Abstract: Aerial dispersion systems that may be employed to allow rapid and temporary conversion of aircraft for aerial dispersion purposes, such as aerial fire-fighting. The aerial dispersion systems may be implemented using modular components that may be configured for compatibility with conventional cargo loading and unloading systems of modern aircraft, including side-loading cargo systems of wide body passenger and cargo aircraft having high lift capacities. The aerial dispersion systems may be rapidly installed in a large fleet of high capacity aircraft in response to a wildfire or other rapidly-developing emergency such as an oil spill, chemical or biological contamination incident, building or refinery fire, etc. After use, the aircraft of the fleet may be rapidly de-modified and returned to original condition.

Abstract: A method for enhancing the Bluetooth transmission speed and robustness of an emitting end and a receiving end is provided. The method is utilized in a system having an emitting end and a receiving end, wherein at least one of the emitting and receiving ends is provided with BlueSPEED-PSK or BlueSPEED-DELTA-PSK (adapted Gray coded D16PSK) modulation with optional FEC.

Abstract: A line of sight antenna supported in an upturned terminal winglet or similar vertical member of an aircraft is disclosed. An aperture is formed in the conductive winglet or vertical member, and the antenna is supported within the aperture by a support mechanism such that the antenna is exposed to the line of sight transmissions. A non-conductive covering may also be used for the aperture. Using the cover, the antenna within the winglet can be configured so that it does not alter the appearance or aerodynamic characteristics of the aircraft. Alternatively, the antenna can be coupled to the outside of the winglet or vertical member if cosmetics are not a concern. The frequency range of the antenna can be tuned to cover desired frequency ranges. The antenna position at the winglet maintains a large physical separation from fuselage-mounted antennas thereby reducing interference.

Abstract: An aircraft stringer clip and related methods are disclosed that provide an apparatus for attaching aircraft elements to an aircraft stringer. In one embodiment, the stringer clip is a three-piece clamp assembly spanning the width of an aircraft stringer and including a single bottom member and two opposing top members that are configured to be engagingly coupled. The top and bottom members of the stringer clip are preferably made of rigid, but light-weight and flame retardant material.

Abstract: A system for data processing comprises a host circuit (104) and an integrated circuit (102), the host circuit (104) being external to the integrated circuit (102). The integrated circuit (102) includes a plurality of programming elements (300), each element (300) including a host interface (606) for receiving data and a first control signal from the host circuit (104), a control interface (604) for receiving a second control signal. Each element (300) includes a crosspoint switch (318), and a register array (628) for receiving and storing data from the crosspoint switch (318) according to the first and second control signals, for receiving and storing data from the host interface (606) according to the first and second control signals, and for communicating stored data to the crosspoint switch (318) according to the first and second control signals.

Abstract: Provided is a method and system for signal-driven recovery of a digital pulse stream. The method includes receiving initial parameters including the base characteristics of a pulse signal, the characteristics including the maximum pulse interval. An incoming analog signal is converted to a digital signal and sampled a predetermined number of times at intervals greater than the maximum pulse interval to record a set of minimum signal values and a set of maximum signal values. Each set is averaged to provide an average minimum value and an average maximum value. Based on these values at least one threshold value is then determined, and the digital pulse stream is identified based on the threshold values. The method is repetitive, continually re-determining the threshold values so as to adapt to changes in the incoming signal. A system for performing the method is also provided.

Abstract: A Hall sensor comprises two separate wells and each having respective contacts provided thereover. An oppositely directed bias current is supplied via contacts. Accordingly, a differential signal can be obtained from the two output contacts. As in each well the middle contact can be precisely centred between the two outer contacts, the intrinsic offset is small. The sensor 300 can be subjected to reversed operation by reversing the bias current direction. This provides a sensor with a low and temperature-stable offset.

Abstract: Systems and methods for rotating objects that shift the center of gravity of an object, such as a wing assembly, from a position outside the rotation axis area of the object to a position within the rotation axis area of the object. In one example, a material handling system that employs rotatable slings may be used to rotate an object by shifting the suspended center of gravity from a position outside the rotation axis area (i.e., outside the rotatable slings in at least one position of rotation) to a position within the rotation axis area (i.e., between the slings at all positions of rotation). The suspended center of gravity may be shifted using at least one ballast component (or other suitable force-applying device) that exerts a force on the object in a direction and magnitude sufficient to so shift the suspended center of gravity of the object.

Abstract: A three dimensional spatial imaging system (10) for generating a three dimensional model of a scanned space includes: a laser rangefinder (42) that obtains spatial data by measuring distances to a plurality of target points within the scanned space; a rotating mirror (46) placed in a path of a laser beam (43) emitted from the laser rangefinder (42), the mirror (46) deflecting the laser beam (43) to varying degrees as the mirror (46) is rotated; a digital camera (52) that obtains image data from photographs of the scanned space; a rotating head (30) on which the laser rangefinder (42), mirror (46) and camera (52) are all mounted, the head (30) rotating up to 360 degrees about a central axis of rotation (64) that is substantially normal to a plane in which the head (30) is rotated; and, a data processor that maps color information from the image data obtained by the camera (52) to the corresponding target points of the spatial data obtained by the laser rangefinder (42).

Abstract: A method and system includes at least one interconnect hub, connecting the at least one interconnect hub to a plurality of audio connection devices to form a network of audio connection devices with the interconnect hub at the center of the ring. The audio connection devices are connected to each other through the at least one interconnect hub, and data is synchronously transmitted between at least two of the audio connection devices through the at least one interconnect hub.

Abstract: A system for data processing comprises a host circuit (104) and an integrated circuit (102), the host circuit (104) being external to the integrated circuit (102). The integrated circuit (102) includes a plurality of programming elements (300), each element (300) including a host interface (606) for receiving data and a first control signal from the host circuit (104), a control interface (604) for receiving a second control signal. Each element (300) includes a crosspoint switch (318), and a register array (628) for receiving and storing data from the crosspoint switch (318) according to the first and second control signals, for receiving and storing data from the host interface (606) according to the first and second control signals, and for communicating stored data to the crosspoint switch (318) according to the first and second control signals.

Abstract: Tools and techniques for suppressing fires. Such tools might transmit a signal that generates one or more waves (which might be mechanical waves, electromagnetic waves, and/or the like) that is sufficient to disrupt the relationship between the electrons in a fire and the ionized nuclei to which those electrons are attracted. The resulting repulsion (between the nuclei and/or the electrons) that form the plasma of the fire can serve to disperse the plasma, thereby suppressing the fire.

Abstract: A system for data processing comprises a host circuit (104) and an integrated circuit (102). The integrated circuit (102) is in communication with the host circuit (104) and the host circuit (104) is external to the integrated circuit (102). The integrated circuit (102) includes a plurality of programmable elements for data processing (300), each programmable element (300) including a host interface (305) for receiving host data and a host control signal from the host, a crosspoint switch (318), and an interpolation module (310). The host data includes a serial stream of input data values. The interpolation module (310) selectively inserts one or more interpolation data values, such as zero, between selected ones of the input data values according to the host control signal, and communicates the input data values and interpolation data values to the crosspoint switch (318).

Abstract: A method and device for computing the multiplicative inverse of element x in Galois field GF(p2m) is proposed. In particular, when p is a prime number and m is an integer, the inverse may be constructed based on the observation that xpm+1 is en element in sub-field GF(pm) and the inverse of xpm+1 can be carried out in the sub-field. The inverse of X may be obtained by multiplying x?1=(xpm+1)?1 by xpm.

Abstract: A geolocation system (10) includes an emitter (12), a plurality of collection nodes (14,16,18), and a control station (20). Each collection node includes a receiver (24) that is operable to receive signals transmitted from the emitter (12), generate a reduced data stream that includes only signal data, and communicate the reduced data stream to the control station (20) along with navigation data. The receiver (24) identifies signal data by detecting an energy level of the raw collection data. More specifically, the receiver (24) determines a bandwidth and a signal-to-noise ratio of each portion of the collection data, and identifies each portion as including signal data if both the bandwidth and the signal-to-noise ratio exceed predetermined threshold amounts. The receiver (24) includes a digital signal processing component (36) for performing calculations used by the receiver (24) to determine the bandwidth and the signal-to-noise ratio.

Abstract: A temperature sensor is formed from three initially unfired (or green) ceramic substrates. The first substrate has a temperature sensitive means printed on a first surface. Additionally first and second conducting elements are also printed thereon. The third substrate has a temperature sensitive means in the form of a resistor printed on a first surface. Additionally first and second conducting elements and are also printed thereon. The second substrate is provided with a conducting via in the form of a hole extending through the substrate, the hole being filled with conductive material. The via is adapted to be aligned with the ends of conducting elements. To construct the sensor the first surfaces of substrates are aligned with substrate such that via is aligned with conducting elements. The substrates are then pressed together. Subsequently the substrates are fired to provide the completed sensor.

Abstract: A communications system and protocol for use in a non-dominant bit radio network. The radio network includes transceivers which communicate with other transceivers to allow network variables to be shared by all transceivers. The protocol allows the network to handle collisions between competing transmissions from different transceivers. The protocol also handles communications between transceivers that are out of transmitting range of each other.

Abstract: A system for identifying phase transitions in phase-shift keying signals and frequency transitions in frequency-shift keying signals broadly comprises a memory and a computing element capable of: selecting a portion of the signal to analyze, wherein the signal comprises a plurality of data samples; applying a transform to the signal to obtain a frequency spectrum; determining a maximum frequency spectrum corresponding to a carrier frequency; determining a starting approximation value of a slope of the phase transition; calculating a bounded limit of slopes within which to search for the phase transition; selecting a plurality of lines; calculating a sum for the data samples associated with each of the lines; and based on the sum for the data samples, identifying a line that corresponds to a location of the phase transition.

Abstract: Systems and methods for determining the occurrences of pulses for implementing a pulse count monitoring method for driving a brushed DC motor driven by a pulse width modulated (PWM) driving current. The method comprises acquiring the driving current signal; performing peak detection on the acquired signal; identifying the largest peaks and thus determining the occurrence of pulses. The peak detect is implemented by fast peak detection or diode peak detection operable to detect appropriate peak widths as determined by the chosen PWM frequency, duty cycle and PWM pulse height.

Abstract: Systems and methods for detection and geolocation of multiple emitters that are emitting RF signal energy on a common frequency, and that may be implemented to separate, geolocate, and/or determine the number of emitters (e.g., radio users) emitting on a common RF frequency. Real-time signal qualification processing may be employed to continuously monitor and collect incoming receiver tuner data for signal activity and ignore irrelevant noise data. Each set of data blocks from an emitter transmission signal may be defined as an emission cluster, and a set of time difference of arrival (TDOA)/frequency difference of arrival (FDOA) pairs may be computed for each emission cluster with each TDOA/FDOA pair yielding a geolocation result. A statistical qualification method may be used to produce a final geolocation answer from each set of emission cluster geolocation results, and a geolocation error ellipse computed for the final geolocation answer of each emission cluster.