Abstract: A chassis configured to hold a cards of at least two form factors comprising: slots disposed in an inner portion the chassis, wherein the slots are aligned with one another and configured to act as card guides; a mid-height structure disposed adjacent a side wall of the chassis, the mid-height structure comprising a second plurality of slots and a third plurality of slots disposed on top and bottom surfaces of the mid-height structure that are substantially parallel to top and bottom walls of the chassis; and a plurality of cooling channels disposed within the walls of the chassis as well as within the mid-height structure, wherein the second and third plurality of slots are configured to align with at least a subset of the plurality of slots disposed in the top and bottom chassis walls and to act as card guides.

Abstract: A guided vehicle that includes a body, a propulsion system operably engaged inside of the body, a housing operably engaged with the body and encasing a guidance device inside of the housing, a viewing window of the guidance device, and a cover moveably engaged with the housing, wherein the cover is moveable between a pre-flight configuration and a flight configuration. In the pre-flight configuration, the cover covers the viewing window. In the flight configuration, the cover is configured to expose the viewing window in the flight configuration in response to an impulse of acceleration generated by a launch of the guided vehicle.

Abstract: A rake assembly for measuring fluid flow parameters in a fluid flow rig, comprises: a rake assembly support frame; a housing mounted on the rake assembly support frame; the housing comprising a wall which defines a flow passage, with a flow inlet and a flow outlet, the flow passage extending from the flow inlet to the flow outlet. The housing is cylindrical and is centred on a longitudinal axis. An instrumentation arm extends from a leading edge end to a trailing edge end, and the instrumentation arm extends from the housing wall to extend at least part of the way across the flow passage, the leading edge end located in an Aerodynamic Instrument Plane (AIP); the housing being rotatably mounted to the rake assembly support frame; such that the housing and instrumentation arm are operable to rotate at least part of the way around the longitudinal axis.

Abstract: Various countermeasure dispensing systems (or CMDSs) and method of use are described herein. CMDS may include a dispenser assembly operably engaged with a platform where at least one electrical connection provides electrical communication between the dispenser assembly and a sequencer. CMDS may also include a magazine assembly operably engaged with the dispenser assembly, wherein the magazine assembly comprises a magazine configured to hold at least two countermeasure expendables. CMDS may also include a breechplate assembly operably engaged with the magazine assembly and adapted to dispense the at least two countermeasure expendables. CMDS may also include at least one magazine identification switch (MIS) operably engaged with the magazine assembly and the breechplate assembly. CMDS may also include that the at least one MIS is configured to enable the sequencer and the breechplate assembly to selectively dispense at least one countermeasure expendable from the at least two countermeasure expendables.

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: Systems and methods for pointing a high gain antenna or other directional instrument connected to a platform by a gimbal are provided. A control system as disclosed can include a flight computer having a processor for executing software and a motor control board having a controller for implementing at least portions of a control algorithm. The software executed by the processor generates pointing commands and implements a Kalman filter included in a feedback loop in the form of a linear Kalman filter disturbance estimator of the control algorithm implemented by the controller. The control algorithm can further implement a proportional control position loop and a proportional control rate loop. Each axis of the gimbal is provided with an instance of the control algorithm and the Kalman filter. Moreover, the processor can be operated at a rate that is less than a rate at which the controller is operated.

Abstract: Various systems and methods for leveraging legacy countermeasure dispensing systems (CMDSs). The legacy CMDSs are leveraged through the expansion of breechplates and magazines in a CMDS by expanding the amount of expendables carried by a CMDS while still maintaining the legacy sequencer and dispenser in a legacy military platform, such as an aircraft. In addition, various circuitry systems are included in a circuit card of the breechplate for duplicating and/or expanding the firing lines provided in a legacy CMDS.

Abstract: An energy management system (EMS) for an aircraft is provided. The aircraft may have one of a plurality of propulsion systems such as a parallel hybrid electric propulsion system, a parallel turbo electric propulsion system, an electric propulsion system, a turbo electric propulsion system and a turbo hybrid electric propulsion system. The EMS comprises redundant control paths for controlling safety critical operation. Each redundant control path is configured to independently determine whether to electrically isolate a line replaceable unit (LRU) from a high voltage DC link (HVDC link) based on status information from the LRU. The isolation is based on the independent determination. The HVDC link is used for propulsion. The number of the redundant control paths and components may be depending on the type of the propulsion system.

Abstract: A distributed control system includes an electronic control unit to establish secure communication with a distributed control module. Upon determination that a previously negotiated session key is stored on the electronic control unit, the electronic control unit transmits encrypted communications with the distributed control module using the previously negotiated session key, negotiates a new session key with the distributed control module, and stores the new session key. Upon determination that the previously negotiated session key is not stored on the electronic control unit, the electronic control unit negotiates the new session key with the distributed control module. After negotiating the new session key with the distributed control module, the electronic control unit ceases transmission of unencrypted communications with the distributed control module, transmits encrypted communications with the distributed control module using the new session key, and stores the new session key.

Abstract: A collet for multiple wire elements is disclosed. In an example, the collet has a body made of a polymeric material and extends along a central axis from a first end to a second end. The body defines a first passageway extending axially through the body, the first passageway in communication with the environment via a first insertion opening extending along an entire length of the first passageway. The body defines a second passageway extending axially through the body and in communication with the environment along an entire length of the second passageway via a second insertion opening, the second passageway spaced circumferentially from the first passageway. When installed, the collet frictionally engages wire elements when a first wire element is seated in the first passageway and a second wire element is seated in the second passageway.

Abstract: Charging apparatus and systems are provide for charging an energy storage system in respective vehicles using grid power where the vehicles are connected to the same transformer. The apparatus and system coordinate the charging and may use field weakening techniques to reduce a peak line-line voltage when a need is determined based on a minimum energy storage system voltage of the vehicles connected to the same transformer.

Abstract: A Laser Designator Pod (LDP) protective system, the LDP protective system comprising: a protective hood a laser detector arranged within the protective hood to generate a signal when exposed to laser radiation within a predefined range of wavelengths; and a computing device to record the generated signal.

Abstract: A wide angle MWIR F-theta lens with an F# of 2. The lens is deployed on airborne platforms for remote sensing applications. The lens is corrected for monochromatic and chromatic aberrations over the wavelength range 5000 nm-3300 nm. The image of the remote target is formed on a focal plane which may constitute CCD or CMOS with micro lenses. The lens comprises four groups of optical elements with a cold shield/aperture stop located behind the last group. One embodiment of the lens includes five types of optical materials and while another embodiment of the lens includes only two types of optical materials.

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 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 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 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 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 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.