Patents by Inventor Dae-Keun JEON

Dae-Keun JEON 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).

  • Aircraft landing apparatus using GNSS and SBAS signals, and control method thereof
    Patent number: 10043403
    Abstract: A landing receiving apparatus for aircraft landing, and a control method thereof are provided, in which the landing receiving apparatus includes a flight management system (FMS) which is inputted with, by a user, destination airport, destination runway, and a receiver mode, a data storage portion which stores approach path data for landing of the aircraft; a receiver portion which calculates aircraft position information by using Global Navigation Satellite System (GLASS) signals and Satellite-Based Augmentation System (SBAS) signals transmitted from an antenna portion, when a receiver mode inputted by a user is a GNSS/SBAS combination mode, and a landing guidance information generating portion which generates landing guidance information by using approach path data corresponding to a destination airport and a destination runway inputted by the user, and the aircraft position information, and transmits the generated landing guidance information to the FMS.
    Type: Grant
    Filed: April 14, 2016
    Date of Patent: August 7, 2018
    Assignee: KOREA AEROSPACE RESEARCH INSTITUTE
    Inventors: Myeong-Sook Jeong, Dae-Keun Jeon, Joongwon Bae, Hyang-sig Jun, Young Jae Lee
  • Method for coupling flight plan and flight path using ADS-B information
    Patent number: 10037703
    Abstract: The present invention relates to a method for coupling a flight plan and a flight path using ADS-B information, and more specifically to a method for coupling a flight plan and a flight path, wherein a flight data processing unit of an air traffic control system or an arrival management system separately and directly receives ADS-B information such that the received ADS-B information can be used for coupling a flight plan and a flight path of an aircraft.
    Type: Grant
    Filed: November 28, 2014
    Date of Patent: July 31, 2018
    Assignee: Korea Aerospace Research Institute
    Inventors: Hyoun Kyoung Kim, Dae Keun Jeon
  • METHOD FOR COUPLING FLIGHT PLAN AND FLIGHT PATH USING ADS-B INFORMATION
    Publication number: 20170330465
    Abstract: The present invention relates to a method for coupling a flight plan and a flight path using ADS-B information, and more specifically to a method for coupling a flight plan and a flight path, wherein a flight data processing unit of an air traffic control system or an arrival management system separately and directly receives ADS-B information such that the received ADS-B information can be used for coupling a flight plan and a flight path of an aircraft.
    Type: Application
    Filed: November 28, 2014
    Publication date: November 16, 2017
    Applicant: KOREA AEROSPACE RESEARCH INSTITUTE
    Inventors: Hyoun Kyoung KIM, Dae Keun JEON
  • AIRCRAFT LANDING APPARATUS USING GNSS AND SBAS SIGNALS, AND CONTROL METHOD THEREOF
    Publication number: 20170116866
    Abstract: A landing receiving apparatus for aircraft landing, and a control method thereof are provided, in which the landing receiving apparatus includes a flight management system (FMS) which is inputted with, by a user, destination airport, destination runway, and a receiver mode, a data storage portion which stores approach path data for landing of the aircraft; a receiver portion which calculates aircraft position information by using Global Navigation Satellite System (GLASS) signals and Satellite-Based Augmentation System (SBAS) signals transmitted from an antenna portion, when a receiver mode inputted by a user is a GNSS/SBAS combination mode, and a landing guidance information generating portion which generates landing guidance information by using approach path data corresponding to a destination airport and a destination runway inputted by the user, and the aircraft position information, and transmits the generated landing guidance information to the FMS.
    Type: Application
    Filed: April 14, 2016
    Publication date: April 27, 2017
    Applicant: KOREA AEROSPACE RESEARCH INSTITUTE
    Inventors: Myeong-Sook JEONG, Dae-Keun JEON, Joongwon BAE, Hyang-sig JUN, Young Jae LEE