Patents by Inventor Stephen Kubik

Stephen Kubik 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: 20150291277
    Abstract: A system and method for controlling a deceleration profile of an aircraft, includes a processor and memory that receives a signal indicative of a deceleration command; receives signals indicative of a sensed velocity and a commanded heading rate; determines a commanded velocity in response to the receiving of the deceleration command and the commanded heading rate; determines an estimated deceleration command as a function of the commanded velocity; and determines an actual deceleration command in response to the determining of the estimated deceleration command.
    Type: Application
    Filed: April 11, 2014
    Publication date: October 15, 2015
    Applicant: Sikorsky Aircraft Corporation
    Inventors: Stephen Kubik, Alex Faynberg, Stephen C. Mcculley, John P. Rucci, Christiaan P. Corry, Edward Pavelka
  • Patent number: 9139290
    Abstract: Embodiments are directed to receiving, by a computing device comprising a processor, at least one control input associated with an aircraft, obtaining, by the computing device, a predicted response to the at least one control input by filtering on a trim position, wherein the predicted response is based on a model of the aircraft, obtaining, by the computing device, an actual response of the aircraft to the at least one control input, comparing, by the computing device, the predicted response and the actual response, and determining, by the computing device, at least one attribute based on the comparison.
    Type: Grant
    Filed: September 10, 2013
    Date of Patent: September 22, 2015
    Assignee: SIKORSKY AIRCRAFT CORPORATION
    Inventors: Anthony Litwinowicz, Stephen Kubik, Steven W. Hong
  • Publication number: 20150073626
    Abstract: Embodiments are directed to receiving, by a computing device comprising a processor, at least one control input associated with an aircraft, obtaining, by the computing device, a predicted response to the at least one control input by filtering on a trim position, wherein the predicted response is based on a model of the aircraft, obtaining, by the computing device, an actual response of the aircraft to the at least one control input, comparing, by the computing device, the predicted response and the actual response, and determining, by the computing device, at least one attribute based on the comparison
    Type: Application
    Filed: September 10, 2013
    Publication date: March 12, 2015
    Applicant: Sikorsky Aircraft Corporation
    Inventors: Anthony Litwinowicz, Stephen Kubik, Steven W. Hong
  • Patent number: 8676405
    Abstract: A method of controlling the flight of a rotorcraft in a feed-forward/feedback architecture includes utilizing an aircraft plant model to control the rotorcraft performance; determining when an external load is coupled to the rotorcraft; and modifying an inverse plant when the external load is present.
    Type: Grant
    Filed: January 20, 2011
    Date of Patent: March 18, 2014
    Assignee: Sikorsky Aircraft Corporation
    Inventors: Stephen Kubik, Vineet Sahasrabudhe, Alex Faynberg
  • Publication number: 20120136512
    Abstract: A method of controlling the flight of a rotorcraft in a feed-forward/feedback architecture includes utilizing an aircraft plant model to control the rotorcraft performance; determining when an external load is coupled to the rotorcraft; and modifying an inverse plant when the external load is present.
    Type: Application
    Filed: January 20, 2011
    Publication date: May 31, 2012
    Applicant: SIKORSKY AIRCRAFT CORPORATION
    Inventors: Stephen Kubik, Vineet Sahasrabudhe, Alex Faynberg