Abstract: A method and system for analysis of a facility may include providing an emulation host system, first generating a golden circuit model on the emulation host system, first inserting a first hardware trojan model, first emulating operation of the golden circuit model, and second emulating operation of the first hardware trojan model. A facility may include a trojan instrument facility having a trojan detection instrument comparing logic circuit output against a threshold for detecting hardware trojan activity, and outputting alert data, and in relation to opening one of a plurality of scannable access points, a scannable register is inserted into an active scan chain with an associated instrument interface.

Abstract: A method for extracting a rescue subject from a surface position includes lowering a rescue pod having an enclosed compartment with a door from an aircraft, the rescue pod having a parachute and a control system, the rescue pod connected by a tether to a winch in the aircraft, controllably releasing the tether from the winch while maneuvering the aircraft into an orbit at altitude, diameter and airspeed, creating a gravity well in which the tether describes a spiral configuration with the pod descending along a vertical centerline, lowering the pod to the surface position, loading the rescue subject into the enclosed compartment, and lifting the rescue pod from the surface position by retrieving the tether with the winch or altering the path and speed of the aircraft, in a manner to gradually increase tension in the tether lifting the rescue pod from the ground point.

Abstract: A satellite refueling system has a refueling satellite carrying fuel, a fuel hose connected to the fuel carried by the refueling satellite, with a maneuverable end effector at a deployed end of the fuel hose, the end effector comprising a fuel supply nozzle connected to the fuel hose, a plurality of thrusters on the end effector providing thrust in a plurality of directions, an imaging device on the end effector capturing images in an immediate environment of the end effector, and computerized circuitry operating individual ones of the plurality of thrusters in response to the images captured by the imaging device. The refueling satellite deploys the fuel hose, and the computerized circuitry operates the thrusters to maneuver the end effector, bringing the fuel supply nozzle to a location to deliver fuel.

Abstract: Provided are systems and methods for vessel risk assessment. This includes determining a risk assessment associated with a vessel, including receiving vessel data from at least one source, generating at least one vessel profile based on the vessel data, wherein each vessel profile provides indication of expected behavior events for one vessel and abnormal behavior events for one vessel, determining at least one abnormal behavior event of the vessel based on the at least one vessel profile, each event in the at least one abnormal behavior event having a time of occurrence, determining at least one frequency of occurrence of abnormal behavior events of the vessel based on the time of occurrence of each event, using at least one model to determine a risk assessment associated with the vessel based on the at least one frequency of occurrence of abnormal behavior events of the vessel.

Abstract: Systems and methods for implementing ejector refrigeration cycles with cascaded evaporation stages that utilize a pump to optimize operation of the ejector and eliminate the need for a compressor between the evaporation stages.

Abstract: Roughly described, the technology disclosed provides a so-called machine-learned conversion optimization (MLCO) system that uses artificial neural networks and evolutionary computations to efficiently identify most successful webpage designs in a search space without testing all possible webpage designs in the search space. The search space is defined based on webpage designs provided by marketers. Neural networks are represented as genomes. Neural networks map user attributes from live user traffic to different dimensions and dimension values of output funnels that are presented to the users in real time. The genomes are subjected to evolutionary operations like initialization, testing, competition, and procreation to identify parent genomes that perform well and offspring genomes that are likely to perform well.

Abstract: Systems and methods for regenerative ejector-based cooling cycles that utilize an ejector as the motivating force in a cooling loop to regeneratively sub-cool a refrigerant in a single-stage cooling cycle.

Abstract: Systems and methods for producing a decarbonized blue hydrogen gas for cracking operations utilizing a standard separation process, such as Pressure Swing Absorption (PSA), to separate a tail gas mixture of hydrogen and hydrocarbons into hydrogen gas and a PSA effluent that is used in a hydrogen generation unit to produce the decarbonized blue hydrogen gas for cracking operations

Abstract: A method for finding a best solution to a problem is provided. The method includes evolving candidate individuals in a candidate pool by testing each candidate individual of the candidate individuals to obtain test results, assigning a performance measure to each of the tested candidate individuals in dependence upon the test results, discarding candidate individuals from the candidate pool in dependence upon their assigned performance measure, and adding, to the candidate pool, a new candidate individual procreated from parent candidate individuals remaining in the candidate pool, and repeating the evolution steps to evolve the candidate individuals in the candidate pool.

Abstract: A refueling system has a vehicle having a fuel tank connected to a deployable fuel hose, an end effector having controlled flight, the fuel hose connected at an end away from the first vehicle, through the end effector to a fuel connector under the end effector, a second vehicle having a fuel tank coupled through a pumping apparatus to a fueling port on an acquisition apparatus adapted to acquire the end effector and connect the fueling port and the fuel connector of the end effector, and control circuitry enabling controlled flight of the end effector, wherein the end effector is controlled to be acquired by the acquisition apparatus to couple the fuel connector with the fueling port and fuel is provided from the fuel tank of one of the vehicles to the fuel tank of the other of the vehicles through the pumping apparatus.

Abstract: A method and system is disclosed herein for decoupling billing for web services from the application logic which governs those web services by instrumenting a web services stack to monitor SOAP envelopes for pre-determined elements and to use those elements to determine questions as to authorization for solvency as well as calculate charges for said web services.

Abstract: Systems and methods for using a multi-stage compressor to increase the temperature and pressure of BOG sent to a heat exchanger for cooling a separate liquid refrigerant. The subsequent stage(s) of the multi-stage compressor further compress the BOG, which is then recycled to a liquefaction unit or used as fuel gas for one or more turbines.

Abstract: Systems and methods for regenerative ejector-based cooling cycles that utilize an ejector as the motivating force in a cooling loop to regeneratively sub-cool a refrigerant in a single-stage cooling cycle.

Abstract: A stabilizing system for a cable has a cable deployed and suspended from a helicopter, a cargo support attached at a deployed end of the cable, an end effector attached to the cable, the end effector comprising thrusters directed in a plurality of directions orthogonal to a vertical axis of the cable, first control circuitry in the helicopter, and second control circuitry in the end effector. Thrust of individual thrusters is controlled through the first and second control circuitry maintaining the axis of the cable vertical, damping swinging of the cable.

Abstract: A system and method for determining a point in time compliance status of a computing system with a security guideline standard (SGS) wherein the computing system has a command line shell available through a native operating system, the method comprising inputting into a host computer of the computing system a SGS package that represents a scripted SGS that is a non-text file and is encrypted that provides instructions for an evaluation of a computing system's compliance with the SGS under consideration wherein the SGS package performs at least a portion of an automated evaluation of a compliance status at the point in time of the computing system under consideration when the SGS package is decrypted by the computing system; sending a command query from the decrypted SGS package to the selected device of the computer system; compiling in a locally hosted database of the host computer compliance results sent from the selected device of the computing system in response to the command query from the decrypted SGS

Abstract: A system for fighting fires has a source of fire-retardant material, a delivery hose connected to the source has a delivery nozzle at an end, and an end effector carrying the delivery hose proximate the nozzle. The end effector has controllable thrusters, an imaging device, and control circuitry including a display monitor, the control circuitry providing commands controlling actuators varying thrust and direction of the thrusters, and a valve in the delivery nozzle. With the delivery hose deployed, images from the end effector are transmitted to the control circuitry and displayed on the display monitor, and an operator viewing the images on the display monitor uses the command inputs to maneuver the end effector, carrying the nozzle at the end of the delivery hose to a position proximate an active fire, and opens the valve on the nozzle, delivering fire retardant material from the nozzle onto the fire.

Abstract: A system for refueling has a boom having a rigid portion and, extendible portion and a fuel nozzle at an end of the extendible portion, the fuel nozzle mates with a port on an aircraft. Control circuitry in the tanker aircraft has input elements by which an operator controls actuators moving the boom left, right and up and down, and a first imaging device proximate the end of the extendible portion of the boom, capturing images and transmitting the captured images to the control circuitry, where the images are displayed on a monitor visible to the operator. The operator controls extension and attitude of the fuel nozzle at the end of the extendible portion, according to the images displayed, mating the fuel nozzle with the refueling port, and transferring fuel from the tanker aircraft to the aircraft to be refueled.

Abstract: Systems and methods for efficient on-line pigging of a coker furnace without interruption of the delayed coking process, which will save time and money during the delayed coking process. This system can be retrofitted to existing coker furnaces.

Abstract: A refueling system has a vehicle having a fuel tank connected to a deployable fuel hose, an end effector having controlled flight, the fuel hose connected at an end away from the first vehicle, through the end effector to a fuel connector under the end effector, a second vehicle having a fuel tank coupled through a pumping apparatus to a fueling port on an acquisition apparatus adapted to acquire the end effector and connect the fueling port and the fuel connector of the end effector, and control circuitry enabling controlled flight of the end effector, wherein the end effector is controlled to be acquired by the acquisition apparatus to couple the fuel connector with the fueling port and fuel is provided from the fuel tank of one of the vehicles to the fuel tank of the other of the vehicles through the pumping apparatus.

Abstract: An imaging system has a tether sub-system deployable and retrievable from an aircraft, an imaging device attached at a deployable end of the tether, and control apparatus comprising control and communication circuitry receiving images captured by the imaging apparatus and storing the images. The tether is deployed to a predetermined length, the aircraft is piloted in a flight pattern causing the imaging device at the deployed end of the tether to attain a fixed position proximate an imaging target, and the control apparatus is operated to capture images of the target.