Abstract: Embodiments of the present invention provide a software core controller for facilitating communication between a UAV control system, a UAV, and other peripheral devices used to control or to determine the status of the UAV. Different UAVs, control systems, and peripheral devices may require that data be transmitted and received according to their own particular specifications, such as a particular data rate and a particular format. The software core controller may be configurable to interface with these devices using the devices' interfaces. The interfaces may be specified by the devices' interface control documents (ICDs). The ICDs may be used to configure the software core controller upon initialization. The software core controller may asynchronously receive and provide data at the data rate specified in the various ICDs. The software core controller may support a plurality of different physical interfaces in order to communicate with different control systems, UAVs, and peripheral devices.

Abstract: A thermal isolator is provided for use with a sensor having a sensing element. The isolator has a main body made of a thermally insulating material. The main body has an outer surface, a sensor receiving passage for receiving the sensor, and at least one venting port fluidly communicating with the sensor receiving passage and the outer surface. The sensor receiving passage is adapted to position the sensor such that the sensing element is unreachable by a linear path from the outer surface through any opening in the main body.

Abstract: A launcher includes a plurality of launch tubes for stowing and launching a plurality of air vehicles. A central air manifold is operatively connected to an air storage tank; a first launch tube air manifold is operatively connected to a first group of the launch tubes and operatively connected to the central air manifold. The first launch tube air manifold has a separate port corresponding to each launch tube of the first group of launch tubes. A release valve mechanism is removably mounted in one of the ports of the first launch tube air manifold, the release valve mechanism controlling the passage of launch air between the first launch tube air manifold and the launch tube corresponding to the port in which the release valve mechanism is mounted. A plug is removably mounted in each of the ports not occupied by the release valve mechanism.

Abstract: A system and method to generate a trigger signal based on a real-time adaptive threshold. The system may include a microphone to receive an audio signal, a device to generate a trigger signal based on a real-time adaptive threshold coupled to the microphone to form an adaptive threshold and generate a trigger signal if a magnitude of the audio signal is greater than a magnitude of the adaptive threshold. The system may also include a waveform capture module coupled to the microphone to receive the audio signal and convert the audio signal into a series of waveform packets and a waveform analysis processor to extract characteristics from the waveform packets.

Abstract: A gyroscopic system for translating parallel and non-parallel lines between a reference line and a device to be aligned with respect to the reference line is provided. The system includes a first inertial sensor configured to be substantially stationary, the first inertial sensor comprising a first three-axis gyroscopic sensor configured to produce an output signal and a reflector. A second inertial sensor is configured to be portable so as to be positionable adjacent to the first inertial sensor and comprises a gimbal restricted to two physical axes, a gimbal drive system, an electromagnetic energy beam generator, a second three-axis gyroscopic sensor configured to generate an output signal, and a collimator. The collimator is operable to determine an angle between a beam projected by the beam generator and a beam reflected from the reflector and to generate an output signal indicative of the determined angle.

Abstract: A phase persistent agile signal source method, apparatus, and/or computer program product provides a direct digital synthesizer (DDS) clock rate, provides a frequency tuning word (FTW) for a desired output frequency, provides a DDS update for a desired DDS update rate, provides an equivalent frequency least significant bit (LSB) for the desired DDS update rate, provides a current phase of an LSB accumulator, and generates a coherent phase of the desired output frequency based on the DDS clock rate, FTW, DDS update rate to the DDS, equivalent LSB for the desired DDS update rate, and current phase of the LSB accumulator. The coherent phase can be the fraction portion of the result obtained from the multiplication of the FTW and the current phase of the LSB accumulator.

Abstract: A payload ejection system is provided for ejecting a payload from a transport vehicle. The system has an ejector mechanism for applying an ejection force to the payload to urge the payload away from the transport vehicle, and a release mechanism for releasing the payload from a restrained state. The release mechanism has a payload mounting bolt for holding the payload in the restrained state, and an actuator that fractures the mounting bolt. The actuator has a shape memory alloy, and an activator that transforms the shape memory alloy from a compressed state to an elongated state. The actuator fractures the mounting bolt as the shape memory alloy transforms into the elongated shape.

Abstract: An improved door assembly has a single movable door and may have a separate movable high platform threshold. The door assembly is formed of an upper door section and a lower door section which is fixed to the upper door section. A support member may be integral with or slidably engaged with the door assembly, disposed as an angle iron fixed to the door assembly, or disposed on the side of a stairwell of a rail passenger car.

Abstract: A portable unmanned air vehicle and launcher system is provided that includes a foldable unmanned air vehicle having a pressure tube; a launch gas reservoir for holding launch gas; a launch tube operatively connected to the launch gas reservoir and having a free end that is positioned in the pressure tube of the air vehicle; a free piston positioned within the launch tube; and a free piston stop to prevent the free piston from leaving the launch tube. A first portion of the launch gas in the launch gas reservoir is released into the launch tube and forces the free piston from an initial position to an end position at which the free piston is stopped by the free piston stop.

Abstract: A gyroscopic system for translating parallel and non-parallel lines between a reference line and a device to be aligned with respect to the reference line is provided. The system includes a first inertial sensor configured to be substantially stationary, the first inertial sensor comprising a first three-axis gyroscopic sensor configured to produce an output signal and a reflector. A second inertial sensor is configured to be portable so as to be positionable adjacent to the first inertial sensor and comprises a gimbal restricted to two physical axes, a gimbal drive system, an electromagnetic energy beam generator, a second three-axis gyroscopic sensor configured to generate an output signal, and a collimator. The collimator is operable to determine an angle between a beam projected by the beam generator and a beam reflected from the reflector and to generate an output signal indicative of the determined angle.

Abstract: An improved door assembly having a single movable door and a separate movable high platform threshold.

Abstract: An improved door assembly has a single movable door and may have a separate movable high platform threshold. The door assembly is formed of an upper door section and a lower door section which is fixed to the upper door section. A support member may be integral with or slidably engaged with the door assembly, disposed as an angle iron fixed to the door assembly, or disposed on the side of a stairwell of a rail passenger car.

Abstract: An improved door assembly has a single movable door and may have a separate movable high platform threshold. The door assembly is formed of an upper door section and a lower door section which is fixed to the upper door section. A support member may be integral with or slidably engaged with the door assembly, disposed as an angle iron fixed to the door assembly, or disposed on the side of a stairwell of a rail passenger car.

Abstract: An improved door assembly having a single movable door and a separate movable high platform threshold.

Abstract: An improved door assembly having a single movable door and a separate movable high platform threshold. The door assembly is formed of an upper door section and a lower door section fixed to the upper door section. A support member can be slidably engaged with the door assembly. A solenoid may also be disposed in the door assembly.

Abstract: Given a trajectory and unit pointing vectors determined based on a planar or other approximation of a shock wave, a method and apparatus are provided to calculate times the sensors should have detected, based on a conical geometry of the shock wave. A difference between the calculated times and the actual times measured by the sensors may be minimized. The minimization may be performed by perturbing the unit vectors. When the perturbation of the unit vectors results in an acceptable difference between the calculated times and the measured times, an accurate trajectory of the projectile can be generated from the perturbed unit pointing vectors.

Abstract: A mobile aircraft launcher includes a towable, tiltable, wheeled trailer, a launch beam comprising a plurality of sections hinged to one another, an aircraft-engaging shuttle mounted on the launch beam, and a shuttle-moving drive arrangement mounted on the trailer. The launch beam is mounted on the trailer and is movable between a folded, transport condition, in which the beam sections are generally side-by-side, and a launch condition, in which the beam sections are colinear. In the colinear arrangement, a portion of the launch beam extends forward of the trailer, that portion being supportable entirely through the trailer.

Abstract: A digital radar landmass simulator (DRLMS) used for stimulation testing pulse radars, wherein the DRLMS operates by synthesizing time-overlapping chirp waveforms using finite impulse response filters. The DRLMS, thus, effectively generates many overlapping complex pulse signals from many radar reflectors representing a semi-infinite continuum of closely spaced targets. The DRLMS also allows the insertion/injection of the effects of Doppler shift and jamming into the synthesized modulated signal.

Abstract: A remotely controlled simulated linear circuit breaker capable of being set and reset remotely, and manually operated. Control signals are received by an on-board controller circuit card assembly. The signals will cause a plunger located in a solenoid housing to do one of two things. Either it will be extracted out of the solenoid housing, thereby popping the simulated circuit breaker, or it will be pulled into the solenoid housing, thereby resetting the simulated circuit breaker. In addition, the position of the switch is remotely sensed.

Abstract: The present invention employs rotary switches that can be electromechanically set or reset remotely. Typical, although not limiting, is the use of the switch of the present invention by a trainer located remotely from students' STE. Manual operation is still possible. This allows the setting of the rotary switches to an initial position prior to the trainees beginning their testing. This facilitates remote setup and thereby saves the instructor significant time in manually resetting the rotary switches.