Patents by Inventor Kenji AHUALLE HORIMOTO

Kenji AHUALLE HORIMOTO 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: 9561868
    Abstract: A method and device including a unit to extract a linear terrain profile stored in memory, a terrain height for a current distance of the aircraft, a unit for determining a current height of the aircraft with respect to the terrain, using at least one measurement taken by a radar altimeter, a unit for computing a first current altitude of the aircraft, using the terrain height and the current height, a unit for computing a second current altitude of the aircraft, corresponding to an altitude on an approach profile of the current position of the aircraft and a unit for computing the difference between the first and second current altitudes, the difference being transmitted to a guidance unit to vertically guide the aircraft.
    Type: Grant
    Filed: December 30, 2014
    Date of Patent: February 7, 2017
    Assignee: AIRBUS OPERATIONS (S.A.S.)
    Inventors: Thierry Bourret, Kenji Ahualle Horimoto
  • Patent number: 9342988
    Abstract: A device comprising a computation unit for computing, for each of a plurality of different distances relative to a threshold of a landing runway along a lateral approach trajectory, a geometric altitude, using a measured and stored barometric altitude, a computation unit for computing a terrain height, by subtracting, from the computed geometric altitude, a measured and stored height, and a computation unit for determining a terrain profile from the set of terrain heights computed for the set of different distances.
    Type: Grant
    Filed: December 30, 2014
    Date of Patent: May 17, 2016
    Assignee: AIRBUS OPERATIONS (S.A.S.)
    Inventors: Thierry Bourret, Kenji Ahualle Horimoto
  • Publication number: 20150317905
    Abstract: A device comprising a computation unit for computing, for each of a plurality of different distances relative to a threshold of a landing runway along a lateral approach trajectory, a geometric altitude, using a measured and stored barometric altitude, a computation unit for computing a terrain height, by subtracting, from the computed geometric altitude, a measured and stored height, and a computation unit for determining a terrain profile from the set of terrain heights computed for the set of different distances.
    Type: Application
    Filed: December 30, 2014
    Publication date: November 5, 2015
    Inventors: Thierry Bourret, Kenji AHUALLE HORIMOTO
  • Publication number: 20150203214
    Abstract: A method and device including a unit to extract a linear terrain profile stored in memory, a terrain height for a current distance of the aircraft, a unit for determining a current height of the aircraft with respect to the terrain, using at least one measurement taken by a radar altimeter, a unit for computing a first current altitude of the aircraft, using the terrain height and the current height, a unit for computing a second current altitude of the aircraft, corresponding to an altitude on an approach profile of the current position of the aircraft and a unit for computing the difference between the first and second current altitudes, the difference being transmitted to a guidance unit to vertically guide the aircraft.
    Type: Application
    Filed: December 30, 2014
    Publication date: July 23, 2015
    Inventors: Thierry Bourret, Kenji AHUALLE HORIMOTO