Patents by Inventor Matthew Chrobak

Matthew Chrobak 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: 11859956
    Abstract: A guided projectile including a precision guidance munition assembly utilizes at least one maneuver envelope to optimally control movement of at least one canard to steer the guided projectile during flight. The maneuver envelopes optimize movements of the at least one canard that effectuate movement in either the range direction or the cross-range direction, or both. The maneuver envelope enables optimal timing such that maneuvering in one direction does not come at the expense of maneuver authority in the other direction.
    Type: Grant
    Filed: August 30, 2019
    Date of Patent: January 2, 2024
    Assignee: BAE Systems Information and Electronic Systems Integration Inc.
    Inventors: Paul Zemany, Matthew Chrobak
  • Patent number: 11555680
    Abstract: A guided projectile including a precision guidance munition assembly utilizes at least one maneuver envelope to optimally control movement of at least one canard to steer the guided projectile during flight. The maneuver envelopes optimize movements of the at least one canard that effectuate movement in either the range direction or the cross-range direction, or both. The maneuver envelope enables optimal timing such that maneuvering in one direction does not come at the expense of maneuver authority in the other direction.
    Type: Grant
    Filed: August 30, 2019
    Date of Patent: January 17, 2023
    Assignee: BAE Systems Information and Electronic Systems Integration Inc.
    Inventors: Paul Zemany, Matthew Chrobak, Egor V. Degtiarev
  • Publication number: 20210231425
    Abstract: A guided projectile including a precision guidance munition assembly utilizes at least one maneuver envelope to optimally control movement of at least one canard to steer the guided projectile during flight. The maneuver envelopes optimize movements of the at least one canard that effectuate movement in either the range direction or the cross-range direction, or both. The maneuver envelope enables optimal timing such that maneuvering in one direction does not come at the expense of maneuver authority in the other direction.
    Type: Application
    Filed: August 30, 2019
    Publication date: July 29, 2021
    Applicant: BAE Systems Information and Electronic Systems Integration Inc.
    Inventors: Paul Zemany, Matthew Chrobak, Egor V. Degtiarev
  • Publication number: 20210231424
    Abstract: A guided projectile including a precision guidance munition assembly utilizes at least one maneuver envelope to optimally control movement of at least one canard to steer the guided projectile during flight. The maneuver envelopes optimize movements of the at least one canard that effectuate movement in either the range direction or the cross-range direction, or both. The maneuver envelope enables optimal timing such that maneuvering in one direction does not come at the expense of maneuver authority in the other direction.
    Type: Application
    Filed: August 30, 2019
    Publication date: July 29, 2021
    Applicant: BAE Systems Information and Electronic Systems Integration Inc.
    Inventors: Paul Zemany, Matthew Chrobak