Patents by Inventor Oleg Yakimenko

Oleg Yakimenko 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: 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: 20130009013
    Abstract: A method is described that includes performing a), b) and c) below with an electronic control unit of a parafoil: a) after being dropped from an airborne vehicle, wirelessly receiving the parafoil's desired landing location; b) determining a flight path for the parafoil that lands at the desired landing location; and, c) controlling the parafoil's flight path consistently with the determined flight path.
    Type: Application
    Filed: April 8, 2011
    Publication date: January 10, 2013
    Inventors: Eugene BOURAKOV, Oleg Yakimenko
  • Publication number: 20130013132
    Abstract: A method is described that involves performing the following with a parafoil's control unit composed of electronic circuitry while the control unit is being transported with a parafoil: determining a desired exit of a turn; determining a desired time for the turn; determining the parafoil's actual entrance for the turn; determining an arc between the actual entrance and the desired exit; and, incorporating said arc as said parafoil's planned flight trajectory through said turn.
    Type: Application
    Filed: April 8, 2011
    Publication date: January 10, 2013
    Inventor: Oleg YAKIMENKO
  • Publication number: 20130009014
    Abstract: A method is described that involves establishing a wireless network between a wireless access node of an existing network and a remote location by wirelessly linking a plurality of electronic processing circuits each transported by a respective parafoil. The wirelessly linked processing circuits are to route packets from the wireless access node to the remote location.
    Type: Application
    Filed: April 8, 2011
    Publication date: January 10, 2013
    Inventors: Alex BORDETSKY, Oleg Yakimenko, Eugene Bourakov
  • 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