérisés par la technique de pressage, p. ex. faisant usage de l'action directe du vide ou d'un fluide sous pression
B32B 38/00 - Opérations auxiliaires liées aux procédés de stratification
62.
MICRO-SMALL FORM FACTOR (USFF) STARING RECEIVER AS A PASSIVE SENSOR
A small-scale receiver design architecture is disclosed. The receiver architecture may include an amplifier, reconfigurable filters, a downconverter assembly, a processor, and one or more risers. The one or more risers may include ball grid array (BGA) interconnects configured for electrical coupling between the front-end assembly, the downconverter assembly, and the processor. The one or more risers may be configured to provide electromagnetically shielding to the front-end assembly, the downconverter assembly, and the processor. The one or more risers may be configured to thermally couple to the front-end assembly, the downconverter assembly, and the processor. The receiver architecture may include a sequential stacking of the one or more risers, the front-end assembly, the downconverter assembly, and the processor.
H04B 1/00 - Détails des systèmes de transmission, non couverts par l'un des groupes Détails des systèmes de transmission non caractérisés par le milieu utilisé pour la transmission
H05K 7/20 - Modifications en vue de faciliter la réfrigération, l'aération ou le chauffage
63.
AESA-BASED SYNTHETIC NULLING FOR ENHANCED RADAR GROUND CLUTTER SUPPRESSION
A radar system uses multiple nulls to improve detection capabilities. Multiple radar pulses are transmitted and or received, each with a different null pattern. The returns from each pulse are averaged together to form a null window that is less noisy and potentially wider than a single null pattern. This approach can improve the signal-to-noise ratio and make it easier to detect objects of interest. The system may generate individual pulses from an AESA divided into several subarrays. Each subarray produces a pulse with a null in a different location in the radiation pattern centered about a location of interest. The contemporaneous return signals are averaged together.
A method of determining a set of landing sites for an aircraft includes retrieving a first map of the reachable area (300) surrounding the aircraft, converting data relating to a plurality of no-go zones into a second map (302), filtering the plurality of no-go zones from the first map using the second map to create a third map of potential landing sites (310), and identifying one or more feasible landing sites (312) from the third map based on one or more landing requirements of the aircraft.
G08G 5/02 - Aides pour l'atterrissage automatique, c. à d. systèmes dans lesquels les données des vols d'avions arrivant sont traitées de façon à fournir les données d'atterrissage
A combiner includes an active breakaway mechanism. The breakaway mechanism includes a biasing element to positively direct the breakaway mechanism to a safe state, and a release element. In the event of a crash, the release element disengages, and the biasing element pushes the combiner into a safe orientation. A processor and detection element may detect a crash event and actuate the release element. The biasing element may be hydraulic, a spring, a linear actuator, or the like. The release element may include a solenoid, electromagnet, spring, compressed gas, expanding gas, or the like.
An in-flight entertainment (IFE) system may include a structural panel supporting one or more aircraft seat components. The one or more aircraft seat components may include a primary IFE display and a secondary IFE display. Both the primary IFE display and the secondary IFE display may be coupled to a portion of the structural panel facing the passenger. The primary display may receive and display a plurality of in-flight related content from at least one IFE source, while the secondary display may receive and display a plurality of media content associated with a personal electronic device (PED) of the passenger. The IFE system may also include at least one controller which is in communication with at least one of the primary IFE display, the secondary IFE display, and the PED. The controller may selectively display content received from at least one of the IFE source or the PED.
A method approximates outlines of weather cells within the weather radar data using geometric shapes. The weather cells are filtered and clustered into clusters. The edges of the clusters are detected through an edge detection algorithm. Geometric shapes are fit to the edges of the clusters. The geometric shapes require significantly less bandwidth when transmitting over a communication channel, as compared to the weather radar data. The method saves the radar data with very few parameters and thus reduces the required memory for storage and required throughput for exchange.
A system collects air samples at altitude and shares data among aircraft in a network. The system includes an antenna with an antenna housing; the housing defines air inlets and outlets. While in flight, air samples are collected through the inlets, processed via sensors, and allowed to flow through to the outlet. Air quality data, including, but not limited to, contrail humidity, gas content, and particle density and size, may be transmitted to other aircraft in a network via the antenna. Air quality measurements are geolocated and correlated from different platforms at different altitudes. A data model or machine learning artificial intelligence may utilize the geolocated air quality data to make certain predictions.
A fuel quantity indicator system (FQIS) for an aircraft or other vehicle includes memory/data storage and a fuel quantity processing unit (FQPU). A neural network trained via machine learning and running on the FQPU receives fuel quantity (FQ) inputs from fuel tank sensors, e.g., tank density, fuel volume, water presence within the tank, at or near a given measurement time. The neural network additionally receives fuel flow (FF) inputs from flow sensors at the measurement time, indicating fuel flow to engines and auxiliary power units (APU) of the vehicle. Based on the FQ inputs and the FF inputs, the neural network calculates an estimated fuel quantity (EFQ) remaining, e.g., across all fuel tanks at or near a particular measurement time.
A system and method for monitoring and verification of digital gyroscopic sensors determines a primary angular velocity vector via a primary digital gyroscopic sensor triad and two or more backup angular velocity vectors via backup analog gyroscopic sensor triads. Based on additional aiding parameters, the aircraft attitude and heading reference system (AHRS) determines a primary attitude solution based on the primary angular velocity vector and one or more backup attitude solutions based on the backup angular velocity vectors. If no other faults are present with respect to the primary and backup gyroscopic sensor triads (e.g., the primary and backup triads are otherwise consistent in their measurements), and the primary attitude solution sufficiently deviates from the backup attitude solutions, the AHRS detects a solution fault in the primary gyroscopic sensor triad.
B64D 45/00 - Indicateurs ou dispositifs de protection d'aéronefs, non prévus ailleurs
B64F 5/60 - Test ou inspection des composants ou des systèmes d'aéronefs
G01C 19/00 - GyroscopesDispositifs sensibles à la rotation utilisant des masses vibrantesDispositifs sensibles à la rotation sans masse en mouvementMesure de la vitesse angulaire en utilisant les effets gyroscopiques
71.
ADAPTIVE SCHEDULER FOR LOAD BALANCING OF UNPREDICTABLE, TIME-SENSITIVE REQUESTS FOR A SHARED RESOURCE
A resource allocation system receives user requests for system resources over time. The system records factors such as number of resource requests, total usage time, etc., and preempts earlier requests in favor of later requests based on those factors. The resource allocation system tracks metrics in real-time and establishes dynamic preemption thresholds based on usage over time. Preemption thresholds may be specific to individual users.
A system and method for removing modulated interference (e.g., FSK, MSK, CW) from an input signal demodulates the input signal into a tracking bitstream via a set of phase locked loop (PLL) filters, one PLL filter for each modulated interference component (e.g., signal) known or suspected to be interfering with the input signal. Each PLL filter estimates, based on an estimated modulation frequency and center frequency associated with its target modulated interference component, a peak magnitude, phase, and updated center frequency and, based on these parameters, approximates the target interference component. Each re-created modulated interference component is subtracted from the original input signal to produce an output signal from which the known or suspected modulated interference components have been substantially removed.
A wearable device includes neuromorphic event cameras. A processor receives data streams from the event cameras and makes application specific predictions/determinations. The event cameras may be outward facing to make determinations about the environment or a specific task, inward facing to monitor the state of the user, or both. The processor may be configured as a trained neural network to receive the data streams and produce output based on predefined sets of training data. Sensors other than event cameras may supply data to the processor and neural network, including other cameras via a feature recognition process.
A cabin management system is described. The cabin management system includes a housing. The housing is configured to receive one or more modules. The modules may be detached and reattached to the housing. The modules may be rearranged to achieve a desired layout of touchscreens, audio converter, and input/output ports. The modules may include a geometry which provides a flush-mounting between the housing and the modules. The flush-mounting may prevent a passenger from accessing the cavity defined by the housing. The audio converter includes a digital-to-analog converter and an audio jack. The digital-to-analog converter converts an uncompressed digital audio signal to an analog audio signal. The audio jack receives a stereo analog signal and outputs the stereo analog signal to an audio plug.
A computer system records eye tracking data and identifies movements in the eye tracking data to determine gaze and pupil dynamics. Eye tracking data is correlated with a current task and predetermined vigilance requirements. The system determines if the user is exhibiting an appropriate level of vigilance based on the task or is becoming fixated. When fixation is detected, the system may engage in remedial action. A task flow diagram represents the operator tasks. Interactions between the user and the instrumentation are used to estimate the probability distribution of the task the user is currently conducting. The system correlates eye tracking data and physiological data such as electroencephalogram (EEG) and functional near-infrared spectroscopy (fNIRs) to determine neuroactivity. Monitoring neuroactivity reduces the probability of a false positive for fixation.
A profile for a tool implementing a unified modeling language (UML) is described. The profile extends the UML to include decision management functionality. The profile includes stereotypes and customizations which generate question elements, decision elements, alternative elements, and the like. The association between the elements permits a design engineer to review previous decisions and the rationale behind the decisions. In particular, the one of alternative elements is associated with decision element by selected alternative relationship.
A runway overrun awareness and alerting system determines a breaking distance based on aircraft capabilities, and renders a graphical depiction of that breaking distance. The graphical depiction may be separately rendered on a head-up display and a primary flight display. The system may determine both a maximum deceleration breaking distance and a nominal deceleration breaking distance. The maximum deceleration breaking distance and nominal deceleration breaking distance may be separately rendered, and may be rendered to include a visual indicator if they exceed some safety threshold.
G08G 5/02 - Aides pour l'atterrissage automatique, c. à d. systèmes dans lesquels les données des vols d'avions arrivant sont traitées de façon à fournir les données d'atterrissage
B64D 43/00 - Aménagements ou adaptations des instruments
The system may include at least one a light emitter configured to emit light over a range of wavelengths onto an environment and at least one sensor assembly. The range of wavelengths emitted by the light emitter may be of wavelengths that are above or below wavelengths used by a night vision imaging system. The sensor assembly may include an image sensor and conversion layer. The image sensor may capture images of the environment illuminated by the light emitters and sense light in a given range of wavelengths. The conversion layer may receive the emitted light and convert the emitted light to converted light with a wavelength within the given range of wavelengths associated with the image sensor. The image sensor may be further configured to receive the converted light from the conversion layer, capture an image of the light emitter and output image data associated with the captured image.
G09G 5/00 - Dispositions ou circuits de commande de l'affichage communs à l'affichage utilisant des tubes à rayons cathodiques et à l'affichage utilisant d'autres moyens de visualisation
G02B 27/00 - Systèmes ou appareils optiques non prévus dans aucun des groupes ,
H04N 23/11 - Caméras ou modules de caméras comprenant des capteurs d'images électroniquesLeur commande pour générer des signaux d'image à partir de différentes longueurs d'onde pour générer des signaux d'image à partir de longueurs d'onde de lumière visible et infrarouge
Techniques for selecting frequencies of operation are described. HF signals may land at the receiver node with power levels dependent upon the transmit frequency. The frequency with the highest power level at the receiver node may be selected when the receiver node is not subject to interfering. The receiver node may be unable to receive a desired signal if an interfering signal has a signal level which is higher than the desired signal. The transmitter node may select a frequency which has a receiver signal level which is higher than the interfering signal for the selected frequency. The receiver node may then receive the transmit signal at the selected frequency even when subject to interfering from the interferer node.
H04B 1/10 - Dispositifs associés au récepteur pour limiter ou supprimer le bruit et les interférences
H04B 1/00 - Détails des systèmes de transmission, non couverts par l'un des groupes Détails des systèmes de transmission non caractérisés par le milieu utilisé pour la transmission
A stack is described. The stack includes a rule engine. The rule engine is accessed via application programming interface (API) from any plug-in mission service. The rule engine includes rules and facts. The rules and facts are loaded separately from the API and from a cloudlet monitor. The rules and facts do not require source code updates to change. The stack is executable on processors of a node within a cloudlet. The cloudlet includes multiple of the nodes. The stack divides high-level tasks into low-level tasks which are individually executable by the nodes in the cloudlet.
Techniques for selecting frequencies of operation are described. HF signals may land at the receiver node with power levels dependent upon the transmit frequency. The frequency with the highest power level at the receiver node may be selected when the receiver node is not subject to interference. The receiver node may be unable to receive a desired signal if an interfering signal has a signal level which is higher than the desired signal. The interfering signals may have a signal level which is higher across all available frequencies. The transmitter node may determine a potential relay table with a communication link between the transmitter node and a relay node and a communication link between the relay node and the receiver node. The communication link may include link margins above the interfering signal, ensuring the links may be established. The nodes may then communicate even when subject to interference.
H04W 40/02 - Sélection d'itinéraire ou de voie de communication, p. ex. routage basé sur l'énergie disponible ou le chemin le plus court
H04W 72/0453 - Ressources du domaine fréquentiel, p. ex. porteuses dans des AMDF [FDMA]
H04W 72/541 - Critères d’affectation ou de planification des ressources sans fil sur la base de critères de qualité en utilisant le niveau d’interférence
82.
INTEGRATING INPUT AND OUTPUT CAPACITANCE WITH HIGH FREQUENCY SHUNT CAPACITANCE ON A SINGLE ADDITIVELY MANUFACTURED SUBSTRATE
A package is described. The package includes a die covered by a lid. The lid maintains a hermetic seal for the die. The package includes high frequency shunt capacitance in parallel with surface-mount capacitors. The high frequency shunt capacitance is formed by interdigital capacitors below the surface-mount capacitors. The interdigital capacitors, the surface-mount capacitors, and the die form a circuit which produces a stable output voltage. The output voltage may remain stable even when subject to noise due to energized particles in space. The package includes solder resist with openings for attaching the surface-mount capacitors to the interdigital capacitors. Advantageously, the interdigital capacitors may achieve high frequency shunt capacitance on the order of nano-farads as part of the frame geometry with minimal increase in package height.
H01L 25/16 - Ensembles consistant en une pluralité de dispositifs à semi-conducteurs ou d'autres dispositifs à l'état solide les dispositifs étant de types couverts par plusieurs des sous-classes , , , , ou , p. ex. circuit hybrides
H01L 23/498 - Connexions électriques sur des substrats isolants
H01L 23/552 - Protection contre les radiations, p. ex. la lumière
83.
SYSTEM AND METHOD FOR ENCODING MISSION CONFIGURATION AND PASSENGER EXPERIENCE DATA FOR URBAN AIR MOBILITY (UAM) PASSENGER TRANSPORT
A system and method for transporting passengers via uncrewed aircraft systems (UAS) receives passenger requests for transport between origin and destination points. Based on the request a transport plan is generated for each passenger, identifying the passenger, assigning a UAS and including a flight plan (which includes flight instructions and a communications plan for the UAS control system). Based on the transport plan one or more encoded flight plan datasets are generated. Each encoded dataset is downloadable to and displayable by the passenger's portable computing device, and scannable and decodable by reader devices at the origin and destination ports and aboard the UAS. Scanning an encoded dataset both grants the passenger access to the origin port and UAS and confirms the passenger's presence. Further, each assigned UAS downloads from the decoded flight plan data the necessary configuration data to fulfill its portion/s of the flight plan.
G05D 1/00 - Commande de la position, du cap, de l'altitude ou de l'attitude des véhicules terrestres, aquatiques, aériens ou spatiaux, p. ex. utilisant des pilotes automatiques
A system, comprising: one or more imaging devices (202) configured to collect image data of a cockpit area of an aircraft; a pilot detection module (212) configured to determine a presence of one or more pilots in the cockpit area based on the image data; and a pilot posture module (214) configured to determine three-dimensional posture of the one or more pilots based on the image data.
G06V 20/52 - Activités de surveillance ou de suivi, p. ex. pour la reconnaissance d’objets suspects
B64D 45/00 - Indicateurs ou dispositifs de protection d'aéronefs, non prévus ailleurs
G06T 7/50 - Récupération de la profondeur ou de la forme
G06T 7/73 - Détermination de la position ou de l'orientation des objets ou des caméras utilisant des procédés basés sur les caractéristiques
G06V 10/82 - Dispositions pour la reconnaissance ou la compréhension d’images ou de vidéos utilisant la reconnaissance de formes ou l’apprentissage automatique utilisant les réseaux neuronaux
G06V 40/10 - Corps d’êtres humains ou d’animaux, p. ex. occupants de véhicules automobiles ou piétonsParties du corps, p. ex. mains
G06V 40/20 - Mouvements ou comportement, p. ex. reconnaissance des gestes
G08B 21/04 - Alarmes pour assurer la sécurité des personnes réagissant à la non-activité, p. ex. de personnes âgées
85.
LANGUAGE MODELS FOR AUTOMATIC MICROBENCHMARK GENERATION
Disclosed is a method of training a language model to generate “microbenchmarks” in which the training data is specifically associated with certain microarchitecture characteristics that the “microbenchmarks” are designed for testing. Also disclosed are language models that have been trained in this manner, and the corresponding use thereof to generate “microbenchmarks”.
An autonomous agent of a team of autonomous agents (e.g., semi- or fully autonomous vehicles) includes a self-simulator incorporating a faster than real time (FTRT) processing environment for online simulation of each agent of the team. Based on the current mission status and one or more action sets determining the behaviors of the autonomous agents, the behaviors of each agent of the team are projected forward within the FTRT environment to determine mission status metrics relevant to the effectiveness of a particular action set towards optimal completion of mission objectives currently assigned to the team. Based on the mission status metrics, the self-simulator can select and provide an action set for optimized completion of mission objectives. For example, the self-simulator can recommend switching to a different preloaded action set or, in some cases, construct an optimized action set selected from multiple preloaded action sets tested in the FTRT environment.
G05D 1/00 - Commande de la position, du cap, de l'altitude ou de l'attitude des véhicules terrestres, aquatiques, aériens ou spatiaux, p. ex. utilisant des pilotes automatiques
A preselect value is sent to a primary flight display for confirmation from both pilots (i.e., from the captain and the first officer). The preselect value removes single point failure when updating the barometric altimeter pressure setting in the barometric altimeter from an uplink message from air traffic control. The preselect value is loaded with the barometric altimeter pressure setting from the uplink message. The pilots each swap the preselect value with the active barometric altimeter pressure setting on the primary flight displays. The new active barometric altimeter pressure setting is then pushed to the barometric altimeters both active barometric altimeter pressure settings match.
A system for detecting threats at an area is disclosed. The system may include a controller including one or more processors configured to execute a set of program instructions stored in a memory. The set of program instructions may be configured to cause the one or more processors to receive safe historical data of an area configured to be representative of a lack of threats, receive new data of the area from one or more nodes, compare the new data and the safe historical data to identify a difference between the new data and the safe historical data, and update a database based on the difference.
An on aircraft computer system records and analyzes biometric data to identify indicia of impaired performance, such as pilot fatigue, attention tunneling, or cognitive overload. Such impairment is identified by alterations in pilot gaze or eye movement, head movement, facial parameters, eye lid position, heart rate, breathing, or brain wave patterns. Appropriate corrective action is applied based on the type of impaired performance identified, including altering a level of automation, contacting a ground dispatcher or ground pilot, or contacting a co-pilot or other crew member. Biometric data is continuously logged and correlated with data from other avionics systems to refine formulas relating biometric data to states of alertness and crew rest procedures.
An aircraft-based system and method for automated reporting and logging of aircraft maintenance events receives flight deck effects (FDEs) with correlated maintenance messages indicating maintenance statuses (e.g., faults and/or failures) and/or Air Transport Association (ATA) classifications for each reporting aircraft system, subsystem or component. The logging system generates event messages based on each received FDE, predicting additional information based on the correlated maintenance message such as recommended maintenance actions, replacement parts or components, and/or Minimum Equipment List (MEL) actions associated with a component fault or failure. Event messages are automatically transmitted via datalink to ground-based maintenance and dispatch. Further, event messages are automatically logged to an aircraft maintenance log.
An augmented reality system in an air traffic control tower receives data from multiple airfield sensors and from local aircraft and correlates the data in space and time. Features of the airfield are rendered visually in an augmented reality headset during low visibility conditions. The augmented reality system renders visualizations of aircraft and may render data from the aircraft to coincide with the visualizations. The augmented reality system may receive data from systems within the air traffic control tower, commonly rendered on displays in the air traffic control tower and rendered such data within the augmented reality display.
A radar system including an AESA illuminates a target with a first pulse for a desired beam pointing angle (azimuth and elevation). The AESA then illuminates the target with a second pulse for the desired pointing angle, the second pulse defining a radiation pattern with a main beam in phase with the first pulse, but side lobes that are out of phase. The radar system receives return signals and combines the return signals to null the side lobes by the principle of superposition. The radar processing unit is time synced such that the pulse-pair is interpreted as a single ultra-low level side lobe return radiation pattern.
A method is disclosed herein. The method includes determining, by a processor, a first time value in response to a switch being actuated a first time by a first striker, determining, by the processor, a second time value in response to the switch being actuated a second time by a second striker, the second striker disposed a first distance from the first striker and the second time value being after the first time value, calculating, by the processor, a change in time between the first time value and the second time value, and adjusting, by the processor, a timing sequence based on the change in time.
A system may include a processor configured to: (a) obtain parameters; (b) based on the parameters, update flight-state data associated with an aircraft; (c) obtain a trained machine learning (ML) model; (d) based at least on the updated flight-state data and the trained ML model, infer a direction from a current cell for a reroute; (e) based on the inferred direction and the updated flight-state data, set the current cell and identify neighboring cells; (f) calculate an optimal next cell by using a shortest path finding (SPF) algorithm to select the optimal next cell from the neighboring cells; (g) iteratively repeat steps (d) through (f) such that the current cell is set as the optimal next cell until a goal state is reached; (h) construct a re-route using optimal cells iteratively calculated in step (f); and (i) output the re-route.
A method is disclosed herein. The method includes receiving, by a processor, a first acceleration data from an accelerometer, calculating, by the processor, a change in velocity based on the first acceleration data, the change in velocity being calculated over a first period of time, and adjusting, by the processor, a timing sequence based on the change in velocity.
G01P 15/16 - Mesure de l'accélérationMesure de la décélérationMesure des chocs, c.-à-d. d'une variation brusque de l'accélération en calculant la dérivée par rapport au temps d'un signal de vitesse mesuré
B64D 11/06 - Aménagements ou adaptations des sièges
96.
SYSTEM AND METHOD FOR ROAAS USING AI/ML MODEL TO SET AUTO BRAKE VALVE
A system may include an auto brake valve installed in an aircraft, an auto brake selector (ABS) switch communicatively coupled to the auto brake valve, and a runway overrun awareness and alerting system (ROAAS) communicatively coupled to the auto brake valve. The ABS switch may be configured to have a manual ABS switch setting to control the auto brake valve. The ROAAS may include at least one processor configured to: obtain ROAAS output data, the ROAAS output data including at least one of selected runway, runway distance remaining, runway stopping point, or runway condition; obtain a trained artificial intelligence (AI) and/or machine learning (ML) model; based at least on the ROAAS output data and the trained AI and/or ML model, infer an ABS brake setting; and set the auto brake valve in accordance with the ABS brake setting.
B60T 8/17 - Utilisation de moyens de régulation électriques ou électroniques pour la commande du freinage
B60T 8/174 - Utilisation de moyens de régulation électriques ou électroniques pour la commande du freinage caractérisées par l'utilisation de logiques particulières de commande, p. ex. de la logique floue
B60T 8/32 - Dispositions pour adapter la force de freinage sur la roue aux conditions propres au véhicule ou à l'état du sol, p. ex. par limitation ou variation de la force de freinage selon une condition de vitesse, p. ex. accélération ou décélération
A system and related method for multiple-sensitivity optical phase modulation splits an optical carrier generated by a photonic source into at least two copies and directs the copies (e.g., via optical circulators or polarization rotators) to an electro-optical (EO) phase modulator such that the phase modulator phase-modulates each optical copy according to a received radio frequency (RF) signal of interest based on characteristics distinct to each optical copy (e.g., optical path direction, signal polarization) that provide for phase modulation of each optical copy at a different sensitivity voltage. The variably modified optical copies are directed to a photonic processor for further signal processing in the optical domain.
A motion planning system and method receives requests for routing a set of dissimilar aircraft through a defined airspace. Each aircraft has a starting and destination position relative to the airspace. A start state is based on the earliest start, and a goal state on the destination. The system connects start and goal states via a sequence of next states by projecting each state incrementally forward in time. Candidate next states include all possible next paths to a next position of each aircraft combined with next paths and positions of its neighbors, with unsafe next states culled from the set. Remaining next states are prioritized on the basis of aggregate system cost for all next paths and an estimated system cost to achieve the goal state, and an optimal next state is added to the sequence. When the goal state is achieved, optimal flight plans are generated for each aircraft.
A system and method for monitoring blood oxygen levels via an eye tracking camera includes a computer system with a processor configured to identify capillaries in the image stream of a pilot's eye. Changes in capillary size over time is directly correlated to blood flow levels. The processor may monitor capillary color. Changes in capillary color is directly correlated to blood oxygen levels. The processor may take remedial action when the pilot's blood oxygen level drops below a threshold. Such remedial action may include alerting the pilot, automatically alerting ground control crew, applying increasing levels of flight automation, etc.
A61B 5/1455 - Mesure des caractéristiques du sang in vivo, p. ex. de la concentration des gaz dans le sang ou de la valeur du pH du sang en utilisant des capteurs optiques, p. ex. des oxymètres à photométrie spectrale
A61B 3/113 - Appareils pour l'examen optique des yeuxAppareils pour l'examen clinique des yeux du type à mesure objective, c.-à-d. instruments pour l'examen des yeux indépendamment des perceptions ou des réactions du patient pour déterminer ou enregistrer le mouvement de l'œil
A61B 3/14 - Dispositions spécialement adaptées à la photographie de l'œil
A61B 5/00 - Mesure servant à établir un diagnostic Identification des individus
A shock load attenuation device is provided. The shock load attenuation device includes a crushable material; a first compartment in the crushable material surrounding a first line; and a second compartment in the crushable material surrounding a second line. In response to the first line being acted upon by a first force and the second line being acted upon by a second force, a first loop in the first line is configured to slide along the second line and a first loop in the second line is configured to slide along the first line, crushing the crushable material.
B64D 17/36 - Suspension de la charge incorporant des dispositifs de frottement ou de raccordement frangibles pour réduire le choc à l'ouverture de la coupole
F16F 7/12 - Amortisseurs de vibrationsAmortisseurs de chocs utilisant une déformation plastique de ses organes
F16F 7/14 - Amortisseurs de vibrationsAmortisseurs de chocs du type support de câble, c.-à-d. des câbles formant des boucles en prise par friction
