Patents by Inventor Sally Ann Keyes

Sally Ann Keyes 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: 11790793
    Abstract: Systems and methods for model based vehicle navigation are provided. In one embodiment, a navigation system: a strapdown navigation processor; a propagator-estimator filter, the navigation processor configured to input inertial sensor data and navigation corrections from the filter to generate a navigation solution comprising a vehicle velocity estimate and a vehicle attitude estimate; a vehicle physics model configured to perform calculations utilizing dynamics equations for a rigid body. The model inputs 1) vehicle state estimates from the navigation solution and 2) platform inputs indicative of forces acting on a vehicle platform. The model outputs a set of three orthogonal predicted translational acceleration measurements based on the inputs.
    Type: Grant
    Filed: January 8, 2021
    Date of Patent: October 17, 2023
    Assignee: Honeywell International Inc.
    Inventors: Sally Ann Keyes, Dean Richard Wilkens, Dale F Enns
  • Patent number: 11781836
    Abstract: Model based inertial navigation for a spinning projectile is provided.
    Type: Grant
    Filed: March 4, 2021
    Date of Patent: October 10, 2023
    Assignee: Honeywell International Inc.
    Inventors: Sally Ann Keyes, Calvin Samborski, Dean Richard Wilkens, Dale F. Enns
  • Publication number: 20220282955
    Abstract: Model based inertial navigation for a spinning projectile is provided.
    Type: Application
    Filed: March 4, 2021
    Publication date: September 8, 2022
    Applicant: Honeywell International Inc.
    Inventors: Sally Ann Keyes, Calvin Samborski, Dean Richard Wilkens, Dale F. Enns
  • Publication number: 20220223054
    Abstract: Systems and methods for model based vehicle navigation are provided. In one embodiment, a navigation system: a strapdown navigation processor; a propagator-estimator filter, the navigation processor configured to input inertial sensor data and navigation corrections from the filter to generate a navigation solution comprising a vehicle velocity estimate and a vehicle attitude estimate; a vehicle physics model configured to perform calculations utilizing dynamics equations for a rigid body. The model inputs 1) vehicle state estimates from the navigation solution and 2) platform inputs indicative of forces acting on a vehicle platform. The model outputs a set of three orthogonal predicted translational acceleration measurements based on the inputs.
    Type: Application
    Filed: January 8, 2021
    Publication date: July 14, 2022
    Applicant: Honeywell International Inc.
    Inventors: Sally Ann Keyes, Dean Richard Wilkens, Dale F. Enns
  • Patent number: 11268813
    Abstract: A system implementing a method for generating a navigation output is provided. The method includes determining a gravitational anomaly estimate based at least in part on inertial sensor data and navigation output; generating navigation and sensor corrections that are due at least in part on inherent sensor errors that include vertical accelerometer/gravimeter corrections from at least a navigation output estimate, the gravitational anomaly estimate, and the gravity map data; and generating the navigation output based on the inertial sensor data, gravity map data and the navigation and sensor corrections.
    Type: Grant
    Filed: April 10, 2020
    Date of Patent: March 8, 2022
    Assignee: Honeywell International Inc.
    Inventor: Sally Ann Keyes
  • Publication number: 20210215484
    Abstract: A system implementing a method for generating a navigation output is provided. The method includes determining a gravitational anomaly estimate based at least in part on inertial sensor data and navigation output; generating navigation and sensor corrections that are due at least in part on inherent sensor errors that include vertical accelerometer/gravimeter corrections from at least a navigation output estimate, the gravitational anomaly estimate, and the gravity map data; and generating the navigation output based on the inertial sensor data, gravity map data and the navigation and sensor corrections.
    Type: Application
    Filed: April 10, 2020
    Publication date: July 15, 2021
    Applicant: Honeywell International Inc.
    Inventor: Sally Ann Keyes