Patents by Inventor Stephen C. Mcculley

Stephen C. Mcculley 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: 10351225
    Abstract: A method for position hold override control of an aircraft includes determining, by a processor, that a position hold mode is enabled to hold the aircraft at a substantially fixed position with respect to a target. The processor receives a control input indicative of a commanded change in acceleration of the aircraft as an override of the position hold mode. The processor determines an acceleration command based on the commanded change in acceleration. The acceleration command is adjusted as an adjusted acceleration command responsive to a non-linear scheduled translational rate command based on feedback of a commanded velocity of the aircraft. An update to the commanded velocity of the aircraft is generated based on the adjusted acceleration command.
    Type: Grant
    Filed: March 4, 2016
    Date of Patent: July 16, 2019
    Assignee: SIKORSKY AIRCRAFT CORPORATION
    Inventors: Steven E. Spoldi, Alex Faynberg, Stephen Kubik, Donald T. Ream, John Rucci, Stephen C. McCulley, Christiaan Corry
  • Publication number: 20180141642
    Abstract: A method for position hold override control of an aircraft includes determining, by a processor, that a position hold mode is enabled to hold the aircraft at a substantially fixed position with respect to a target. The processor receives a control input indicative of a commanded change in acceleration of the aircraft as an override of the position hold mode. The processor determines an acceleration command based on the commanded change in acceleration. The acceleration command is adjusted as an adjusted acceleration command responsive to a non-linear scheduled translational rate command based on feedback of a commanded velocity of the aircraft. An update to the commanded velocity of the aircraft is generated based on the adjusted acceleration command.
    Type: Application
    Filed: March 4, 2016
    Publication date: May 24, 2018
    Inventors: Steven E. Spoldi, Alex Faynberg, Stephen Kubik, Donald T. Ream, John Rucci, Stephen C. McCulley, Christiaan Corry
  • Patent number: 9308985
    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: Grant
    Filed: April 11, 2014
    Date of Patent: April 12, 2016
    Assignee: SIKORSKY AIRCRAFT CORPORATION
    Inventors: Stephen Kubik, Alex Faynberg, Stephen C. Mcculley, John P. Rucci, Christiaan P. Corry, Edward Pavelka
  • 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