Patents by Inventor Randal K. Douglas

Randal K. Douglas 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: 8027413
    Abstract: An observation lock detector block receives I&Q correlations and generates error measurement vectors, each including phase, frequency, code, pseudorange, and covariance residual estimates, and generates validity indicator and confidence indicator vectors, one of which error measurement vectors is an output as a selected error measurement vector with a respective validity indicator and confidence indicator vector, both of which selected vectors are communicated to a navigation solution processor in a ultratightly coupled navigation system for providing improved estimations of a navigation solution, the indicators indicating the usefulness of measurement errors, the prefilter detector block comprising discriminators, sequential filters, observation lock detectors and a measurement selector for selecting measurement vector based on phase, frequency, and code discriminations, the measurement errors being residual estimates that are indicated as valid or invalid for dynamic propagation of the residuals in a na
    Type: Grant
    Filed: July 11, 2007
    Date of Patent: September 27, 2011
    Assignee: The Aerospace Corporation
    Inventors: Walter E. Lillo, Manorama Gollakota, John Lukesh, Randal K. Douglas
  • Patent number: 7944997
    Abstract: An m-code GPS receiver receives m-code GPS communication signals having a multimodal autocorrelation, using an m-code mode identifier unambiguously determining a mode value of one of the m-code modal peaks coherently aligned to a coherent unimodal detected envelope, based on sequential probability estimation in an m-code envelope tracking filter using filter residual estimation or with a coherent m-code and c/a-code tracking filter also based on filter residual estimation, for generating m-code phase errors, for unambiguous and precise m-code code phase tracking in closed feedback loops, for preferred use in navigation systems.
    Type: Grant
    Filed: November 2, 2009
    Date of Patent: May 17, 2011
    Assignee: The Aerospace Corporation
    Inventor: Randal K. Douglas
  • Patent number: 7899109
    Abstract: An m-code GPS receiver receives m-code GPS communication signals having a multimodal autocorrelation, using an m-code mode identifier unambiguously determining a mode value of one of the m-code modal peaks coherently aligned to a coherent unimodal detected envelope, based on sequential probability estimation in an m-code envelope tracking filter using filter residual estimation or with a coherent m-code and c/a-code tracking filter also based on filter residual estimation, for generating m-code phase errors, for unambiguous and precise m-code code phase tracking in closed feedback loops, for preferred use in navigation systems.
    Type: Grant
    Filed: August 8, 2006
    Date of Patent: March 1, 2011
    Assignee: The Aerospace Corporation
    Inventor: Randal K. Douglas
  • Publication number: 20100046589
    Abstract: An m-code GPS receiver receives m-code GPS communication signals having a multimodal autocorrelation, using an m-code mode identifier unambiguously determining a mode value of one of the m-code modal peaks coherently aligned to a coherent unimodal detected envelope, based on sequential probability estimation in an m-code envelope tracking filter using filter residual estimation or with a coherent m-code and c/a-code tracking filter also based on filter residual estimation, for generating m-code phase errors, for unambiguous and precise m-code code phase tracking in closed feedback loops, for preferred use in navigation systems.
    Type: Application
    Filed: November 2, 2009
    Publication date: February 25, 2010
    Applicant: The Aerospace Corporation
    Inventor: Randal K. Douglas
  • Publication number: 20090016414
    Abstract: An observation lock detector block receives I&Q correlations and generates error measurement vectors, each including phase, frequency, code, pseudorange, and covariance residual estimates, and generates validity indicator and confidence indicator vectors, one of which error measurement vectors is an output as a selected error measurement vector with a respective validity indicator and confidence indicator vector, both of which selected vectors are communicated to a navigation solution processor in a ultratightly coupled navigation system for providing improved estimations of a navigation solution, the indicators indicating the usefulness of measurement errors, the prefilter detector block comprising discriminators, sequential filters, observation lock detectors and a measurement selector for selecting measurement vector based on phase, frequency, and code discriminations, the measurement errors being residual estimates that are indicated as valid or invalid for dynamic propagation of the residuals in a na
    Type: Application
    Filed: July 11, 2007
    Publication date: January 15, 2009
    Inventors: Walter E. Lillo, Manorama Gollakota, John Lukesh, Randal K. Douglas
  • Publication number: 20080037614
    Abstract: An m-code GPS receiver receives m-code GPS communication signals having a multimodal autocorrelation, using an m-code mode identifier unambiguously determining a mode value of one of the m-code modal peaks coherently aligned to a coherent unimodal detected envelope, based on sequential probability estimation in an m-code envelope tracking filter using filter residual estimation or with a coherent m-code and c/a-code tracking filter also based on filter residual estimation, for generating m-code phase errors, for unambiguous and precise m-code code phase tracking in closed feedback loops, for preferred use in navigation systems.
    Type: Application
    Filed: August 8, 2006
    Publication date: February 14, 2008
    Inventor: Randal K. Douglas
  • Patent number: 6914931
    Abstract: A GPS receiver receives GPS spread spectrum communication signals subject to carrier demodulation and code phase autocorrelation using tightly coupled Kalman filter residual estimation based on Ricatti matrix computation for generating code phase errors and carrier phase errors for improved code phase tracking and carrier phase tracking in feedback loops for use in navigation systems.
    Type: Grant
    Filed: September 26, 2001
    Date of Patent: July 5, 2005
    Assignee: The Aerospace Corporation
    Inventors: Randal K. Douglas, Anthony S. Abbott
  • Patent number: 6587761
    Abstract: A vehicular position and attitude can be accurately determined from GPS signals by positioning a master and two slave orthogonally disposed receiver antennas rigidly mounted together enabling the rotation of the slave receiver antennas about the master antenna. The slave antennas are rotated and then dither back and forth so that differential phase measurements between the slave antennas and the master antenna is nulled in carrier phase alignment of the GPS signals for determining azimuth angles and elevation angles to the GPS satellites for determining the position and attitude of the vehicle.
    Type: Grant
    Filed: October 23, 2001
    Date of Patent: July 1, 2003
    Assignee: The Aerospace Corporation
    Inventors: Lalit Kumar, Randal K. Douglas
  • Publication number: 20030078705
    Abstract: A vehicular position and attitude can be accurately determined from GPS signals by positioning a master and two slave orthogonally disposed receiver antennas rigidly mounted together enabling the rotation of the slave receiver antennas about the master antenna. The slave antennas are rotated and then dither back and forth so that differential phase measurements between the slave antennas and the master antenna is nulled in carrier phase alignment of the GPS signals for determining azimuth angles and elevation angles to the GPS satellites for determining the position and attitude of the vehicle.
    Type: Application
    Filed: October 23, 2001
    Publication date: April 24, 2003
    Applicant: The Aerospace Corporation
    Inventors: Lalit Kumar, Randal K. Douglas
  • Publication number: 20030058927
    Abstract: A GPS receiver receives GPS spread spectrum communication signals subject to carrier demodulation and code phase autocorrelation using tightly coupled Kalman filter residual estimation based on Ricatti matrix computation for generating code phase errors and carrier phase errors for improved code phase tracking and carrier phase tracking in feedback loops for use in navigation systems.
    Type: Application
    Filed: September 26, 2001
    Publication date: March 27, 2003
    Applicant: The Aerospace Corporation
    Inventors: Randal K. Douglas, Anthony S. Abbott