Abstract: A secure system includes a data port, a network on chip (NoC) module, a processor communicatively coupled to the NoC module, a communication interface operatively coupled to the processor and to the data port, an electronic field-programmable gate array (eFPGA) configuration module operatively coupled to the NoC module, and a clock operatively coupled to the NoC module. In a first modality, the communication interface is at least partially disabled. In a second modality, the communication interface is at least partially disabled, boundary scan operations are disabled, a RESET signal is held in a constant state, and/or redacted code is rendered inoperable. In a third modality, the communication interface is at least partially enabled to send and receive commands and data via the data port, the boundary scan operations are enabled, the RESET signal is not held in the constant state, and/or the redacted code is operable.

Abstract: A common-mode current sensor system and method for a traction inverter of an electric hybrid vehicle. The system and method detects/reduces excess common-mode currents that can be caused by the presence of alternating current (AC)-chassis type short circuit faults at the outputs of an inverter used for driving a two or more-phased load. In an embodiment, the system detects the presence of an AC-chassis fault of any varying strength, e.g., weak, medium, hard, in respective parallel paths. The system and method can isolate a particular AC-chassis type fault to a particular phase leg of the inverter thereby obviating a need of having to shut-down and/or re-program each phase leg of the whole power supply and vehicle operation. Rather, upon detecting a chassis short, a fault signal is asserted to control shutting down of one or more inverter switches without having to shut-down the vehicle or negatively impact the vehicle status.

Abstract: A weapon-mountable smart optic comprising: a time reference configured to output a signal comprising a periodically-repeating feature and time metadata and comprising a first oscillator; at least two sensors configured to gather data, each comprising secondary oscillators; and at least one processor in communication with each of the at least two sensors; wherein each of the at least two sensors is in operative communication with the time reference and is configured to associate an edge of the periodically-repeating signal with a time conveyed by the time metadata, and wherein each of the at least two sensors is configured to gather data, associate time metadata with the gathered data, and to send the gathered data with time metadata to the at least one processor, and wherein the at least one processor is configured to fuse the data gathered by each of the at least two sensors.

Abstract: A passive sensor is used in conjunction with a trained machine learning classifier to make a You Are The One/You Are Not The One (YATO/YANTO) classification or determination as to whether an object, such as a threat, is moving toward a platform. The trained machine learning classifier utilizes a feature vector generated from conditioned temporal data and angular data obtained from passive sensor carried by the platform.

Abstract: A programmable transimpedance amplifiers (TIA) having T-network feedback architectures for achieving varying levels of gain based on a magnitude of an input current signal.

Abstract: A global navigation satellite system (GNSS) signal authentication methodology includes receiving, by one or more processors, a first digital signal and a second digital signal, the first digital signal and the second digital signal each representative of a GNSS satellite signal received from a GNSS satellite and including a ranging code that uniquely identifies the GNSS satellite, the first and second GNSS satellite signals transmitted contemporaneously from physically separate antennas onboard the GNSS satellite. The methodology continues with computing, by the one or more processors, a digital fingerprint based on the first digital signal and the second digital signal, and determining, by the one or more processors, that the first GNSS satellite signal and the second GNSS satellite signal are authentic (or not) based on the digital fingerprint. If the first and/or second GNSS satellite signals are found to not be authentic, remedial action may be taken.

Abstract: A sample and hold amplifier output buffer with the low leakage of metal oxide semiconductor field effect transistors (MOSFET) combined with the linearity and dynamic range of silicon-germanium (SiGe) bipolar junction transistors (BJT). In one aspect, the present disclosure provides a sample and hold amplifier output buffer placing a MOSFET input device between the base and emitter of a high linearity SiGe BJT.

Abstract: A device includes a frame and at least one printed circuit board attached to the frame. The frame includes an integrated aperture antenna array and an antenna feed in electrical communication with the at least one printed circuit board. The integrated aperture antenna array further includes a first conductive dipole arm in planar alignment with a surface of the frame; a second conductive dipole arm in planar alignment with the surface of the frame and adjacent to the first conductive dipole arm; a first feedline in electrical communication with the first conductive dipole arm and the antenna feed; a second feedline in electrical communication with the second conductive dipole arm and the surface of the frame; and a shorting arm in electrical communication with second conductive dipole arm and the frame.

Abstract: A system for enhancing a coupling laser beam to create a larger beam radius thus increasing sensitivity inside the system. The system includes a coupling laser source to emit a coupling laser defining a first power level. The system also includes a resonant optical cavity that is optically aligned with the coupling laser source and the probe laser source. The resonant optical cavity enhances the coupling laser to a second power level that is greater than the first power level inside of the resonant optical cavity. The power increase of the coupling level also increases the sensitivity of the atomic receiver system by increasing the diameter of the coupling laser inside of the resonant optical cavity. The system also includes at least one photodetector positioned outside of and optically aligned with the resonant optical cavity for monitoring a resonance condition of the coupling laser circulating within the resonant optical cavity.

Abstract: An impulse cartridge (IC) cup has at least one aperture defined in a cylindrical sidewall. The first aperture extends radially relative to a primary axis through the cylindrical sidewall from an inner surface to an outer surface. A first electrical connector is disposed in the first aperture. The first electrical connector is adapted to physically contact the impulse cartridge at a first location. The IC cup is adapted to be connected to a canister that houses a payload of a countermeasure defense system, wherein the payload is to be deployed in response to explosion of the impulse cartridge.

Abstract: A system that includes a plurality of encapsulation blocks having a plurality of digital signal processing (DSP) blocks provided with preconfigured logic functions and a plurality of pacing control networks operatively connected with the plurality of DSP blocks. The system also includes a streaming cross bar operatively connected with each encapsulation block of the plurality of encapsulation blocks. Each encapsulation block of the plurality of encapsulation blocks includes a DSP block of the plurality of DSP blocks and a pacing control network of the plurality of the pacing control networks. Each DSP block of the plurality of DSP blocks is independently and separately connected with the streaming cross bar via the plurality of pacing control networks.

Abstract: A guidance system for a guided munition has an inertial measurement unit (IMU) or another type of first sensor on the guided munition, electro-optical/infrared (EO/IR) sensor on the guided munition, and a guidance computer assembly (GCA) having a Programmable Real-Time Unit Industrial Communication SubSystem (PRU-ICSS), wherein the PRU-ICSS is in operative communication with the IMU or another type of first sensor and the EO/IR. The PRU-ICSS has a first Programmable Real-Time Unit (PRU), wherein the first PRU is programmed to receive and process input data from the IMU or another type of first sensor on the guided munition, and the PRU-ICSS has a second PRU, wherein the second PRU is programmed to receive and process input data from the EO/IR sensor on the guided munition.

Abstract: A guidance system for a guided munition has an inertial measurement unit (IMU) or another type of first sensor on the guided munition, electro-optical/infrared (EO/IR) sensor on the guided munition, and a guidance computer assembly (GCA) having a Programmable Real-Time Unit Industrial Communication SubSystem (PRU-ICSS), wherein the PRU-ICSS is in operative communication with the IMU or another type of first sensor and the EO/IR. The PRU-ICSS has a first Programmable Real-Time Unit (PRU), wherein the first PRU is programmed to receive and process input data from the IMU or another type of first sensor on the guided munition, and the PRU-ICSS has a second PRU, wherein the second PRU is programmed to receive and process input data from the EO/IR sensor on the guided munition.

Abstract: A portable launcher to launch a guided projectile at an aerial target, wherein the guided projectile has a projectile guidance kit and a target leading guidance kit that is provided with the guided projectile and the portable launcher. The target leading guidance kit includes a target lead estimation protocol stored on a computer readable media and accessible by a processor of the target leading guidance kit. When the processor executes the target lead estimation protocol, the processor is instructed to dynamically lead a reticle of an electronic sight of the target leading guidance kit from the initial target position to the lead target position in response to the projectile guidance kit detecting a speed of the aerial target and an inertial measurement unit of the target leading guidance kit that measures the slew of the guided projectile from the initial position to the translated position.

Abstract: A method fabricating at least one universal substrate from a batch product. The method includes steps of: providing a preform having a predetermined profile; wrapping a plurality of conductors about an outer surface of the preform; injecting a nonconductive matrix between conductors of the plurality of conductors, wherein the nonconductive matrix permeates between interstitial spaces of the plurality of conductors to isolate some conductors of the plurality of conductors from one another; forming the batch product that includes the plurality of conductors and the nonconductive matrix; and wafering at least one section of the batch product to form the at least one universal substrate. The plurality of conductors of the at least one universal substrate defines a first connection surface, a second connection surface opposite to the first connection surface, and a plurality of conductive pathways defined between the first connection surface and the second connection surface.

Abstract: A system for partially pre-charging an electrical power system having a high voltage power source, a DC link device with a DC Link capacitor, a low voltage power source and a DC/DC converter. In one embodiment a partial pre-charge of the DC Link capacitor can be achieved in three ways: first, through a DC/DC converter boosting from the low voltage power source, second, through a first circuit provided to charge the DC link capacitor to a partial pre-charge state using the voltage directly from the low voltage power source, and third, through a second circuit provided to limit current flowing to the DC link capacitor from the high voltage power source to charge the DC Link capacitor only to a partial pre-charge level.

Abstract: A crimping tool for assembling a countermeasure expendable. The crimping tool includes a main body that has a top end, a bottom end vertically opposite to the top end, and an axis defined between the top end and the bottom end. The main body is configured to receive a cap of the countermeasure expendable, a spacer of the countermeasure expendable, and a cartridge case of the countermeasure expendable. The crimping tool also includes a presser that selectively operably engages with the main body and is configured to press the cap and the spacer of the countermeasure expendable into the cartridge case of the countermeasure expendable. The crimping tool also includes a set of crimpers that operably engages with the main body and is configured to crimp at least the cap, the spacer, the cartridge case with one another to collectively maintain the cap and the spacer with the cartridge case.

Abstract: A smart store communication interface (SSCI) squib of a countermeasure expendable. SSCI squib also includes a first electrical network. SSCI squib also includes a second electrical network that is isolated from the first electrical network. SSCI squib includes a fire pin contact that operably engages with the first electrical network and the second electrical network. The SSCI squib is configured to one of ignite a propellant loaded inside of a housing of the SSCI squib and communicate with a processor of the countermeasure expendable in response to receiving at least one electrical signal at the fire pin contact.

Abstract: Techniques are provided for employing an embedded software defined radio (SDR) in a navigation system. A navigation system implementing the techniques according to an embodiment includes a global positioning system (GPS) receiver configured to acquire and track received GPS signals. The system also includes an SDR configured to process received communication signals. The communication signals include timing data. The SDR is further configured to calculate position and navigation data based on a combination of the processed communication signals and the tracked GPS signals provided by the GPS receiver. The system further includes a system timer configured to provide a common time base for use by the GPS receiver and the SDR. The navigation system is implemented in an application specific integrated circuit (ASIC).