• Title/Summary/Keyword: 406 MHz beacon

Search Result 3, Processing Time 0.018 seconds

Analysis of COSPAS-SARSAT 406 MHz Personal Locator Beacon Specification (COSPAS-SARSAT 406 MHz 개인용 탐색구조 단말기의 기술기준 분석)

  • Jeong, Gi-ryong;Jeong, Seong-hoon;Lim, Jong-gun
    • Journal of Advanced Navigation Technology
    • /
    • v.22 no.6
    • /
    • pp.514-521
    • /
    • 2018
  • COSPAS-SARSAT 406 MHz emergency beacons include ELTs for aviation, EPIRBs for maritime, and PLBs for individuals in distress. They are used to sending messages encoded on 406 MHzdistress frequency and sending alertsfor search and rescue in distress. C/S T.001 and T.018 are COSPAS-SARSAT technical documents. They include basic technical information needed for developing beacons, howmessages are constructed, and test methods for type approval. COSPAS-SARSAT systems that use existing low earth orbit (LEO) and geostationary earth orbit (GEO) satellites do not have a return link service (RLS). So, the survivors could not confirm whether the distress signal was sending or not. However, a new medium earth orbit (MEO)satellite system has been added to thissystem, allowing confirmation through the RLS function. This paper analyzed C/S T.001 and T.018 needed to develop navigation structuresthat incorporated improved PLB of 406 MHz, a homing signal generator of 121.5 MHz, and a VHF AM transmitter for aviation of 243 MHz.

Analysis of the Detection Time of Distress Signal for LEOSAR and MEOSAR Systems (LEOSAR 및 MEOSAR 시스템의 조난신호 탐지시간 해석)

  • Lim, Sang-Seok
    • Journal of Advanced Navigation Technology
    • /
    • v.10 no.4
    • /
    • pp.377-384
    • /
    • 2006
  • In this paper the detection time of the distress signal for the satellite-based search and rescue (SAR) system is evaluated. Present LEOSAR system in operation employs a few Low-altitude Earth Orbit (LEO) satellites and hence provides poor and local coverage availability. This results in a considerably long waiting time for a distress beacon to be detected by a rescue mission control center. One can expect that the detection time of the distress signal will be significantly reduced if the proposed MEOSAR system, which is based on the Medium-altitude Earth Orbit (MEO) satellites, is implemented. Taking into account the influence of the obstacles on the beacon signal, simulations are carried out to evaluate the detection time of distress signals for the LEOSAR and MEOSAR systems and the corresponding results are analyzed.

  • PDF

Beacon Geolocation Scheme of COSPAS-SARSAT System for Heavy Disaster Environment (다중 재난 상황에 적합한 COSPAS-SARSAT 탐색구조 비컨 위치추정 기법)

  • Kim, Jaehyun;Lee, Sanguk;Sin, Cheonsig;Ahn, Woo-Geun
    • Journal of Satellite, Information and Communications
    • /
    • v.10 no.4
    • /
    • pp.146-150
    • /
    • 2015
  • The COSPAS-SARSAT committee decides MEOSAR (Medium-Earth Orbit for search and rescue) service development for installing 406MHz SAR instruments on their respective MEO navigation satellite system of the United States, EU, and Russia, since 2000. The transmitted beacon signal is separately arrived by satellites with different FOA (Frequency of Arrival) and TOA (Time of Arrival). It is directly transferred to MEOLUT. In MEOLUT, a LUT track at least 3 or 4 satellites simultaneously and estimate location of beacon using time difference of arrival (TDOA) and frequency difference arrival (FDOA). But the transmitted distress signals may be overlapped each other because the distress beacons transmit signal on mean interval of 50 seconds in arbitrary time. It's difficult that simultaneously estimate location of beacon by current scheme for several overlapped distress signal. So we use cross ambiguity function (CAF) Map algorithm and present Multi-CAF MAP scheme in order to satisfy performance requirement of system. The performance is analyzed for COSAPS-SARSAT MEOSAR.