Patents by Inventor Rebecca A. Bird

Rebecca A. Bird 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).

  • Publication number: 20160213317
    Abstract: A system, associated method, and computer readable medium for monitoring one or more test subjects. The system is comprised of a subject wearable interface which features at least one sensor to read data from the test subject. A processor module receives data from the sensor(s) on the subject wearable interface. The system includes an output module and a wireless transceiver module that receive data from the processor module, any of which may or may not be located on the subject wearable interface. The system allows for the subject to be monitored while wearing the subject wearable interface without being tethered to any sensing device or data acquisition device that would be wired and restrain the subject from normal movement. The system allows a researcher or user (or device) to record data on a test subject while the test subject is allowed to freely move and engage in normal activity.
    Type: Application
    Filed: September 30, 2014
    Publication date: July 28, 2016
    Inventors: Neal T. RICHARDSON, Aaron O. OLOWIN, Rebecca A. BIRD, Patricia L. FOLEY, Eugene B. PARKER, JR.
  • Patent number: 6208914
    Abstract: A system for adaptive and reconfigurable control of aircraft and other complex objects and processes, herein referred to collectively as controlled “plants.” A modified form of sequential least-squares estimation is used to obtain near-real-time estimates of the values of plant parameters. The parameter estimates are used in a novel piecewise-linear optimal receding-horizon sampled-data controller in which internal controller parameters, known in the art as Riccati gains, are propagated from their current values using the most recent plant parameter estimates. This method of updating Riccati gains is a major departure from the prior art in receding-horizon control, where the Riccati gains (or equivalent) are re-initialized at each control update using terminal boundary conditions. The present invention provides improved robustness of control, lessened need for re-tuning control-effort penalties when operating conditions change, and significantly reduced computational burden.
    Type: Grant
    Filed: November 19, 1997
    Date of Patent: March 27, 2001
    Assignee: Barron Associates, Inc.
    Inventors: David G. Ward, Jeffrey F. Monaco, Roger L. Barron, Rebecca A. Bird
  • Patent number: 5107424
    Abstract: A ship steering system has a multiplicity of selectable steering stations. A continuously rotating helm at each steering station generates digital rudder control signals which cause a predetermined rudder movement for each 360.degree. of helm rotation. Steering stations are selected through a multiplexer controlled at a command steering station. The steering system is operable from the command steering station in a plurality of modes, which includes auto-pilot, helm (full-follow-up), and tiller (non-follow-up). Helm and/or tiller modes of operation are available at steering stations remote from the command steering station. The system provides for an emergency takeover from the helm or autopilot modes by automatically establishing the tiller mode when the tiller stick is moved. When in the autopilot mode an alarm system provides an alert should the course deviate from a selected course tolerance.
    Type: Grant
    Filed: March 5, 1990
    Date of Patent: April 21, 1992
    Assignee: Sperry Marine Inc.
    Inventors: Rebecca A. Bird, David A. Bennett, Albert L. Coleman, Jeffrey C. Johnson, Ronald K. Richey, Gregory Schluge, Steven E. Schubert, Eldon J. Thompson, John F. Yancey, Jr.
  • Patent number: 5034895
    Abstract: The rudder order bias integrator of a marine autopilot is reactivated upon substantial completion of a turning maneuver in response to heading error, heading rate and the derivative portion of the rudder order signal. Upon reactivation, the integrator time constant is ramped from a predetermined small value to the normal large time constant of the integrator.
    Type: Grant
    Filed: January 3, 1990
    Date of Patent: July 23, 1991
    Assignee: Sperry Marine Inc.
    Inventors: Jeffrey C. Johnson, Rebecca A. Bird, David A. Bennett
  • Patent number: 4924233
    Abstract: A sensor input/output system in a main radar system maintains continuous power to the compass interface when the main radar system is shut down. A single level of interrupt handlers is utilized without interrupt nesting or control by task executive software. The sensor input/output system is functionally partitioned such that all of the service required by an interrupt is continuously provided until the service is completed. A digital processor for providing the interrupt servicing and control and PROM firmware for storing the interrupt handlers also have backup power continuously applied. Since the processor compass interrupt handler and compass interface are continuously powered, heading synchronization is maintained by the main radar system during power down conditions.
    Type: Grant
    Filed: September 2, 1988
    Date of Patent: May 8, 1990
    Assignee: Sperry Marine Inc.
    Inventor: Rebecca A. Bird