Patents by Inventor Patrick A. Nelson

Patrick A. Nelson 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: 8716606
    Abstract: A conformal electro-magnetic (EM) shield and a method of applying such a shield are provided herein as well as variations thereof. Variations include, but are not limited to, frequency-selective shielding, shields containing active and/or passive electronic components, and strippable shields that can easily be applied to and removed from underlying components. Variations of a shield structure include at least an insulating layer between the underling component and the shield, and shielding and/or capping layers disposed over the insulating layer.
    Type: Grant
    Filed: October 14, 2010
    Date of Patent: May 6, 2014
    Assignee: Lockheed Martin Corporation
    Inventors: Matthew Kelley, Christian Adams, Patrick A. Nelson
  • Publication number: 20130257473
    Abstract: A long-life embedded structure sensor, remote long-life fluid measurement and analysis system, long-life off-grid enclosed space proximity change detector, surface-mount encryption device with volatile long-life key storage and volume intrusion response, and a portable encrypted data storage with volatile long-life key storage and volume intrusion response are provided to be powered by and equipped with a long-life power source that can provide operative power for at least a twenty year duration.
    Type: Application
    Filed: July 16, 2009
    Publication date: October 3, 2013
    Applicant: Lockheed Martin Corporation
    Inventors: Christian Adams, Joseph M. Wright, Patrick A. Nelson, Kenneth S. Gurley, Richard A. Vaughn
  • Patent number: 8499172
    Abstract: A system and method of recovering encoded information contained in a device by storing and retrieving at least part of the necessary decoding data by setting and measuring the physical characteristics of the device. Storage and recovery options include, but are not limited to, measurement of electronic or optical characteristics of electrically or optically conductive portions of the device using a range of measurement techniques that include, but are not limited to, time-domain reflectometry.
    Type: Grant
    Filed: April 12, 2012
    Date of Patent: July 30, 2013
    Assignee: Lockheed Martin Corp.
    Inventors: Patrick A. Nelson, Christian Adams
  • Publication number: 20120198244
    Abstract: A system and method of recovering encoded information contained in a device by storing and retrieving at least part of the necessary decoding data by setting and measuring the physical characteristics of the device. Storage and recovery options include, but are not limited to, measurement of electronic or optical characteristics of electrically or optically conductive portions of the device using a range of measurement techniques that include, but are not limited to, time-domain reflectometry.
    Type: Application
    Filed: April 12, 2012
    Publication date: August 2, 2012
    Applicant: LOCKHEED MARTIN MISSILES AND FIRE CONTROL
    Inventors: Patrick A. NELSON, Christian Adams
  • Patent number: 8127151
    Abstract: A system and method of recovering encoded information contained in a device by storing and retrieving at least part of the necessary decoding data by setting and measuring the physical characteristics of the device. Storage and recovery options include, but are not limited to, measurement of electronic or optical characteristics of electrically or optically conductive portions of the device using a range of measurement techniques that include, but are not limited to, time-domain reflectometry.
    Type: Grant
    Filed: October 13, 2009
    Date of Patent: February 28, 2012
    Assignee: Lockheed Martin Corporation
    Inventors: Patrick A. Nelson, Christian Adams
  • Patent number: 8119958
    Abstract: A matrix of explosive cells can include plural explosive cells formed in an array in a common substrate. Each cell can be formed as a recess filled with explosive material. An ignition device has an addressable ignition source for each cell. This matrix can be used in combination with a projectile guidance system. The projectile guidance system includes an antenna, a transceiver and a control processor. A method of guiding a projectile can include firing a projectile at a target, tracking the projectile and the target, determining a desired change in a flight path of the projectile, transmitting guidance commands to effect the desired change in the projectile's flight path to the projectile, receiving the guidance commands onboard the projectile and selectively igniting an explosive cell in a matrix of addressable explosive cells contained in a common substrate using the guidance commands.
    Type: Grant
    Filed: February 19, 2009
    Date of Patent: February 21, 2012
    Assignee: Lockheed Martin Corporation
    Inventors: Christian Adams, Kenneth S. Gurley, Tara Y. Rohter, Patrick A. Nelson
  • Publication number: 20120012690
    Abstract: A matrix of explosive cells can include plural explosive cells formed in an array in a common substrate. Each cell can be formed as a recess filled with explosive material. An ignition device has an addressable ignition source for each cell. This matrix can be used in combination with a projectile guidance system. The projectile guidance system includes an antenna, a transceiver and a control processor. A method of guiding a projectile can include firing a projectile at a target, tracking the projectile and the target, determining a desired change in a flight path of the projectile, transmitting guidance commands to effect the desired change in the projectile's flight path to the projectile, receiving the guidance commands onboard the projectile and selectively igniting an explosive cell in a matrix of addressable explosive cells contained in a common substrate using the guidance commands.
    Type: Application
    Filed: February 19, 2009
    Publication date: January 19, 2012
    Applicant: LOCKHEED MARTIN CORPORATION
    Inventors: Christian Adams, Kenneth S. Gurley, Tara Y. Rohter, Patrick A. Nelson
  • Publication number: 20110120764
    Abstract: A conformal electro-magnetic (EM) shield and a method of applying such a shield are provided herein as well as variations thereof. Variations include, but are not limited to, frequency-selective shielding, shields containing active and/or passive electronic components, and strippable shields that can easily be applied to and removed from underlying components. Variations of a shield structure include at least an insulating layer between the underling component and the shield, and shielding and/or capping layers disposed over the insulating layer.
    Type: Application
    Filed: October 14, 2010
    Publication date: May 26, 2011
    Applicant: Lockheed Martin Corporation
    Inventors: Matthew Kelley, Christian Adams, Patrick A. Nelson
  • Publication number: 20110087897
    Abstract: A system and method of recovering encoded information contained in a device by storing and retrieving at least part of the necessary decoding data by setting and measuring the physical characteristics of the device. Storage and recovery options include, but are not limited to, measurement of electronic or optical characteristics of electrically or optically conductive portions of the device using a range of measurement techniques that include, but are not limited to, time-domain reflectometry.
    Type: Application
    Filed: October 13, 2009
    Publication date: April 14, 2011
    Inventors: Patrick A. NELSON, Christian ADAMS
  • Patent number: 7437222
    Abstract: Various embodiments of the present invention are directed to precision control system for spacecraft gimbaled payloads. Embodiments of the invention provide an innovative technique of calibrating gimbals disturbances to directly canceling gimbal control disturbances. Such a calibration system includes a receiver for receiving telemetry data for pointing a payload, a processor for calculating a disturbance parameter vector for a gimbal disturbance model with the telemetry data and a transmitter for transmitting the disturbance parameter vector to compensate for pointing error when applied in pointing the payload. The gimbal disturbance model comprises a harness stiffness term, a disturbance harmonics term and at least one friction hysteresis term. The telemetry data may be time matched prior to calculating the disturbance parameter vector.
    Type: Grant
    Filed: July 28, 2005
    Date of Patent: October 14, 2008
    Assignee: The Boeing Company
    Inventors: Ketao Liu, Justin Burch, Gregory S. Becker, Patrick A. Nelson