• Title/Summary/Keyword: Goheung Aeronautical Center

Search Result 3, Processing Time 0.018 seconds

Implementation and Operational Test of ADS-B System in Goheung Aeronautical Center (고흥항공센터 ADS-B 구축 및 운용시험)

  • Yoo, Chang-Sun;Song, Bok-Sub;Cho, Am;Sung, Ki-Jung;Koo, Sam-Ok
    • Aerospace Engineering and Technology
    • /
    • v.13 no.1
    • /
    • pp.1-9
    • /
    • 2014
  • Goheung aeronautical center is located in the area of Goheung of which land is reclaimed from sea and has a runway of length 700m, width 25m with test facility which has been used for flight test of UAV and small aircraft. To support the enhancement of aircraft safety, 1090ES ADS-B ground system as the ground surveillance system has been implemented. ADS-B system based on GPS and digital data link provides the function of enhancing the aircraft safety through flight information among aircrafts. This paper gives the result that the implementation of ADS-B ground system and the flight test with onboard ADS-B transmitter has been conducted.

Operation of the GPS Receiver System for KSLV-I on the Launch Site at Naro Space Center (나로우주센터 발사장에서 나로호 GPS 수신기 시스템의 운용)

  • Kwon, Byung-Moon;Moon, Ji-Hyeon;Shin, Yong-Sul;Choi, Hyung-Don;Cho, Gwang-Rae
    • Journal of the Korean Society for Aeronautical & Space Sciences
    • /
    • v.38 no.7
    • /
    • pp.737-745
    • /
    • 2010
  • This paper describes the operation results of the GPS receiver system for KSLV (Korea Space Launch Vehicle)-I on the launch site at Naro Space Center that is the first spaceport of South Korea located at Goheung. All equipments of KSLV-I including the GPS receiver system should be monitored and controlled through hard-wired interface during KSLV-I is on standby at the launch pad. The GPS receiver for KSLV-I is connected to triple almost omni-directional patch antennas mounted on the cylindrical surface of KSLV-I that should be erected vertically on the launch pad until lift-off. Signal interference and multipath effects observed in the GPS receiver on the launch site are analyzed in this paper based on the GPS signals received from each GPS antenna.

Tracking and Orbit Determination of International Space Station using Radar (레이더를 이용한 국제우주정거장 추적 및 궤도결정)

  • Yu, Ki-Young;Chung, Dae-Won
    • Journal of the Korean Society for Aeronautical & Space Sciences
    • /
    • v.44 no.5
    • /
    • pp.447-454
    • /
    • 2016
  • Increase of space debris makes low earth orbit(LEO) environment more complex day by day and space situation Awareness(SSA) is becoming more important. As an essential part of SSA, space object surveillance and tracking is studied by many countries including America and Europe. And radar system forms the backbone of an space surveillance and tracking. Currently, Korea operates many LEO satellites like KOMPSAT but does not have dedicated radar systems which provide collision surveillance between satellite and space debris. Korea Aerospace Research Institute(KARI) NARO space center operates launch-vehicle tracking radar system in GOHEUNG and JEJU, respectively. In this paper, we describe developing operation concept to track International Space Station(ISS) using NARO radar and results of tracking. Then, we describe ISS orbit determination using radar tracking data. Lastly, orbit determination result is compares with TLE for analyzing effectiveness of orbit determination.