Patents by Inventor Gregory Ortet

Gregory Ortet 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).

  • Method and device for determining a reliable position of an aircraft
    Patent number: 8244467
    Abstract: The invention relates to a method and device for determining a reliable position of an aircraft. The device (1) includes means (3, 10) for determining different aircraft position values and means (8, 16, 18) for deducing a reliable position therefrom, using coherence tests and a consolidation method.
    Type: Grant
    Filed: June 16, 2008
    Date of Patent: August 14, 2012
    Assignee: Airbus Operations SAS
    Inventors: Jean-Philippe Huynh, Alain Guillet, Stéphane Dattler, Grégory Ortet
  • Method and device for monitoring a position indication of an aircraft
    Patent number: 7908046
    Abstract: A device and method calculate a global error relating to a position indication of an aircraft and compare the global error with a threshold value, which depends on flight constraints.
    Type: Grant
    Filed: May 19, 2008
    Date of Patent: March 15, 2011
    Assignee: Airbus France
    Inventors: Jean-Philippe Huynh, Alain Guillet, Stephane Dattler, Gregory Ortet
  • METHOD AND DEVICE FOR DETERMINING A RELIABLE POSITION OF AN AIRCRAFT
    Publication number: 20100169014
    Abstract: The invention relates to a method and device for determining a reliable position of an aircraft. The device (1) includes means (3, 10) for determining different aircraft position values and means (8, 16, 18) for deducing a reliable position therefrom, using coherence tests and a consolidation method.
    Type: Application
    Filed: June 16, 2008
    Publication date: July 1, 2010
    Applicant: Airbus Operations (SAS)
    Inventors: Jean-Philippe Huynh, Alain Guillet, Stéphane Dattler, Grégory Ortet
  • METHOD AND DEVICE FOR MONITORING A POSITION INDICATION OF AN AIRCRAFT
    Publication number: 20080294306
    Abstract: The device (1) comprises means (8, 9, 10) for calculating a global error relating to a position indication of the aircraft, means (13) for comparing this global error with a threshold value which depends on the flight constraints, and alarm means (15).
    Type: Application
    Filed: May 19, 2008
    Publication date: November 27, 2008
    Applicant: AIRBUS France
    Inventors: Jean-Philippe Huynh, Alain Guillet, Stephane Dattler, Gregory Ortet
  • Device For Assisting a Vertical Guidance Approach For Aircraft
    Publication number: 20080172149
    Abstract: The invention concerns an approach assisting device (1) comprising a flight management system (2) which determines an approach paths, an inertial reference system (3) which prepares inertial position data, which receives position data of the aircraft, and which determines a hybrid position of said aircraft, a landing assisting multimode receiver (4) which receives data concerning said approach path and said hybrid position, and which deduces therefrom lateral and vertical angular differences, at least when said approach axis is captured, and a guiding system (7) which receives said lateral and vertical angular differences and uses same for guiding the aircraft, at least when said approach path is captured.
    Type: Application
    Filed: July 11, 2006
    Publication date: July 17, 2008
    Applicant: AIRBUS FRANCE
    Inventors: Patrice Rouquette, Adrien Ott, Laure Maes, Caroline Aucher, Melanie Bats, Gregory Ortet