Patents Assigned to Hughes Aircraft
  • Patent number: 5731708
    Abstract: A portable integrated circuit die testing system that offers a cost-effective solution for electrically testing bare, unpackaged, integrated circuit chips or die. The system provides for direct electrical interconnection of die of various sizes and thicknesses to an automatic tester without wire bonding or packaging of the semiconductor chip or die. The system includes an X-Y table that is adjustable in horizontal X and Y directions. A contact platform is disposed above the X-Y table that has an opening therein, and is movable in a vertical direction relative to the X-Y table. An adjustment member is coupled to the contact platform for finely adjusting the movement thereof in the vertical direction. A die holder is secured to the X-Y table for holding the die that is to be tested, and in response to movement of the X-Y table. A vacuum connection is provided for drawing a vacuum on the tested die to secure it in the die holder.
    Type: Grant
    Filed: October 31, 1995
    Date of Patent: March 24, 1998
    Assignee: Hughes Aircraft Company
    Inventor: Mohi Sobhani
  • Patent number: 5732384
    Abstract: A method for interactively displaying flight information in an air traffic control system. Flight information lists are displayed relative to associated geographic fixes, and further flight information is displayed pursuant to user selection of an item on a flight list.
    Type: Grant
    Filed: September 8, 1995
    Date of Patent: March 24, 1998
    Assignee: Hughes Aircraft
    Inventors: James W. Ellert, Patricia R. Etter
  • Patent number: 5729016
    Abstract: A low cost night vision system for use in connection with law enforcement vehicles, marine vessels, and other nonmilitary surface vehicles. The invention includes a night vision camera having an array of uncooled detectors. A mechanism is provided for adjusting the pointing angle of the night vision camera in response to scan control signals. Output signals from the uncooled detectors are further processed into a standard video format and displayed on a conventional display located, for example, within a vehicle or marine vessel.
    Type: Grant
    Filed: August 26, 1996
    Date of Patent: March 17, 1998
    Assignee: Hughes Aircraft Company
    Inventors: Stuart H. Klapper, Howard Laitin, Alex L. Kormos, Lacy G. Cook, David M. Masarik, Paul R. Salvio
  • Patent number: 5729230
    Abstract: A continuous-time tunable Gm-C architecture for a .DELTA..SIGMA. modulator includes a tunable resonator and a low bit rate, high sample rate quantizer connected in a feedback loop. The resonator shapes the quantization noise spectrum so that the bulk of the quantization noise occurs outside the signal spectrum. A tunable Gm cell tunes the resonator's resonant frequency to maximize the modulator's SNR. The tunable Gm cell includes a fixed Gm cell having transconductance G.sub.f, a current divider and a recombination circuit that together effectively multiply G.sub.f by a factor .alpha., where -1<=.alpha.<=1, without effecting the cell's common mode current I.sub.cm. A positive current source supplies I.sub.cm, while maintaining a common mode resistance of R/2 and a theoretically infinite differential mode resistance. Thus, the resonator's resonant frequency can be varied from DC to approximately 1 Ghz while maintaining a stable common mode operating point and improving the modulator's quality factor.
    Type: Grant
    Filed: January 17, 1996
    Date of Patent: March 17, 1998
    Assignee: Hughes Aircraft Company
    Inventors: Joseph F. Jensen, Gopal Raghavan, Albert E. Cosand
  • Patent number: 5727000
    Abstract: Test equipment and test methods employing signature analysis to achieve fault isolation of parts contained in digital modules. Fault free signatures of a digital module are stored in a lookup table that are derived from physical measurement or simulation of all parts. All of the parts in the functional digital module are shorted and opened (either physically or by simulation) and each of their resulting faulty signatures are recorded in a storage device. Each signature with its corresponding faulty part is stored in the lookup table or memory. Test input signals are then applied to a tested digital module, and outputs of all parts thereof are applied to masking circuitry which allows sequential selective masking of all parts but one, for each part on the tested digital module. Outputs of the masking circuitry are applied to a multiple input shift register signal analyzer that performs pass/fail signature analysis using the applied signals.
    Type: Grant
    Filed: December 27, 1995
    Date of Patent: March 10, 1998
    Assignee: Hughes Aircraft Company
    Inventor: Stephen V. Pizzica
  • Patent number: 5726600
    Abstract: An active filter circuit component includes an all NPN bipolar tunable Gm cell and a positive current source (PCS) for supplying common mode current. The tunable Gm cell includes a fixed Gm cell having transconductance G.sub.f, a current divider and recombination circuit that together effectively multiply G.sub.f by a tuning factor .alpha., where -1.ltoreq..alpha..ltoreq.1, without effecting the cell's common mode current I.sub.cm. The PCS includes a pair of unity gain inverting single ended amplifiers that are connected in antiparallel across a pair of matched resistors. Alternately, the resistors can be connected across the inverting and non-inverting sides of a differential amplifier. A constant voltage is applied across the resistors to supply I.sub.cm, while maintaining a common mode resistance of R/2 and a differential mode resistance approaching infinity.
    Type: Grant
    Filed: January 17, 1996
    Date of Patent: March 10, 1998
    Assignee: Hughes Aircraft Company
    Inventors: Gopal Raghavan, Joseph F. Jensen, Albert E. Cosand
  • Patent number: 5726915
    Abstract: An automated system and method for testing a sensor by evaluating the output thereof with respect to a known target. The advantageous method includes the step of acquiring an output signal from the sensor in response to a known target, said output including signature signal S, random noise N.sub.R and fixed pattern noise N.sub.FP. Next, the sensor output signal is processed to provide a first signal which includes essentially signature signal S and fixed pattern noise N.sub.FP, a second signal which includes essentially random noise N.sub.R and a third signal which includes essentially fixed pattern noise N.sub.FP. The third signal is adaptively filtered to provide a filtered signal fixed pattern noise signal N'.sub.FP. The filtered signal N'.sub.FP is subtracted from the first signal to extract a signature S. In a particular embodiment, the signature is processed to acquire a modulation transfer function and a signal peak baseline therefrom.
    Type: Grant
    Filed: October 17, 1995
    Date of Patent: March 10, 1998
    Assignee: Hughes Aircraft Company
    Inventors: Kenneth E. Prager, Robby Mauri
  • Patent number: 5724043
    Abstract: An apparatus for measuring the properties of the tropopause includes a variable frequency microwave radiometer operating over a range of from about 118.0 to about 119.0 GHz. The radiometer receives as an input a frequency selector signal and produces as an output a measured power level at a measurement frequency corresponding to the input frequency selector signal. The apparatus further includes a feedback controller having as an input the measured power level and producing as an output the frequency selector signal. The feedback controller varies the frequency selector signal to a target frequency so as to produce a minimum value in the measured power level. The tropopause equivalent altitude is determined from the target frequency.
    Type: Grant
    Filed: July 31, 1995
    Date of Patent: March 3, 1998
    Assignee: Hughes Aircraft Company
    Inventors: Richard C. Savage, James L. Peirce
  • Patent number: 5721161
    Abstract: An epitaxial structure and method of manufacture for a field-effect transistor capable of high-speed low-noise microwave, submillimeterwave and millimeterwave applications. Preferably, the epitaxial structure includes a donor layer and/or buffer layer made from a semiconductor material having the formula AlP.sub.0.39+y Sb.sub.0.61-y.
    Type: Grant
    Filed: November 9, 1995
    Date of Patent: February 24, 1998
    Assignee: Hughes Aircraft Company
    Inventors: Chanh Nguyen, Takyiu Liu, Mehran Matloubian
  • Patent number: 5721503
    Abstract: The number of input latching comparators in a flash analog-to-digital converter is significantly reduced by merging the input latching function into exclusive OR gates used in the converter's decoding section. A latching exclusive OR gate used for this purpose employs resonant tunneling diodes as the latching devices, with hysteresis and impedance elements connected to ensure that the gate latches in a logic state that corresponds to the input analog signal. The latching logic gates operate in a current mode, enabling updated logic states to be latched in response to a periodic clock signal.
    Type: Grant
    Filed: October 26, 1994
    Date of Patent: February 24, 1998
    Assignee: Hughes Aircraft Company
    Inventors: Lawrence M. Burns, William E. Stanchina
  • Patent number: 5716459
    Abstract: A monolithically integrated solar cell microarray includes an isolation layer or multiple isolation layers between a substrate and a solar cell layer, and a trench in the solar cell layer that exposes the isolation layer. Together the isolation layer and trench define solar cells that are spaced apart and electrically isolated on the monolithic substrate. The solar cells are scaled to provide a desired current. Base contacts and integral emitter contact/interconnects connect a number of the scaled solar cells in series to sum their voltages to supply a desired output voltage and current. The trench and integral emitter contact/interconnects are formed using photolithographic etching and liftoff processes, respectively, which are much quicker and less expensive than the conventional dicing and soldering processes.
    Type: Grant
    Filed: December 13, 1995
    Date of Patent: February 10, 1998
    Assignee: Hughes Aircraft Company
    Inventors: Kou-I Chang, David R. Lillington
  • Patent number: 5716030
    Abstract: A spacecraft telescope door (10) adapted for use with remote sensing devices requiring optical and infrared calibration. The door (10) includes a first calibration surface (24) disposed on a first panel (14) for providing a radiant temperature reference for infrared calibrations. A second calibration surface (26) is disposed on a second panel (12) for providing an absolute radiance reference for optical calibrations. A panel hinge (16) controls the relative position of the panels (12,14) with respect to each other, and an aperture hinge (20) controls the relative position of the panels with respect to the aperture (28). In a specific embodiment, the first surface (24) is painted with chemglaze Z306, a highly emissive paint with a low reflectance for facilitating infrared calibration. The second surface (26) is painted with YB71, a diffuse reflective paint for facilitating optical calibration.
    Type: Grant
    Filed: February 6, 1996
    Date of Patent: February 10, 1998
    Assignee: Hughes Aircraft Company
    Inventors: Carlo F. LaFiandra, William M. Rappoport, George R. Huse, Edward F. Zalewski
  • Patent number: 5712000
    Abstract: Diamondlike carbon is deposited on a deposition substrate in a deposition apparatus that can be evacuated and backfilled with a carbonaceous gas. A plasma is generated in the gas by heating a filament within the chamber to produce electrons, and positively biasing the filament with respect to the deposition chamber wall to accelerate the electrons into the carbonaceous gas. The carbonaceous gas dissociates and ionizes in the resulting plasma to produce positively charged carbon ions. A deposition substrate within the chamber is negatively biased with respect to the deposition chamber wall, accelerating the carbon ions so that they are deposited onto the surface of the substrate.
    Type: Grant
    Filed: October 12, 1995
    Date of Patent: January 27, 1998
    Assignee: Hughes Aircraft Company
    Inventors: Ronghua R. Wei, Jesse N. Matossian
  • Patent number: 5709450
    Abstract: An arrangement of an automotive lamp assembly is provided including a reflector housing with a central opening; a discharge light assembly mounted to the reflector through the opening; a base supporting the discharge light assembly in the reflector, the base having a concentric conductor connected to the discharge light assembly at one end and a pin first terminal on an opposite end of the first conductor, and the base having a second eccentric conductor connected to the discharge light assembly on one end with a collar connected on an opposite end; a socket sealed with the base, the socket having a concentric conductor for mating with the base concentric conductor, the socket concentric conductor having a collar terminal at a first end toward the base and a blade terminal at a second opposite end, the socket also having an eccentric conductor having a collar terminal at a first end toward the base and a blade end at a second opposite end; an annular high voltage insulation member surrounding the first end of
    Type: Grant
    Filed: December 27, 1995
    Date of Patent: January 20, 1998
    Assignees: General Motors Corporation, Hughes Aircraft Company
    Inventors: Michael Eugene Francis, Dany Paul Delaporte, Richard Charles Brennan, III, Russell Mistretta Abbott
  • Patent number: 5708473
    Abstract: Methods and systems for encoding data representative of a sequence of video frames for transmission to a decoder. A motion compensated predictive coder (24) substantially losslessly compresses the data, computes a motion vector, and forms an intermediate coded representation which includes the compressed data and the motion vector. A frame detector (26), which detects frames having a prediction error which exceeds a predetermined threshold, is coupled to the motion compensated predictive coder (24). A digital storage device (22) is coupled to the motion compensated predictive coder (24) and the frame detector (26). The digital storage device (22) stores the intermediate coded representation and stores a representation of the frames having the prediction error which exceeds the predetermined threshold. A lossless decoder (29), coupled to the digital storage device (22), substantially losslessly decodes the intermediate coded representation to form a decoded representation.
    Type: Grant
    Filed: August 30, 1994
    Date of Patent: January 13, 1998
    Assignee: Hughes Aircraft Company
    Inventor: Donald Mead
  • Patent number: 5708570
    Abstract: A glass-ceramic substrate for encapsulating an electronic component, with at least two shrinkage control layers restricting shrinkage of the substrate during a co-firing process. The shrinkage control layers are chosen so that they have substantially the same shrinkage characteristics, during co-firing, as the buried electronic component. This results in substantially no differential shrinkage between the electronic component and the substrate, along predetermined directions, during co-firing. In addition, the thermal expansion coefficients of the substrate, shrinkage control layers and electronic component are chosen so that they substantially match, such that their thermal-induced contraction during the cooling phase of the co-firing process substantially match. In the preferred embodiment, the electronic component is buried within the layers of an LTCC structure. The shrinkage control layers are preferably implemented as Al.sub.2 O.sub.3 or TiO.sub.
    Type: Grant
    Filed: October 11, 1995
    Date of Patent: January 13, 1998
    Assignee: Hughes Aircraft Company
    Inventor: Paul W. Polinski, Sr.
  • Patent number: 5707215
    Abstract: Disclosed is a tuned resonant oscillating mass pump, and particularly a pump structure and assembly which can be conveniently and readily mounted inside automotive tires for the purposes of maintaining optimum tire pressure and generating of electrical power from the movement of the tuned oscillating mass in such pumps. The oscillating mass can be a pendulum or a freely moving weight or a ball rolling within an arcuate chamber.
    Type: Grant
    Filed: November 14, 1994
    Date of Patent: January 13, 1998
    Assignee: Hughes Aircraft Company
    Inventors: Ross D. Olney, William S. Griffin, Donald K. Murphy
  • Patent number: 5708425
    Abstract: A sequential messaging method for use in a vehicle detector and classification system having a processor and that uses first and second beams to detect transitions of front and rear ends of a vehicle. The method comprises detecting the vehicle when its front end breaks the first beam, assigning a new vehicle ID number to the vehicle, and transmitting a vehicle detection report containing the vehicle ID number to the processor. The vehicle is detected when its front end passes the second beam, and a vehicle detection update report is transmitted to the processor comprising left edge position, right edge position, range to each edge, vehicle height, and vehicle speed, all of which are derived from the beams reflected from the vehicle. The vehicle is detected when its rear end passes the first beam, and a rear vehicle detection report is transmitted to the processor comprising the left edge position, right edge position, range to each edge, vehicle height, and vehicle speed.
    Type: Grant
    Filed: January 17, 1997
    Date of Patent: January 13, 1998
    Assignee: Hughes Aircraft Company
    Inventors: Douglas Dwyer, Stephen J. Feitelson
  • Patent number: 5708283
    Abstract: A high power, flip-chip microwave monolithic integrated circuit (MMIC) assembly (30) has a high power microwave monolithic integrated circuit (MMIC) having a surface with an active area (72) in which heat is generated. The assembly also has a host substrate (34). A thermally conductive bump (51) formed over the surface of the MMIC has a first portion (51') in close proximity to and in thermal communication with the active area (72) of the MMIC and a second portion (51") which is in close proximity to and in thermal communication with the host substrate (34). The second portion (51") of the thermal bump (51) has a greater cross-sectional area than the first portion (51'). A multi-layer, multi-exposure method of manufacturing the improved thermal bump (51) includes several steps. A plating membrane (80) is formed on a surface of the MMIC (32). A first layer of negative photoresist is applied to the surface of the plating membrane (80), and is exposed with a first masked pattern of light.
    Type: Grant
    Filed: December 20, 1996
    Date of Patent: January 13, 1998
    Assignee: Hughes Aircraft
    Inventors: Cheng P. Wen, Wah S. Wong, William D. Gray
  • Patent number: 5708747
    Abstract: A fiber-based delivery system and method for delivering pulsed high power optical radiation (14) over longer fiber lengths than prior fiber-based systems comprises a fiber bundle (10) and a beam launcher (12) that directs a high power optical beam (14) to an input end (18) of the fiber bundle (10), and distributes it over the individual fibers (22) in the bundle. The number of fibers (22) is large enough so that substantially all of the individual fibers (22) are subjected to an optical intensity level below that required to induce substantial nonlinear optical losses. In addition, the diameters of the individual fiber cores (34) are small enough so that the modal dispersion experienced by the optical beam (14) does not exceed approximately 80 ns/km. In a preferred embodiment for transmission of pulsed 1.06 micron light, the fiber bundle (10) comprises 96 individual fibers (22), with respective core (34) diameters of approximately 600 microns, that are encapsulated in a jacketed adhesive (30).
    Type: Grant
    Filed: April 18, 1996
    Date of Patent: January 13, 1998
    Assignee: Hughes Aircraft Company
    Inventor: Thomas M. Danckwerth