Abstract: A method of controlling an aeronautical gas turbine engine may be performed with an electronic controller. The method may include determining an airfoil pitch control command for at least one of a plurality of airfoils of the aeronautical gas turbine engine based at least in part on an excitation load acting upon the aeronautical gas turbine engine, and outputting the airfoil pitch control command to one or more actuators actuatable to change a pitch angle of the at least one of the plurality of airfoils. The airfoil pitch control command may be configured to augment and/or compensate for the excitation load acting upon the aeronautical gas turbine engine. The method may be embodied by a non-transitory computer-readable medium that includes computer-executable instructions, which when executed by a processor associated with the electronic controller, cause the electronic controller to perform the method.

Abstract: A method at a computing device including fragmenting a malware sample into a plurality of byte strings, each of the plurality of byte strings having a predetermined length; embedding each of the plurality of byte strings in an embedding network to generate a plurality of embeddings; for each embedding in the plurality of embeddings, finding a nearest neighbor; and setting a predicted family for the malware sample based on a fusion of the nearest neighbor for each of the plurality of embeddings.

Abstract: A gas turbine engine oil flow control system can include a variable flow oil pump useful to provide oil at varying rates to a variety of oil consumers, such as, power gearboxes, engine shaft bearings, electrical generators, etc. Oil flow control valves that have an ability to provide a variable flow of oil can be used in conjunction with the variable flow oil pump. Flow sensors can be used along with an oil flow controller to measure a flow of oil at various points in the gas turbine engine oil flow control system. The oil flow controller can use information from the flow sensors along with a variable consumption demand association with one or more of the oil consumers (either provided to the oil controller or calculated based upon an operational need of the oil consumer) to change operation of the variable flow oil pump and/or oil flow control valve.

Abstract: Systems and methods for providing a customized exercise protocol to a computing device of a user. As the user performs the exercise protocol, one or more cameras of the computing device can track the user's movements. The user's movement are assessed to determine if proper form and technique is being used.

Abstract: An inflatable penile prosthesis includes a fluid reservoir for holding fluid, an inflatable member, and a pump assembly for transferring fluid between the fluid reservoir and the inflatable member. The pump assembly includes a pump bulb, a valve block, and valves in the valve block. The valves include a control valve configured to move in a passageway formed within the valve block between an inflation position and a deflation position to control the flow of fluid within the valve block and the transfer of fluid between the fluid reservoir and the inflatable member. The control valve and the passageway are configured to form a seal that blocks fluid flow from the from a first side to a second side of the control valve, but to allow the seal to break when fluid pressure on the control valve is high, so as to relieve a high-pressure condition.

Abstract: Methods and systems for a device connectivity services system. A method for using the device connectivity services includes receiving a request to connect with a device to perform one or more tasks at the device, processing the request with respect to connectivity factors related to the request and the device, scheduling the request based on the connectivity factors, instantiating a controller to execute the one or more tasks at the device, sending commands to the device over a connection to perform the one or more tasks, and receiving responses from the device over the connection after completing the one or more tasks.

Abstract: A fuel flow measuring system includes an ultrasonic fuel flow sensor. The fuel flow sensor includes a first transducer and a second transducer. The first transducer is excited at multiple different excitation frequencies and a voltage, an electric current, and a phase difference between the voltage and the electric current is sensed at the first transducer during excitation. Data points are generated based on the sensed readings and a model is fit to the data points to determine a complex impedance spectrum. The complex impedance spectrum indicates a range of excitation frequencies within a range of a peak resonance frequency of the first transducer. One or more characteristics of excitation signals directed to the second transducer are set based on the determined complex impedance spectrum. In this manner, the signal to noise ratio of ultrasonic signals emitted by the second transducer and received by the first transducer can be maximized.

Abstract: A fuel flow measuring system includes an ultrasonic fuel flow sensor. The fuel flow sensor includes a first transducer and a second transducer. The first transducer is excited at multiple different excitation frequencies and a voltage, an electric current, and a phase difference between the voltage and the electric current is sensed at the first transducer during excitation. Data points are generated based on the sensed readings and a model is fit to the data points to determine a complex impedance spectrum. The complex impedance spectrum indicates a range of excitation frequencies within a range of a peak resonance frequency of the first transducer. One or more characteristics of excitation signals directed to the second transducer are set based on the determined complex impedance spectrum. In this manner, the signal to noise ratio of ultrasonic signals emitted by the second transducer and received by the first transducer can be maximized.

Abstract: A modular system and method for improving the receiving, processing, storing, and transloading of bulk materials such as organic waste. A system includes at least a receiving module to receive material, a storage module, a discharge module, and a control system. A liquid capture system captures and retains liquid from the organic material. Systems can be adapted with additional modules, such as processing modules and transfer modules, depending on the site and materials to be handled. The storage module has a levelling component for levelling out the organic material stored therein, including a levelling conveyor in a top region, and a removal component for discharging the organic material. A control system interfaces with the modular components and local operators, and provides remote reporting and monitoring.

Abstract: Radio transceiver device and method are provided. The method includes sequentially transmitting radio frequency signals on radio channels, each channel being nonuniformly spaced and representing a distinct continuous tone, sequentially transmitting radio frequency signals with distinct continuous tones on same channels as those received from the first radio transceiver device, as well as measured phase difference of the radio frequency signals on each radio channel received from the first radio transceiver device, creating a first set of estimate candidates, repeatedly for the radio channels, determining an optimal phase unwrapping vector candidate based on the first set of estimate candidates and the measured phase differences of signals received on the first and second transceiver devices to determine a second set of candidates, and calculating the distance between the first and second radio transceiver devices using the optimal phase unwrapping vector candidate and the second set.

Abstract: A method for controlled phase adjustment and coherent modulation in a radio frequency transceiver is provided. The radio frequency transceiver comprises an analogue circuitry for transmitting and receiving radio frequency signals and an all-digital phase locked loop controlled by a Phase Locked Loop, PLL, Control unit (200). The method comprises: receiving a phase shift, and based thereon, deriving a corresponding digital control signal; inputting the digital control signal to the PLL Control unit (200), the control signal defining a temporary iteration pattern of delays to be used by a configurable delay block, DTC (240); locking a radio frequency oscillator signal of a Digital Controlled Oscillator (220) in the phase locked loop to the temporary iteration pattern of delays; adjusting the phase of the frequency signal in digital circuitry, until the signal phase matches the phase shift defined by the digital control signal.

Abstract: A method and device for phase-based ranging measurement between a first radio frequency transceiver and a second radio frequency transceiver.

Abstract: An unmanned aerial vehicle (UAV) is disclosed that includes a retractable payload delivery system. The payload delivery system can lower a payload to the ground using a delivery device that secures the payload during descent and releases the payload upon reaching the ground. The location of the delivery device can be determined as it is lowered to the ground using image tracking. The UAV can include an imaging system that captures image data of the suspended delivery device and identifies image coordinates of the delivery device, and the image coordinates can then be mapped to a location. The UAV may also be configured to account for any deviations from a planned path of descent in real time to effect accurate delivery locations of released payloads.

Abstract: A method of controlling an aeronautical gas turbine engine may be performed with an electronic controller. The method may include determining an airfoil pitch control command for at least one of a plurality of airfoils of the aeronautical gas turbine engine based at least in part on an excitation load acting upon the aeronautical gas turbine engine, and outputting the airfoil pitch control command to one or more actuators actuatable to change a pitch angle of the at least one of the plurality of airfoils. The airfoil pitch control command may be configured to augment and/or compensate for the excitation load acting upon the aeronautical gas turbine engine. The method may be embodied by a non-transitory computer-readable medium that includes computer-executable instructions, which when executed by a processor associated with the electronic controller, cause the electronic controller to perform the method.

Abstract: A quality of service management system includes a rules engine that receives information associated with a communication path having an assigned quality of service (QoS) to be provided for a customer communication device, and identifies one or more network elements assigned to provide the communication path. Each network element having a plurality of queues configured to provide varying QoS levels relative to one another. For each of the network elements, the rules engine determines at least one queue that is configured to provide the communication path at the assigned quality of service, and transmits queue information associated with the determined queue to its respective network element, the network element conveying the communication path through the determined queue.

Abstract: Methods and systems for a device connectivity services system. A method for using the device connectivity services includes receiving a request to connect with a device to perform one or more tasks at the device, processing the request with respect to connectivity factors related to the request and the device, scheduling the request based on the connectivity factors, instantiating a controller to execute the one or more tasks at the device, sending commands to the device over a connection to perform the one or more tasks, and receiving responses from the device over the connection after completing the one or more tasks.

Abstract: A beverage dispense apparatus and associated method, comprises a frame (11) for removably locating and holding a sealed beverage unit package (C) in a vertical orientation. A first piercing element (14) punctures a vent opening into a headspace of the beverage package (C) and, subsequently as the first piercing element is driven downward, a second piercing element (15) punctures an outlet opening into the beverage package so that beverage can flow through a nozzle (17) under gravity. An ultrasonic transducer (16) against the nozzle (17) may supply excitation energy that breaks gas out of solution so that a creamy head is formed on the beverage in a delivery vessel underneath the frame. Control of the vent opening/vale (13) enables flow to be slowed or stopped through the nozzle (17) enabling a settle time and “two-part” pour.

Abstract: A system and methods of providing credibility and trustworthiness to users in a wellness platform. A method for providing search results to a user in an app including searching a query provided in the app, generating a plurality of results of the query, wherein the generating is based on a relevancy of the plurality of results, presenting at least one of the plurality of results in the app to the user, wherein the presenting is based on the relevancy, and displaying, by the at least one processor, the at least one of the plurality of the results in the app as a page, wherein the page has a plurality of sections associated with the at least one of the plurality of results.