Patents by Inventor Russell G. Torti

Russell G. Torti has filed for patents to protect the following inventions. This listing includes patent applications that are pending as well as patents that have already been granted by the United States Patent and Trademark Office (USPTO).

  • Patent number: 9115996
    Abstract: A method and system for managing an aircraft's flight path by identifying and categorizing potential threats in the aircraft's original flight path and determining an alternate flight path. The alternate flight path is selected from potential flight paths and has a threat value lower than any of the potential flight paths. The potential flight path candidates are generated from combinations of the original flight path coordinates, and coordinates that vary from the original coordinates by a set range.
    Type: Grant
    Filed: July 29, 2009
    Date of Patent: August 25, 2015
    Assignee: Lockheed Martin Corporation
    Inventors: Uday N. Desai, John M. Williams, Russell G. Torti
  • Publication number: 20110029234
    Abstract: A method and system for managing an aircraft's flight path by identifying and categorizing potential threats in the aircraft's original flight path and determining an alternate flight path. The alternate flight path is selected from potential flight paths and has a threat value lower than any of the potential flight paths. The potential flight path candidates are generated from combinations of the original flight path coordinates, and coordinates that vary from the original coordinates by a set range.
    Type: Application
    Filed: July 29, 2009
    Publication date: February 3, 2011
    Applicant: Lockheed Martin Corporation
    Inventors: Uday N. Desai, John M. Williams, Russell G. Torti
  • Patent number: 7290710
    Abstract: A system passively identifies objects at large distances with an integrated two-dimensional pattern, spectral tailoring, and an imaging system. Encoded information allows objects of various origin and configuration to be easily and rapidly identified by optical means, but is invisible to the naked eye. The devices used for detecting the objects may be ground-based, airborne, or even satellite-based, and can track engagements of such marked objects in real-time. A tailored reflective surface at a specific wavelength band is applied to the exteriors of the objects to form a unique signature. A scanning system passively records the light emanating from the signature in the specific band, and recognizes the signature to discern what the object is based on a database of information.
    Type: Grant
    Filed: August 21, 2003
    Date of Patent: November 6, 2007
    Assignee: Lockheed Martin Corporation
    Inventors: William J. Betush, James R. Reed, Russell G. Torti
  • Patent number: 6781697
    Abstract: A method is provided for determining one or more reflectance properties of a surface using a portable apparatus that includes reflecting a first beam of electromagnetic energy off of a measured surface, the first beam contacting the measured surface at an angle that is near normal to the measured surface. The method also includes reflecting a second beam of electromagnetic energy off of the measured surface, the second beam contacting the measured surface at an angle that is near grazing to the measured surface. Reflected portions of the first and second beams of electromagnetic energy are then collected and at least one reflectance characteristic value associated with the measured surface is determined based on the reflected portions of the first and second beams of electromagnetic energy.
    Type: Grant
    Filed: January 16, 2002
    Date of Patent: August 24, 2004
    Assignee: Lockheed Martin Corporation
    Inventors: William M. Carra, Russell G. Torti
  • Publication number: 20030184564
    Abstract: A method for simulating a celestial sphere in real-time within a data processing system is disclosed. Initially, information of an observer, such as date, time and longitude/latitude positions, are obtained. Then, a Julian Day and a Greenwich mean sidereal time are determined from the above-mentioned information. A local mean sidereal time is subsequently determined. Furthermore, a tilt angle about a celestial equator of a celestial sphere is determined by using the latitudinal position of the observer. The determined values provide a real-time representation of the position of the celestial sphere relative to the observer at a specific position on the earth.
    Type: Application
    Filed: April 1, 2002
    Publication date: October 2, 2003
    Applicant: Lockheed Martin Corporation
    Inventors: Russell G. Torti, Stephen M. Guest
  • Patent number: D315423
    Type: Grant
    Filed: February 27, 1989
    Date of Patent: March 12, 1991
    Assignee: Fresnel Technologies, Inc.
    Inventors: Richard N. Claytor, Russell G. Torti
  • Patent number: D315425
    Type: Grant
    Filed: February 27, 1989
    Date of Patent: March 12, 1991
    Assignee: Fresnel Technologies, Inc.
    Inventors: Richard N. Claytor, Russell G. Torti
  • Patent number: D315805
    Type: Grant
    Filed: February 27, 1989
    Date of Patent: March 26, 1991
    Assignee: Fresnel Technologies, Inc.
    Inventors: Richard N. Claytor, Russell G. Torti
  • Patent number: D315806
    Type: Grant
    Filed: February 27, 1989
    Date of Patent: March 26, 1991
    Assignee: Fresnel Technologies, Inc.
    Inventors: Richard N. Claytor, Russell G. Torti
  • Patent number: D315807
    Type: Grant
    Filed: February 27, 1989
    Date of Patent: March 26, 1991
    Assignee: Fresnel Technologies, Inc.
    Inventors: Richard N. Claytor, Russell G. Torti
  • Patent number: D315808
    Type: Grant
    Filed: February 27, 1989
    Date of Patent: March 26, 1991
    Assignee: Fresnel Technologies, Inc.
    Inventors: Richard N. Claytor, Russell G. Torti
  • Patent number: D315966
    Type: Grant
    Filed: November 7, 1988
    Date of Patent: April 2, 1991
    Assignee: Fresnel Technologies, Inc.
    Inventors: Richard N. Claytor, Russell G. Torti