Patents by Inventor Hyang-Sig JUN

Hyang-Sig JUN 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: 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
  • Patent number: 9911343
    Abstract: An integrated landing receiver for landing of an aircraft and a controlling method thereof are provided, in which the integrated landing receiver includes a receiver including a plurality of signal information processors that generate landing guidance information respectively corresponding to a plurality of landing support facilities, a collector collecting the landing guidance information respectively generated at the plurality of signal information processors, and an integrator generating integrated landing guidance information by using the landing guidance information collected at the collector and outputting the result. Accordingly, when a plurality of landing support facilities are installed together at an airport, the landing guidance information provided from these landing support facilities are mixed and provided so that shortcomings that each landing supporting facility may have can be advantageously compensated, thus enabling safe and effective provision of the landing guidance information.
    Type: Grant
    Filed: July 24, 2015
    Date of Patent: March 6, 2018
    Assignee: KOREA AEROSPACE RESEARCH INSTITUTE
    Inventors: Myeong-Sook Jeong, Hyang-Sig Jun, Joong-Won Bae
  • 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
  • Publication number: 20160328982
    Abstract: An integrated landing receiver for landing of an aircraft and a controlling method thereof are provided, in which the integrated landing receiver includes a receiver including a plurality of signal information processors that generate landing guidance information respectively corresponding to a plurality of landing support facilities, a collector collecting the landing guidance information respectively generated at the plurality of signal information processors, and an integrator generating integrated landing guidance information by using the landing guidance information collected at the collector and outputting the result. Accordingly, when a plurality of landing support facilities are installed together at an airport, the landing guidance information provided from these landing support facilities are mixed and provided so that shortcomings that each landing supporting facility may have can be advantageously compensated, thus enabling safe and effective provision of the landing guidance information.
    Type: Application
    Filed: July 24, 2015
    Publication date: November 10, 2016
    Applicant: KOREA AEROSPACE RESEARCH INSTITUTE
    Inventors: Myeong-Sook JEONG, Hyang-Sig JUN, Joong-Won BAE