Patents Represented by Attorney H. P. Gortler
  • Patent number: 5764414
    Abstract: A biocular display system (19) for generating a virtual image (30) of a visible display (20). A diffractive binary optical element (22) is used to create the virtual image (30). The binary optical element (22) contains magnifying power to increase the size of the virtual image (30). Also, the binary optical element (22) contains prismatic power to displace the virtual image (30) away from the display (20). Multiple displays (40), (42) may be viewed by employing a binary optical element (34) having multiple diffractive orders.
    Type: Grant
    Filed: August 23, 1993
    Date of Patent: June 9, 1998
    Assignee: Hughes Aircraft Company
    Inventors: William B. King, Chungte W. Chen
  • Patent number: 5485038
    Abstract: A High-Density-Multi-Chip (HDMI) substrate structure (10) includes alternating conductor metallization (24,28,36,54,56) and insulating dielectric layers (14,38). The dielectric layers (14,38) are formed by curtain coating of ultraviolet photoimageable epoxy material, and the metallization (24,28,36,54,56) is formed by electroless plating or sputtering of copper. The dielectric layers (14,38) are photoimaged and developed to form via holes (16,40,44), and vias (18,42,46) are formed in the holes (16,40,44) by electroless copper plating. The metallization (24,28,36,54,56) can be formed in the same manner as the dielectric layers (14,38), or can alternatively be formed by subtractive photolithography using photoresist masks.
    Type: Grant
    Filed: September 12, 1994
    Date of Patent: January 16, 1996
    Assignee: Hughes Aircraft Company
    Inventors: James J. Licari, Deborah J. Smith
  • Patent number: 5485306
    Abstract: The optical sensor (10) has a multiple telescope assembly (12), a rotating periscope assembly (14), an imager optical system (16) and a detector (18). The sensor (10) may be utilized with visible, ultraviolet or infrared wavelength radiation. Each telescope (12) views a particular sector of a scene. The rotating periscope (14) multiplexes the output of each telescope (12) to provide a combined wide field of view of each of the sectors. The system may be used in various types of navigation, pilotage, and monitoring systems.
    Type: Grant
    Filed: November 13, 1992
    Date of Patent: January 16, 1996
    Assignee: Hughes Aircraft Company
    Inventors: Paul C. Kiunke, Dean C. Hatfield, Jr., Reynold S. Kebo
  • Patent number: 5479025
    Abstract: A boresight thermal reference source capable of rapidly providing a uniform high intensity Infra-Red signal, comprises a boresight source housing, a ceramic rod, and a heater wire helically surrounding, at least partially, the ceramic rod. The coiled heater wire has a plurality of turns extending outwardly from one end of the ceramic rod forming a blackbody cavity therein from the plurality of outwardly extending turns on the end of the ceramic rod. The small mass of the ceramic rod, optimum geometry of ceramic rod, heater wire, and housing for reduced heat loss, and the aforementioned blackbody cavity configuration, all provide for low operating power with uniform rapid heating of one end (ceramic floor) of the ceramic rod to about 1000.degree. C.
    Type: Grant
    Filed: November 18, 1994
    Date of Patent: December 26, 1995
    Assignee: Hughes Aircraft Company
    Inventors: Lee J. Huniu, Charles N. Boyar
  • Patent number: 5471240
    Abstract: A scene based nonuniformity correction method (40) that computes and applies offset correction errors to a video signal corresponding to an image derived from a imaging sensor (11). A video signal derived from the sensor (11) is processed such that a vector representing offset correction terms is formed, and this vector is initially set to zero. Each element in this vector represents a correction term for a particular detector of the sensor (11). The vector is applied to each pixel of the image by a processor (13) as the pixels are read from the sensor (11). To measure the offset error, the image is separated into vertically oriented regions, each comprising a plurality of channels. The average of each channel within a region is computed (42), and a set of region vectors is foraged, such that there is one region vector for each region. Each region vector is then globally high-pass filtered and then edges larger than a predefined threshold are detected (43), and marked (44).
    Type: Grant
    Filed: November 15, 1993
    Date of Patent: November 28, 1995
    Assignee: Hughes Aircraft Company
    Inventors: Kenneth E. Prager, Stephen J. Herbst, Jerry N. Sisneros, John J. Wootan, Douglas M. Gleichman
  • Patent number: 5463494
    Abstract: An optical filter (18) includes a first layer (22) of material having a bandgap and being doped with an impurity having an energy level in the bandgap such that the first layer absorbs optical energy below a first wavelength and transmits optical energy thereabove. The filter further includes a second layer of optical material (26) disposed on said first layer (22) which transmits optical energy at a second wavelength, above the first wavelength, and reflects optical energy at a third wavelength above the second wavelength. The first and second layers in combination provide a filter (18) with high transmission in-band, low transmission out-of-band and a sharp cutoff therebetween.
    Type: Grant
    Filed: December 23, 1993
    Date of Patent: October 31, 1995
    Assignee: Hughes Aircraft Company
    Inventor: Lowell M. Hobrock
  • Patent number: 5459636
    Abstract: Disclosed are a system and method for determining the pose (translation, rotation, and scale), or position and orientation, of a model object that best matches a target object located in image data. Through an iterative process small adjustments are made to the original position and orientation of the model object until it converges to a state that best matches the target object contained in the image data. Edge data representative of edges of the target object and edge data representative of the model object are processed for each data point in the model object relative to each point in the target object to produce a set of minimum distance vectors between the model object and the target object. A neural network estimates translation, rotation, and scaling adjustments that are to be made to the model object. Pose of the model object is adjusted relative to the target object based upon the estimated translation, rotation, and scaling adjustments provided by the neural network.
    Type: Grant
    Filed: January 14, 1994
    Date of Patent: October 17, 1995
    Assignee: Hughes Aircraft Company
    Inventors: Allen Gee, David M. Doria
  • Patent number: 5386119
    Abstract: The thickness of the entire surface of a thick semiconductor (94) layer on an insulator is determined all at once by dividing the surface into a plurality of pixels, by varying the length of a variable length optical path (110) in a Michelson interferometer (66) having an infrared source (62), illuminating the entire surface of the layer with an image of the IR source during the length variation operation, and by detecting (64) the product of the intensity (I.sub.s (z)) from the Michelson interferometer and the reflectivity R(t) of the layer as the path length is varied, such being indicative of the thickness of the layer, and by determining, for each pixel, which one of a plurality of groups of stored reflectance values, for a corresponding plurality of thicknesses, best matches the detected values, thereby providing a thickness map of the semiconductor layer.
    Type: Grant
    Filed: March 25, 1993
    Date of Patent: January 31, 1995
    Assignee: Hughes Aircraft Company
    Inventor: Anthony Ledger
  • Patent number: 5301130
    Abstract: A system and method for determining the speed of a vehicle independent of angular wheel rotation rates is provided. The system generates time-varying signals corresponding to the vertical acceleration of the front and rear wheels. The front and rear wheel signals include corresponding perturbations caused by the wheels crossing road disturbances such as bumps. A time lag occurs between perturbations in the rear wheel signal and corresponding perturbations in the front wheel signal. An adaptive algorithm correlates the signals for various time delay values until a time delay value is determined which maximizes the correlation between the two signals. The calculated time delay value corresponds to the actual time lag between the front and rear wheels occurring before the rear wheels encounter a road disturbance previously encountered by the front wheels. Thus, the invention provides a determination of the actual speed of the vehicle determined independently from the angular rotation rates of the wheels.
    Type: Grant
    Filed: October 22, 1992
    Date of Patent: April 5, 1994
    Assignee: Hughes Aircraft Company
    Inventors: Jerry M. Alcone, James W. Jeter