Patents by Inventor Charles Hewgley

Charles Hewgley 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: 8483891
    Abstract: A method is described performing the following with a parafoil's control unit composed of electronic circuitry while the control unit is being transported with a parafoil: calculating a desired landing location for a parafoil, the desired landing location corresponding to a moving target, the calculating including using a term representative of the moving target's velocity; determining a flight path to the desired landing location; and, controlling the parafoil's flight path so as to follow the flight path.
    Type: Grant
    Filed: April 8, 2011
    Date of Patent: July 9, 2013
    Assignee: The United States of America as represented by the Secretary of the Navy
    Inventors: Oleg Yakimenko, Charles Hewgley, Eugene Bourakov
  • Patent number: 8437891
    Abstract: A method is described that involves determining a higher altitude wind. The method further includes determining a wind model with the higher altitude wind. The wind model includes a linear or logarithmic increase in wind magnitude with increasing altitude beneath the higher altitude. The method further includes determining locations of a flight path for a parafoil based on calculations that use the wind model. The calculations are performed by an electronic control unit that is transported by the parafoil. The method also includes controlling the parafoil's flight path consistently with the determined locations. The controlling is performed by the control unit.
    Type: Grant
    Filed: April 8, 2011
    Date of Patent: May 7, 2013
    Assignee: The United States of America as represented by the Secretary of the Navy
    Inventors: Oleg Yakimenko, Eugene Bourakov, Charles Hewgley
  • Publication number: 20130013131
    Abstract: A method is described that involves determining a higher altitude wind. The method further includes determining a wind model with the higher altitude wind. The wind model includes a linear or logarithmic increase in wind magnitude with increasing altitude beneath the higher altitude. The method further includes determining locations of a flight path for a parafoil based on calculations that use the wind model. The calculations are performed by an electronic control unit that is transported by the parafoil. The method also includes controlling the parafoil's flight path consistently with the determined locations. The controlling is performed by the control unit.
    Type: Application
    Filed: April 8, 2011
    Publication date: January 10, 2013
    Inventors: Oleg YAKIMENKO, Eugene Bourakov, Charles Hewgley
  • Publication number: 20130013135
    Abstract: A method is described performing the following with a parafoil's control unit composed of electronic circuitry while the control unit is being transported with a parafoil: calculating a desired landing location for a parafoil, the desired landing location corresponding to a moving target, the calculating including using a term representative of the moving target's velocity; determining a flight path to the desired landing location; and, controlling the parafoil's flight path so as to follow the flight path.
    Type: Application
    Filed: April 8, 2011
    Publication date: January 10, 2013
    Inventors: Oleg YAKIMENKO, Charles Hewgley, Eugene Bourakov