Patents by Inventor Brian D. Cordill

Brian D. Cordill 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: 11637368
    Abstract: Systems and methods are provided for phased array passband calibration, which permits repeated calibration of the antenna system in the field without a moving far field sensor. An implementation includes an equalization filter coupled to a phased array feed; a calibration probe disposed to couple with an antenna array to transfer radio frequency (RF) energy; a database of probe-to-far-field (FF) transforms having a probe-to-FF transform for each of a plurality of incidence angles; a calibration component operable to: receive calibration probe measurements for a plurality of frequencies; and determine a calculated phased array passband response for at least a first incidence angle, based at least on the calibration probe measurements and a probe-to-FF transform for the first incidence angle; and a filter generation component operable to generate a tuning configuration for the equalization filter, based at least on the calculated phased array passband response.
    Type: Grant
    Filed: July 18, 2019
    Date of Patent: April 25, 2023
    Assignee: The Boeing Company
    Inventors: Brian D. Cordill, Bader Akbik, Ron Y. Lee, Jeffrey J. Calvagna, Nikolay A. Angelov
  • Patent number: 11067666
    Abstract: A method for self-calibrating a radar system includes forming a calibration loop-back signal path. The calibration loop-back signal path is configured for determining a passband response of each of a radio frequency (RF) signal path, a local oscillator (LO) signal path, and an intermediate frequency (IF) signal path of the radar system. The method also includes transmitting a set of calibration signals into the RF signal path and the LO signal path and measuring output signals from the IF signal path in a receiver of the radar system. The method further includes determining the passband response of each of the RF signal path, the LO signal path and the IF signal path from the measured output signals and compensating for distortions and/or non-linearities in the signal paths using the passband response of each signal path.
    Type: Grant
    Filed: May 29, 2018
    Date of Patent: July 20, 2021
    Assignee: The Boeing Company
    Inventors: Brian D. Cordill, James Douglas Franklin
  • Publication number: 20210021029
    Abstract: Systems and methods are provided for phased array passband calibration, which permits repeated calibration of the antenna system in the field without a moving far field sensor. An implementation includes an equalization filter coupled to a phased array feed; a calibration probe disposed to couple with an antenna array to transfer radio frequency (RF) energy; a database of probe-to-far-field (FF) transforms having a probe-to-FF transform for each of a plurality of incidence angles; a calibration component operable to: receive calibration probe measurements for a plurality of frequencies; and determine a calculated phased array passband response for at least a first incidence angle, based at least on the calibration probe measurements and a probe-to-FF transform for the first incidence angle; and a filter generation component operable to generate a tuning configuration for the equalization filter, based at least on the calculated phased array passband response.
    Type: Application
    Filed: July 18, 2019
    Publication date: January 21, 2021
    Inventors: Brian D. Cordill, Bader Akbik, Ron Y. Lee, Jeffrey J. Calvagna, Nikolay A. Angelov
  • Publication number: 20190369210
    Abstract: A method for self-calibrating a radar system includes forming a calibration loop-back signal path. The calibration loop-back signal path is configured for determining a passband response of each of a radio frequency (RF) signal path, a local oscillator (LO) signal path, and an intermediate frequency (IF) signal path of the radar system. The method also includes transmitting a set of calibration signals into the RF signal path and the LO signal path and measuring output signals from the IF signal path in a receiver of the radar system. The method further includes determining the passband response of each of the RF signal path, the LO signal path and the IF signal path from the measured output signals and compensating for distortions and/or non-linearities in the signal paths using the passband response of each signal path.
    Type: Application
    Filed: May 29, 2018
    Publication date: December 5, 2019
    Inventors: Brian D. Cordill, James Douglas Franklin
  • Patent number: 10313220
    Abstract: A signal receiver includes receive circuitry. The signal receiver further includes a processor coupled to the receive circuitry and configured to receive, from a filter, a stream of samples including a first set of samples. A data rate of an input of the filter may correspond to a data rate of an output of the filter. The first set of samples includes multiple samples. The processor is further configured to perform a detection operation on the first set of samples. The processor is further configured to detect a signal emitter based on the detection operation.
    Type: Grant
    Filed: July 18, 2016
    Date of Patent: June 4, 2019
    Assignee: THE BOEING COMPANY
    Inventors: Peter S. Wittenberg, Brian D. Cordill
  • Publication number: 20180017665
    Abstract: A signal receiver includes receive circuitry. The signal receiver further includes a processor coupled to the receive circuitry and configured to receive, from a filter, a stream of samples including a first set of samples. A data rate of an input of the filter may correspond to a data rate of an output of the filter. The first set of samples includes multiple samples. The processor is further configured to perform a detection operation on the first set of samples. The processor is further configured to detect a signal emitter based on the detection operation.
    Type: Application
    Filed: July 18, 2016
    Publication date: January 18, 2018
    Applicant: THE BOEING COMPANY
    Inventors: Peter S. Wittenberg, Brian D. Cordill