Abstract: Methods and systems for analyzing engine unbalance conditions are disclosed. In one embodiment, a method includes receiving vibrational data from a plurality of locations distributed over an engine and a surrounding engine support structure, and inputting the vibrational data into a neural network inverse model. The neural network inverse model establishes a relationship between the vibrational data and an unbalance condition of the engine, and outputs diagnostic information indicating the unbalance condition of the engine. In a further embodiment, a method further includes subjecting the vibrational data to a Fast Fourier Transformation to extract a desired once per revolution vibrational data prior to input to the neural network inverse model.

Abstract: Methods and systems for analyzing engine unbalance conditions are disclosed. In one embodiment, a method includes receiving vibrational data from a plurality of locations distributed over an engine and a surrounding engine support structure, and inputting the vibrational data into a neural network inverse model. The neural network inverse model establishes a relationship between the vibrational data and an unbalance condition of the engine, and outputs diagnostic information indicating the unbalance condition of the engine. In a further embodiment, a method further includes subjecting the vibrational data to a Fast Fourier Transformation to extract a desired once per revolution vibrational data prior to input to the neural network inverse model.

Abstract: Propagation of a mobile platform's public IP address though Internet service providers is monitored as the mobile platform is handed-off from a first ground station to a second ground station. The mobile platform's public IP address is removed from the first ground station. The first ground station is checked to determine whether the mobile platform's public IP address is no longer present there. After a predetermined period, the second ground station is checked to determine whether the mobile platform's public IP address is no longer present at the first ground station. The mobile platform's public IP address is added to the second ground station. The second ground station is checked to determine whether the mobile platform's public IP address is now present there. After a predetermined period, the first ground station is checked to determine whether the mobile platform's public IP address is now present at the second ground station.

Abstract: Systems and methods are provided for simulating a target platform. An incoming radar signal is transmitted from a radar source and is received at a first platform. Time of the received radar signal is modulated to generate first and second range extent signals. The first range extent signal is vector modulated, and the second range extent signal is divided into a plurality of divided second range extent signals. A first of the plurality of divided second range extent signals is phase modulated. A second of the plurality of divided second range extent signals is amplitude modulated. The modulated signals are transmitted from the first platform.

Abstract: Exemplary methods and systems manage a mobile network. A mobile network node is managed when the node is connected to the network. However, an alarm is not necessarily generated when the node is not connected to the network. A status message is periodically generated and transmitted from the mobile network node to a network control facility. The status message may include any status information regarding the mobile network node as desired. When the status message is indicative of a predetermined condition, an alarm is automatically generated. When no status message is received from the mobile network node, a determination is made whether connectivity exists between the mobile network node and the network. If connectivity does not exist between the mobile network node and the network, then no alarm is generated. If connectivity does exist between the mobile network node and the network, then an alarm is generated.

Abstract: Methods and systems for analyzing engine unbalance conditions are disclosed. In one embodiment, a method includes receiving vibrational data from a plurality of locations distributed over an engine and a surrounding engine support structure, and inputting the vibrational data into a neural network inverse model. The neural network inverse model establishes a relationship between the vibrational data and an unbalance condition of the engine, and outputs diagnostic information indicating the unbalance condition of the engine. In a further embodiment, a method further includes subjecting the vibrational data to a Fast Fourier Transformation to extract a desired once per revolution vibrational data prior to input to the neural network inverse model.

Abstract: Bidirectional video teleconferences are provided on a mobile platform. A first video teleconference terminal is disposed on a mobile platform. A first local area network is arranged to provide network data services on the mobile platform and is arranged to communicate with the first video teleconference terminal. A second local area network is arranged to provide network data services and is arranged to communicate with a second video teleconference terminal. The first and second local area networks are in bidirectional packet data communications, and packets of video teleconference data are prioritized over packets of data for services other than video teleconferencing.

Abstract: Systems, methods, and computer program products are provided for accurately measuring frequency-and/or-phase-related parameters of a sinusoidal signal that varies non-linearly in frequency or phase. A sinusoidal signal is sampled over a finite period of time at a plurality of sample points. The sampled signals are pre-processed, and a Fourier transform is performed on the pre-processed sampled signals. Phases of the pre-processed sampled signals are extracted from the Fourier transform, and a measurement indicative of frequency of the sinusoidal signal is determined from slope of the phases of the pre-processed sampled signals. Range to a target may be determined using the exemplary signal processing described above on laser radar interference signals.

Abstract: Methods and systems are provided for evaluating electrical characteristics of a transmitter in real time using cross-correlation of a reference signal with a signal transmitted by the transmitter. A code generator is configured to generate reference code and test code that both include a plurality of frames of data. The reference code is output at a first rate and the test code is output at a second rate that is different from the first rate. A modulator is configured to modulate the reference code into a first modulated code. A correlator is configured to correlate the first modulated code with test code that has been modulated and transmitted by a transmitter.

Abstract: A portable ice rescue craft includes a plurality of locking raft sections that are foldable for storage and transport. A drive unit includes a drive wheel driven by an electric motor via a drive belt. The drive wheel may include a plurality of spikes configured to engage ice and a plurality of paddles that are centripetally urgeable outward to pull the rescue craft through water. A forward raft section may include a pair of outboard pontoons to provide stability and minimize lateral rocking. An aft raft section includes at least one rudder. A pair of rudders may be mounted to a plate on a pivoting, biased system. The rudders automatically fold upwardly when the ice rescue craft is on ice or land. The rudders automatically activate downwardly when the ice rescue craft is in water.

Abstract: The present invention provides an aircraft engine vibration system that provides information about engine health. Embodiments of the present invention monitor for excessive vibration, monitor for bird strike, monitor for ice build up on the fan section, and monitor general engine health. An embodiment of the present invention utilizes neural network architecture for the detection of excessive vibration and ice detection build-up on the fan section of a turbo-fan engine and to monitor engine health through the high-pressure turbine section of the engine.

Abstract: A passive terminator between a plurality of nodes includes a first voltage divider configured to passively set a differential voltage level between a first voltage level and a second voltage level. The first voltage divider has a Thevenin resistance and is electrically connectable to a first node. At least a second voltage divider is configured to passively set the differential voltage level between the first voltage level and the second voltage level. The second voltage divider has the Thevenin resistance and is electrically connectable to at least a second node. A transformer is electrically connected between the first voltage divider and the at least second voltage divider. The transformer has a reactance that is substantially greater than the Thevenin resistance of the first voltage divider and the at least second voltage divider.

Abstract: A heat transfer cover mitigates temperature changes of an object. A cover body is configured to receive the object. A plurality of heat transfer channels are defined in an interior of the cover body. The channels are arranged to transport a heat transfer fluid in thermal communication with the object. An inlet port is configured to connect the plurality of channels with a source of the heat transfer fluid. An interior surface of the cover body may substantially conform to a shape of an exterior of the object. A plurality of lands may be defined in the interior of the cover body. The lands are arranged to engage the exterior of the object. The heat transfer channels may be defined between adjacent lands. At least a first end of the cover body may define an opening. The at least first end and the object are substantially sealed at the opening.

Abstract: A squib firing device is constructed to test and fire a squib load being applied to the squib firing device. A power supply of the squib firing device conditionally stores and discharges a squib firing power, which is a function of an analog OR of a first voltage from an external power source and a second voltage from a battery source of the squib firing device. When the squib firing power is being stored by the power supply, the squib firing device establishes a flow of a squib testing current through the applied squib load to thereby detect a resistance of squib load. When the squib firing power is being discharged by the power supply, the squib firing device establishes and regulates a flow of a squib firing current through the applied squib load to thereby fire squib load.

Abstract: Systems and methods enable numerically creating a flat field in a compact radar range with a curved reflector, and without use of a separate phased array of elements, at frequencies lower than those that are possible with currently known, reflector-only compact radar ranges. A compact radar range is calibrated to enable weighting factors to be computed. The weighting factors may be computed by performing an optimization algorithm. The weighting factors are used to weight separate target signals sequentially returned from a target zone such that, when combined, a numerically composite measurement has a substantially constant magnitude across the target zone.

Abstract: An exemplary calorimeter includes a body configured to capture radiation generated by a source of the radiation, such as without limitation a laser, and absorb energy from the captured radiation. The calorimeter is simple to manufacture, operate, and maintain and is compact, highly accurate, able to withstand high power beams, and self-calibrating. NIST traceable electrical wires are used for the measurement. No fluids are used during measurements of the input radiation. A simple built in fluid or gaseous cooling system may be used post-measurement to reset the calorimeter temperature back to ambient for repeated measurement capability.

Abstract: A transformable airplane may be reconfigured easily and rapidly to perform any one or a combination of tanking, transport, bombing, or command and control missions as desired for a tactical situation by installing or replacing mission-specific modules as desired. A reconfigurable aircraft includes a pair of wings and an aircraft body having at least one bay defined in an interior of the aircraft body. The at least one bay is configured to accept a plurality of removably replaceable modules that configure the aircraft to perform a plurality of missions. Transport mission modules may include space and tie-downs for cargo pallets and/or palletized seating. A roll-on/roll-off ramp may be provided. Tanking mission modules may include a remote aerial refueling operator station. Bombing mission modules may include a bomb rack and a bomb ejector. ISR mission modules may include command and control stations in signal communication with phased array antennas.

Abstract: A device for capturing radiation includes multi-axis, multiple chambers with two dimensional geometry. A first chamber has a first axis and is configured to receive a beam of radiation and absorb a portion of the beam of radiation. A second chamber has a second axis that is not collinear with the first axis. The second chamber is configured to receive at least a portion of the beam of radiation and absorb at least a portion of the beam of radiation. In one preferred embodiment, the second chamber terminates at a vertex. Additional chambers may be provided, as desired, with axes not collinear with either the first chamber, the second chamber, or any other chamber such that the plurality of chambers absorb substantially all of the radiation.

Abstract: Embodiments of the present invention provide a gliding submersible transport system. Exemplary submersible gliders have wings capable of providing sufficiently high lift-to-drag ratios such that the submersible gliders of may be used for transporting large volumes of military or commercial hardware, equipment, personnel, or the like. According to one exemplary embodiment of the present invention, a submersible glider has a step-wise glider range. The glider includes a substantially cylindrical hull having a bow and a stern. A generally planar lifting surface is disposed toward the stern. The lifting surface has a pair of generally planar stabilizer surfaces that extend generally perpendicular to a plane of the lifting surface from ends of the lifting surface. A nose cone and at least one steering device are disposed toward the bow.

Abstract: The present invention provides a ventilated seating system. The ventilated seating system provides a back rest portion including an upper end and a lower end and a perforated duct positioned adjacent to the lower end of the back rest portion. The ventilated seating system further provides a seat base portion including a front end and a back end with the back end positioned adjacent to the perforated duct, and wherein air is drawn across a surface of the seat base portion and a surface of the back rest portion without passing through the seat base and the back rest portions, and into the perforated duct. The ventilated seating system may utilize a pressure differential to draw the air into the duct. To enhance operation, the system may further include adjustable perforated ducts. The adjustable perforated ducts may be adjusted manually or mechanically.