Patents by Inventor Anthony S. Abbott

Anthony S. Abbott 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: 7555033
    Abstract: An M code envelope detector receives an incoming binary offset carrier (BOC) signal, such as the M code signal, and generates inphase BOC and quadraphase BOC signals, separated by an offset, that have respective ambiguous correlation envelopes, that when combined, provide a near unimodal correlation function with respect to code phase error of the BOC signal having an inherent multimodal autocorrelation function, with the near unimodal correlation envelope being tracked by early and late code replicas at broad one chip phases for providing unambiguous but nonlinear code phase error tracking, which detector is then further improved with the use of code replicas having narrow partial chip phases, such as ? chip phases, for providing near linear code phase error tracking for unambiguous and accurate code tracking of the BOC signal.
    Type: Grant
    Filed: June 22, 2004
    Date of Patent: June 30, 2009
    Assignee: The Aerospace Corporation
    Inventors: Walter E. Lillo, Phllip W. Ward, Anthony S. Abbott
  • 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
  • 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
  • Patent number: 6516021
    Abstract: An ultratight coupling method generates navigation error state information from an integration Kalman filter for updating the navigation solution based upon inertial measurement data and computes pseudorange and pseudorange rate data from the navigation solution and from ephemeris data, to generate the prompt, early and late replica signals that drive the signal correlators having quadrature outputs samples by a federation of Kalman prefilters providing errors residuals to the integration Kalman filter in a closed coupled tracking loop. The coupled tracking loops offer improved tracking of the received signal based upon updated navigation solution.
    Type: Grant
    Filed: September 14, 1999
    Date of Patent: February 4, 2003
    Assignee: The Aerospace Corporation
    Inventors: Anthony S. Abbott, Walter E. Lillo