Abstract: A reliable delivery protocol for wireless networks, where a source node applies network forward error correction coding such that no transmission is ever repeated, instead all retransmissions and relay transmissions use coded packets further out in the coding sequence so that intermediate and destination nodes can make maximal use of overheard transmissions.

Abstract: A multimode display for night vision imaging system (NVIS) compatible operation including a display assembly including a display subassembly having a display component; and, a backlight printed wiring board (PWB) assembly positioned behind the display subassembly. The backlight printed wiring board (PWB) assembly includes a printed wiring board (PWB). A top side mounted LED array is mounted on a first side of the printed wiring board (PWB) including a top side plurality of LEDs including a top side set of white LEDs. A reverse-mounted LED array is mounted on a second side of the printed wiring board (PWB) including a reverse-mounted plurality of LEDs including a reverse-mounted set of white LEDs. A dedicated primary IR filtering means is operatively associated with the reverse-mounted LED array for conditioning light emitted from the reverse-mounted LED array for NVIS compatible operation. In a day mode of operation the forward-side mounted LED array illuminates the display subassembly.

Abstract: A communication system comprises a covert channel detector. The covert channel detector can be used in a multi-level security system (MLS) or multiple single levels of security (MSLS). The covert channel detector detects covert channels in a cryptographic system. The cryptographic system can be used in a military radio system.

Abstract: A system determining whether the shielding on a shielded signal or power cable has been compromised without the need of detaching the cable. A special-made cable is used with a dedicated shielding surveillance conductor and a process for injecting a known current on the shield of the cable and monitoring a voltage on the shielding surveillance conductor.

Abstract: A turbulence data circuit for use in an aircraft. The aircraft can include a radar system configured to transmit a first radio frequency wave and receive a second radio frequency wave and a display for receiving a display signal representative of turbulence. The aircraft can further include a flight management system configured to determine a phase of flight, an aircraft inertial/air data system configured to determine an altitude and an airspeed. The turbulence data circuit can include an interface for coupling to the radar system, the display, the flight management system, and the aircraft inertial/air data system. The turbulence data circuit can be configured to determine the display signal representative of turbulence based on at least one of the phase of flight, the altitude, the airspeed and the second radio frequency wave.

Abstract: The present invention is directed to low-cost, low-processing temperature, and simple reinforcement, repair, and corrosion protection for hermetically sealed modules and hermetic connectors. A thin layer of glass is applied over the module's seal or the connector' glass frit. The layer of glass comprises an alkali silicate glass. The layer of glass is produced from a material which is a low viscosity liquid at room temperature prior to curing and is cured at low temperatures (typically no more than about 160 degrees Celsius). Subsequent to curing, the layer of glass is intimately bonded to the seal, watertight, and is stable from about negative two-hundred forty-three degrees Celsius to at least about seven-hundred twenty-seven degrees Celsius. The glass layer provides corrosion protection, seals any existing leaks, and possesses good flexibility and adhesion. The resulting bond is hermetic with good aqueous durability and strength similar to that of monolithic structures.

Abstract: A spoofer location system includes a number of receivers that receive positioning signals. A data engine receives information from the receivers and determines a location of a spoofer source signal. The location of the spoofer source signal is determined by determining a range from each of the number of receivers to the source. The system can be employed in a global positioning system. The spoofer location system can be utilized with guided munitions and other vehicles.

Abstract: The present invention is directed to the graphical selection of objects. A selection indicator, one or more object indicators, and a position indicator are presented on a display. The selection indicator may be manipulated to indicate object indicators by rotating the selection indicator until an object indicators is within the area of the selection indicator and to select an object indicator which has been indicated. The selection indicator may be rotated so a portion overlaps with the location occupied by a portion prior to rotation. A menu indicator is also presented on the display. The menu indicator comprises a selector icon and a list of representations of the object indicators indicated by selection indicator. The selector icon may be manipulated to indicate a single representation of an object indicator and to select the object indicator represented by the representation of the indicated object indicator.

Abstract: A system and method for presenting an image of terrain threats are disclosed. Substantially transparent terrain symbols (color or monochrome) are depicted where each symbol is representative of a level of threat. Terrain symbols may overlay a weather image without a loss in information. A system is disclosed which comprises a navigation system, a terrain database, an image processor, and an indicating system. The navigation system acquires navigation data representative of aircraft position and direction; the database stores data of a plurality of cells; and the indicating system receives image data and presents symbols representative of the terrain image. The image processor receives navigation data defines a range of elevations of threat levels based upon the aircraft altitude, receives terrain data from the terrain database, determines the terrain threat of each cell, and provides an image representing the threat level and locations to the display.

Abstract: A system and method of determining an available frequency sub-band for radio traffic in a multiple node radio network is disclosed. The method and system provide for communication over a radio frequency band, the radio frequency band comprising radio frequency sub-bands and providing a radio node group of at least one radio communications devices configured to broadcast and receive on the radio frequency band. The system and method create a time for a window of radio broadcast silence on at least one of the radio frequency sub-bands by the radio node group. The system and method survey the at least one of the radio frequency sub-bands during the window of radio broadcast silence. The system and method choose, based on the survey, a radio frequency sub-band for broadcast from the radio frequency band.

Abstract: A log periodic antenna comprises a plurality of radiating elements in an end fire configuration, each radiating element in the plurality of radiating elements comprises a conductor, and at least two shunt inductances connected to the conductor; a substrate connecting the plurality of radiating elements; and a log periodic stripline feed pathway superimposed on the substrate. The height of each radiating element of the plurality of radiating elements is about one hundredth the size of the wavelength and the length is about 0.14 the size of the wavelength at the lowest operating frequency of the log periodic antenna. The plurality of radiating elements is configured to produce impedance and radiation characteristics that are regularly repetitive as a logarithmic function of an excitation of frequency without performance degradation.

Abstract: The present invention is directed to a multifunctional cellular modem for an aircraft computing device (ACD). The ACD is connectible to a wireless handheld cellular communication device. The ACD may utilize the wireless handheld cellular communication device as a cellular modem to download a file. Alternatively, the wireless handheld cellular communication device may include a storage media and may download the file and store the file in the storage media. Then the ACD may download the file from the storage media of the wireless handheld cellular communication device. The ACD may be installed in the aircraft and may be operable to install the downloaded file in the aircraft. By utilizing the present invention, an ACD is operable to provide a file for an aircraft without requiring costly dedicated PCMCIA (Personal Computer Memory Card International Association) cellular cards and service contracts for every ACD.

Abstract: A runway identification system including a weather radar system. The weather radar system includes a receiver. The receiver is configured to receive a runway characteristic signal from a transponder associated with a runway. The runway identification system determines a runway identification based on the runway characteristic signal.

Abstract: A method of integrating a detected signal along a given angle of arrival to improve detection. The method includes receiving the signal at a first antenna, receiving the signal at a second antenna, generating a phase difference trajectory based on the signal from the first antenna and the signal from the second antenna, and extracting a signal by integrating the phase difference trajectory over frequency for a plurality of angles of arrival.

Abstract: A radio system comprises a power source and a power amplifier circuit coupled to the power source on a power line. The radio system also comprises an active cancellation circuit. The active cancellation circuit comprises a bi-directional DC-DC converter. The active cancellation circuit is configured to cancel low-frequency emissions from the power amplifier circuit on the power line.

Abstract: The present invention is directed to a quick, low-distortion and efficient reduction in sample rate requiring minimal logic. An IF signal is passed into an analog-to-digital converter. The converted signal is mixed with the combination of an in-phase and a quadrature component. The mixed signal is then split into an in-phase signal and a quadrature signal. The quadrature signal is interpolated to form a new signal aligned in time to the in-phase signal. Alternatively, the in-phase signal is interpolated to form a new signal aligned in time to the quadrature signal. The interpolation may comprise linear interpolation or parabolic interpolation. The simplified signal processing reduces the sample rate of the signal and the interpolation reduces aliasing introduced by the simplification. One advantage of this approach is that only half of the signal needs to be processed.

Abstract: A method of determining an angle with a beam to terrain for a terrain avoidance system includes receiving first data associated with first returns associated with a first portion of an antenna. The method further includes receiving second data associated with second returns associated with a second portion of the antenna, wherein the first portion is different than, intersects, or includes the second portion. The method further includes determining the angle to terrain using the first data and second data.

Abstract: A radar system includes an antenna and has short range detection capability. The radar system includes a receiver coupled to the antenna for receiving a receive signal associated with a pulse compressed transmission signal and a matched filter configured to accumulate at least a portion of the receive signal for a particular range. The portion of the receive signal is associated with a corresponding portion of the pulse compressed transmission signal.

Abstract: A method for detecting carrier wave dropout may include but is not limited to: a) receiving a carrier wave; b) determining a carrier wave power; c) applying a Kalman filter to the carrier wave power; d) detecting a decrease in carrier wave power; and e) delaying a transmission of the carrier wave to a demodulator. A system for detecting carrier wave dropout may include, but is not limited to: a) circuitry for receiving a carrier wave; b) circuitry for determining a carrier wave power; c) circuitry for applying a Kalman filter to the carrier wave power; d) circuitry for detecting a decrease in carrier wave power; and e) circuitry for delaying a transmission of the carrier wave to a demodulator.

Abstract: A display screen device may comprise a first substrate including at least a substantially transparent glass having a thickness less than or equal to 1.1 millimeters; an anti-reflective thin film coating; and a second substrate including a touch screen device. Additionally, a method for providing a display screen device is disclosed.