Abstract: A system comprises a vehicle platform of an underwater vehicle, and a model based navigation system for vehicle dynamics modeling navigation of the underwater vehicle. The model based navigation system comprises inertial sensors on the vehicle platform; a strapdown navigation processor that receives inertial sensor data from the inertial sensors; platform input sensors and a vehicle physics model that receives platform input measurements from the platform input sensors; a propagator-estimator filter that receives vehicle data from the vehicle physics model; and a depth sensor that determines depth measurements for the vehicle platform. A tethered platform is releasably coupled to the vehicle platform and communicates with the model based navigation system. The tethered platform comprises an aiding source that determines position and velocity measurements that are transmitted to the propagator-estimator filter.

Abstract: Methods and systems to process and assure integrity of radar measurements, detect the effects of GNSS jamming and/or spoofing events, identify GNSS measurements affected by the GNSS jamming and/or spoofing events, and assure the integrity of the GNSS measurements unaffected by jamming and/or spoofing events in a vehicle navigation system are disclosed. The methods are implemented to integrate inertial measurements, GNSS measurements, and radar measurements for the vehicle, and apply solution separation techniques to all of the measurements. The solution separation techniques use a main filter for hybridization of the inertial measurements, the GNSS measurements, and the radar measurements, with additional sub-solution filters and sub-sub-solution filters that use combinations of these measurements. This provides common processing of the GNSS and radar sensors in a single hybridization and solution separation framework.

Abstract: Devices, methods, and systems for monitoring a self-testing fire sensing device are described herein. One device includes a memory, and a processor configured to execute instructions stored in the memory to receive, from a self-testing fire sensing device, measurements of outputs of light-emitting diodes (LEDs) of the self-testing fire sensing device during operation of the self-testing fire sensing device, determine when a deviation in the measured outputs of the LEDs of the self-testing fire sensing device meets or exceeds a threshold deviation amount, determine an action to take on the self-testing fire sensing device upon determining the deviation in in the measured outputs of the LEDs meets or exceeds the threshold deviation amount, and send a notification of the determined action to take on the self-testing fire sensing device to an additional computing device.

Abstract: Lower noise and complexity techniques are disclosed for compensating for time varying phase changes in fiber optics in a resonant fiber optic gyroscope (RFOG). Orthogonal components derived from an electrical beat note signal and a difference between clockwise and counterclockwise resonant frequencies of an optical resonator coil of the RFOG are determined. The orthogonal products are converted to a phase which is differentiated with respect to time to obtain a beat note correction signal.

Abstract: A bleed system including control circuitry and a variable jet pump. The control circuitry is configured to receive a signal indicative of a fluid parameter in the bleed system and cause the jet pump to alter a mixing ratio of a higher pressure gas and a lower pressure gas based on the signal. The jet pump is configured to combine the lower pressure gas and the higher pressure gas in the mixing ratio to generate a mixed gas. The jet pump is configured to supply the mixed gas to one or more gas loads in the bleed system. In examples, the control circuitry is configured to establish a system setpoint for the fluid parameter based on an operating status of the one or more gas loads.

Abstract: Embodiments of the disclosure are directed to a shock initiation system for initiating shock in a shock tube for demolition. In some embodiments, the shock initiation system comprises a reusable discharge unit and a replaceable shock initiation platform. The reusable discharge unit may comprise a power source, a timer, a switch, and user inputs and may function to store a time, countdown the timer, and generate and transmit an electrical energy to the replaceable shock initiation platform. The shock initiation platform may receive the electrical energy from the discharge unit overpowering a resistor disposed on the shock initiation platform. The resistor may then detonate providing an initiation shock to a proximally disposed shock tube, thereby initiating shock in the shock tube.

Abstract: An electronic assembly comprises a printed circuit board including a plurality of stacked layers, wherein the stacked layers comprise a plurality of conductive layers, a plurality of dielectric layers respectively interposed between the conductive layers, and one or more phase change material layers interposed between at least one pair of the dielectric layers or at least one pair of the conductive layers. During a phase change, the one or more phase change material layers are configured to absorb thermal energy at a phase transition temperature to provide enhanced cooling of the printed circuit board. In some embodiments, the printed circuit board can be a metal core printed circuit board.

Abstract: A method and system for airline operation center (AOC) data communications are disclosed. The method comprises providing a computing device for use onboard an aircraft, with the computing device hosting at least one application configured to interact with at least one avionics processing unit onboard the aircraft. The method further comprises automatically retrieving, by the at least one application, AOC information for storage and processing on the computing device, and transmitting by the at least one application, the AOC information from the computing device to the at least one avionics processing unit. The AOC information is used by the at least one avionics processing unit to execute an AOC application hosted by the at least one avionics processing unit.

Abstract: Various examples of the present disclosure provide aircraft engine sensing apparatuses and methods of manufacturing aircraft engine sensing apparatuses. For example, an example aircraft engine sensing apparatus includes an aircraft engine sensor, a plurality of connection wires, and at least one ceramic insulator. In some examples, the aircraft engine sensor is positioned within an aircraft engine. In some examples, the plurality of connection wires connect the aircraft engine sensor to a sensor connector. In some examples, the plurality of connection wires are positioned within a wire protection housing. In some examples, the at least one ceramic insulator is positioned within the wire protection housing and defines a plurality of insulator openings. In some examples, each of the plurality of connection wires passes through one of the plurality of insulator openings.

Abstract: One embodiment includes a monitor module for a first device, wherein the first device is configured to obtain measurement data from a second device, to compare the measurement data to a reference value, and to send a signal when the measurement data in comparison to the reference indicates an error condition. Machine learning can be used, where a head-end is capable of modifying the second device when the reference value so indicates. This enables various embodiments to fix the second device without human intervention.

Abstract: An RFOG includes a resonator and an optical signal source configured to produce optical signals. Further, the RFOG includes optical components that introduce a first and second optical signals derived from the optical signals for propagation within the resonator wherein the first and second optical signals propagate in opposite directions. Additionally, the RFOG includes serrodyne modulation electronics that generate a serrodyne modulation control signal, wherein a first and second serrodyne modulation signal are generated from the serrodyne modulation control signal, wherein a sign of a slope of the first serrodyne modulation signal is opposite a sign of a slope of the second serrodyne modulation signal, wherein the signs of the slopes of the first and second serrodyne modulation signals periodically switch.

Abstract: One or more datalink labels are displayed on a shared panel of a user interface. The datalink labels are generated in response to receiving a datalink message from at least one ground station. Upon receiving a selection of the datalink label, one or more sub-panels that include information or a representation of the datalink message are displayed on the user interface. In some embodiments, the sub-panel includes a button that, when selected, automatically generates a response message. Utilizing datalink labels in conjunction with the shared panel simplifies datalink messaging and enables messaging functions to be completed on the same screen regardless of which application (or function of an application) is currently displayed on the user interface.

Abstract: Various embodiments describe time-multiplexing of optical channels in an air data sensor. At least one switch outputs a reference optical signal, and each of a plurality of backscattered optical signals to at least one common optical path at a time. Alternatively stated, the at least one common optical path is configured to receive the reference optical signal and at least one of the backscattered optical signals in sequence. In doing so, the extent of systematic bias present in the at least one common optical path can be compensated for and even reduced during sensor operation.

Abstract: Methods and systems for access control involve dynamically controlling an access to firmware running a certified feature in an energy meter and a non-certified feature in the energy meter. The access can be based on a bifurcation between the certified feature and the non-certified feature running in the energy meter on one or more of a single microcontroller or a group of different microcontrollers.

Abstract: A processing element for implementation in a digital signal processing system is provided. The processing element is configured to receive a first data stream comprising a plurality of digital values where each value represents a sample of an analog signal. The processing element is further configured to receive a second data stream comprising a series of digital values where each value represents a sample of the analog signal. The processing element is configured to filter the first data stream via a first Farrow-structured fractional delay (FD) filter and output a filtered first data stream; filter the second data stream via a second Farrow-structured FD filter and output a filtered second data stream; and temporarily store values from the second data stream and output the stored values to the first Farrow-structured FD filter so that the stored values can be used to filter the first data stream.

Abstract: An example method includes combining an interlayer and a carbon fiber fabric, wherein the interlayer comprises a highly oriented milled carbon fiber ply comprising a plurality of out-of-plane carbon fibers. The method further includes winding the interlayer and the carbon fiber fabric around a core to form a composite fiber preform comprising a plurality of layers defining an annulus extending along a central axis. The method further includes densifying the composite fiber preform.

Abstract: Systems and methods for an active transistor RNG circuit with MEMS entropy are described herein. In one example, an RNG circuit includes one or more MEMS structures configured to provide an output, wherein the output includes active oscillations, charge, resistance, capacitance, and/or inductance values. The RNG circuit further includes active transistor RNG circuitry communicatively coupled to the one or more MEMS structures. The active transistor RNG circuitry is configured to generate a random number output based on the output by the one or more MEMS structures. The random number output generated by the active transistor RNG circuitry is an output of the RNG circuit.

Abstract: A vehicle having a doppler based cellular navigation system is provided. The vehicle includes a radio frequency (RF) antenna, an RF receiver in communication with the RF antenna, a memory and a controller. The memory includes a ground-based RF emitter database with ground-based RF emitter location information. The controller is in communication with the RF receiver and the memory. The controller is configured to monitor a doppler shift in received RF signals from ground-based RF emitters. The controller is further configured to determine location information when the controller detects a doppler shift in a received RF signal of zero. The controller is further configured to implement the determined location information in navigating a vehicle.

Abstract: Systems and methods for codependent physical unclonable function (PUF)/random number generator (RNG) generator pairing for physical provenance are described herein. In one example a device includes physical unclonable function (PUF) circuitry configured to produce a PUF output in response to an input and random number generator (RNG) circuitry configured to output one or more random numbers. The PUF circuitry and the RNG circuitry share one or more components such that an alteration of the RNG circuitry alters the PUF circuitry. The device is configured to determine whether the RNG circuitry is an untainted source of random numbers based on an output of the PUF circuitry.