• Title/Summary/Keyword: Meteorological Satellite

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TRANSFER ORBIT THERMAL ANALYSIS FOR SATELLITE (위성의 전이궤도 열해석)

  • Jun, Hyoung-Yoll;Kim, Jung-Hoon;Kim, Sung-Hoon;Yang, Koon-Ho
    • 한국전산유체공학회:학술대회논문집
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    • 2007.10a
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    • pp.227-231
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    • 2007
  • COMS (Communication, Ocean and Meteorological Satellite) is a geostationary satellite and has been developing by KARI for communication and ocean and meteorological observations. It will be launched by ARIANE 5. Ka-band components are installed on South panel, where single solar array wing is mounted. Radiators, embedded heat pipes, external heat pipe, insulation blankets and heaters are utilized for the thermal control of the satellite. The Ka-band payload section is divided several areas based on unit operating temperature in order to optimize radiator area and maximize heat rejection capability. Other equipment for sensors and bus are installed on North panel. The ocean and meteorological sensors are installed on optical benches on the top floor to decouple thermally from the satellite. During the transfer orbit operation, satellite will be under severe thermal environments due to low dissipation of components, satellite attitudes and LAE(Liquid Apogee Engine) firing. This paper presents temperature and heater power prediction and validation of thermal control design during transfer orbit operation.

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Beginning of the Meteorological Satellite: The First Meteorological Satellite TIROS (기상위성의 태동: 최초의 기상위성 TIROS)

  • Ahn, Myoung-Hwan
    • Atmosphere
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    • v.22 no.4
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    • pp.489-497
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    • 2012
  • Recently released a top secret document explicitly shows that the early development plan for an earth observation satellite in the USA has a hidden and more important purpose for a concept of 'free space' than the scientific purpose. At that time, the hidden and secret concept imbedded within the early space development plan prevail other national policies of the USA government for purpose of the national security. Under these circumstances, it is quite reasonable to accept a possibility that the meteorological satellites which play a key role in the every area of meteorology and climatology was also born for the hidden purposes. Even it is so, it is quite amazing that the first meteorological satellite is launched in the USA despite of the facts that the major users of the meteorological satellites were not very enthusiastic with the meteorological satellite and the program was not started as a formal meteorological satellite project. This was only possible because of the external socio-political impact caused by the successful launch of the Russian Sputnik satellite and a few key policy developers who favored the meteorological satellite program. It is also interesting to note that the beginning of the first Korean meteorological satellite program was initiated by a similar socio-political influence occurred by the launch of a North Korean satellite.

Analysis on Spectrum for COMS User Data (COMS 사용자 데이터의 스팩트럼 분석)

  • Park Durk-Jong;Koo In-Hoi;Ahn Sang-Il
    • Proceedings of the KSRS Conference
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    • 2006.03a
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    • pp.386-389
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    • 2006
  • 본 논문에서는 2008년에 발사예정인 통신해양기상위성의 사용자 데이터의 스팩트럼에 대해 분석한 내용이 작성 되어 있다. 사용자 데이터는 통신해양기상위성에 탑재되어 있는 기상탑재체로부터 얻은 데이터에 대해 각각 radiometric과 geometric correction을 수행 후 만들어지게 된다. 사용자 데이터의 전송 형태는 전송하려는 데이터의 양과 전송시간으로부터 계산된 전송율에 따라 각각 HRIT (High Rate Information Transmission)와 LRIT (Low Rate Information Transmission)으로 나누어진다. 이들 데이터는 각각 QPSK (Quad-Phase Shift Keying), BPSK (Bi-Phase Shift Keying)로 변조된 후에 S-Band로 위성에서 수신한 후 별도의 데이터처리에 대한 과정이 없이 바로 L-Band로 송신하여 수신기를 갖춘 일반 사용자에게 영상 및 각종 기상데이터를 제공하게 된다. 본 논문에서는 이러한 사용자 데이터의 전송에 필요한 HRIT와 LRIT의 변조 및 신호 생성 그리고 현재 기본적으로 기상위성의 수신기로써 사용되는 장비를 이용하여 사용자의 처리시스템을 고려하여 구축한 후 실제 데이터수신에 대한 성능을 확인하였다. 그 결과 현재의 사용자 주파수의 간격에 대해서는 각각의 데이터를 독립적으로 처리하는데 상호간의 간섭에 대한 영향은 무시할 수 있음을 확인하였다.

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A Progress Status of Remote Sensing in the Korean Meteorological Society (한국기상학회 원격탐사 분야 학술 발전 현황)

  • Myoung-Hwan Ahn;Jhoon Kim;GyuWon Lee;Sang-Woo Kim
    • Atmosphere
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    • v.33 no.2
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    • pp.197-222
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    • 2023
  • Remote sensing becomes a new and core framework for the atmospheric sciences and closely related areas concerning with the ever-changing global environmental status. However, remote sensing in the Korea Meteorological Society is relatively new, where the first relevant paper is appeared in 1983, as well as is an area with relatively limited number of research groups. Here, we review and summarize some of the key progress in this area within Korea Meteorological Society focusing on the areas of satellite, radar, and ground based remote sensing such as lidar, spectrometer and sun photometer. Overall, the area is shown to have the most significant progress occur along with the acquisition of the key infra structures such as the COMS (Communication, Ocean and Meteorological Satellite) and S-band radar system led by Korea Meteorological Administration in early 2000. After that, the area has quickly developed into a status playing important roles to lead and support the overall activities in the atmospheric measurements. It is expected that the importance and role of the remote sensing will increase in the coming years.

Estimation of Insolation over the Oceans around Korean Peninsula Using Satellite Data

  • Park, Kyung-Won;Kim, Young-seup;Sang, Chung-Hyo
    • Proceedings of the KSRS Conference
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    • 1999.11a
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    • pp.227-230
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    • 1999
  • Surface solar radiation over the sea is estimated using Visible and Infrared Spin Scan Radiometer data onbord Geostationary Meteorological Satellite(GMS) 5 for January, 1997 to December 1997 in clear and cloudy conditions. The hourly insolation is estimated with a spatial resolution of 5$\times$ 5 km grid. The island pyranometer belonging to the Japan Meteorological Agency is used for validation of the estimated insolation. It is shown that the estimated hourly insolation has RMSE(root mean square) error of 104 W/$m^2$. The variability of the hourly solar radiation was investigated on 3 areas over seas around Korean Peninsula. The solar radiation of East Sea is similar to Yellow Sea. The maximum value of solar radiation is on June of year. The maximum value in south sea is on August because weather is poor by low pressure and front in June

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System Design of COMS(Communication, Ocean and Meteorological Satellite) Propulsion System (통신해양기상위성 추진시스템 시스템설계)

  • Park Eung-Sik;Han Cho-Young;Chae Jong-Won;Bucknell S.
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2005.11a
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    • pp.426-430
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    • 2005
  • The COMS(Communication, Ocean and Meteorological Satellite) is the first developed three-axis stabilization multi-function satellite on geostationary earth orbit(GEO) in korea, presently scheduled to be launched in 2008. The COMS propulsion system provides the thrust and torque required for the insertion into GEO, attitude and orbit control/adjustment of spacecraft. In this paper, system design of propulsion system, basic functions and design requirement of components are described.

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Derivation of SST using MODIS direct broadcast data

  • Chung, Chu-Yong;Ahn, Myoung-Hwan;Koo, Ja-Min;Sohn, Eun-Ha;Chung, Hyo-Sang
    • Proceedings of the KSRS Conference
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    • 2002.10a
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    • pp.638-643
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    • 2002
  • MODIS (MODerate-resolution Imaging Spectroradiometer) onboard the first Earth Observing System (EOS) satellite, Terra, was launched successfully at the end of 1999. The direct broadcast MODIS data has been received and utilized in Korea Meteorological Administration (KMA) since february 2001. This study introduces utilizations of this data, especially for the derivation of sea surface temperature (SST). To produce the MODIS SST operationally, we used a simple cloud mask algorithm and MCSST algorithm. By using a simple cloud mask algorithm and by assumption of NOAA daily SST as a true SST, a new set of MCSST coefficients was derived. And we tried to analyze the current NASA's PFSST and new MCSST algorithms by using the collocated buoy observation data. Although the number of collocated data was limited, both algorithms are highly correlated with the buoy SST, but somewhat bigger bias and RMS difference than we expected. And PFSST uniformly underestimated the SST. Through more analyzing the archived and future-received data, we plan to derive better MCSST coefficients and apply to MODIS data of Aqua that is the second EOS satellite. To use the MODIS standard cloud mask algorithm to get better SST coefficients is going to be prepared.

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Red Tide Prediction in the Korean Coastal Areas by RS and GIS

  • Yoon, Hong-Joo
    • Proceedings of the KSRS Conference
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    • v.1
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    • pp.332-335
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    • 2006
  • Red tide(harmful algae) in the Korean Coastal Waters has a given a great damage to the fishery every year. However, the aim of our study understands the influence of meteorological factors (air and water temperature, precipitation, sunshine, solar radiation, winds) relating to the mechanism of red tide occurrence and monitors red tide by satellite remote sensing, and analyzes the potential area for red tide occurrence by GIS. The meteorological factors have directly influenced on red tide formation. Thus, We want to predict and apply to red tide formation from statistical analyses on the relationships between red tide formation and meteorological factors. In future, it should be realized the near real time monitoring for red tide by the development of remote sensing technique and the construction of integrated model by the red tide information management system (the data base of red tide - meteorological informations). Finally our purpose is support to the prediction information for the possible red tide occurrence by coastal meteorological information and contribute to reduce the red tide disaster by the prediction technique for red tide.

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TRANSFER ORBIT THERMAL ANALYSIS FOR COMS (통신해양기상위성의 전이궤도 열해석)

  • Jun, Hyoung-Yoll;Kim, Jung-Hoon;Kim, Sung-Hoon;Yang, Koon-Ho
    • Journal of computational fluids engineering
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    • v.13 no.2
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    • pp.48-54
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    • 2008
  • COMS (Communication, Ocean and Meteorological Satellite) is a geostationary satellite and has been developing by KARI for communication, ocean and meteorological observations. It will be launched by ARIANE 5. Ka-band components are installed on South panel, where single solar array wing is mounted. Radiators, embedded heat pipes, external heat pipe, insulation blankets and heaters are utilized for the thermal control of the satellite. The Ka-band payload section is divided several areas based on unit operating temperature in order to optimize radiator area and maximize heat rejection capability. Other equipment for sensors and bus are installed on North panel. The ocean and meteorological sensors are installed on optical benches on the top floor to decouple thermally from the satellite. During the transfer orbit operation, satellite will be under severe thermal environments due to low dissipation of components, satellite attitudes and LAE(Liquid Apogee Engine) firing. This paper presents temperature and heater power prediction and validation of thermal control design during transfer orbit operation.

Preprocessing of the Direct-broadcast Data from the Atmospheric Infared Sounder (AIRS) Sounding Suite on Aqua Satellite

  • Kim, Seungbum;Park, Hyesook;Kim, Kumlan;Park, Seunghwan;Kim, Moongyu;Lee, Jongju
    • Atmosphere
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    • v.13 no.4
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    • pp.71-79
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    • 2003
  • We present a pre processing system for the Atmospheric Infrared Sounder (AIRS) sounding suite onboard Aqua satellite. With its unprecedented 2378 channels in IR bands, AIRS aims at achieving the sounding accuracy [s1]of a radiosonde (1 K in 1-km layer for temperature and 10% in 2-km layer for humidity). The core of the pre p rocessor is the International MODIS/AIRS Processing Package (IMAPP) that performs the geometric and radiometric correction to compute the Earth's radiance. Then we remove spurious data and retrieve the brightness temperature (Tb). Since we process the direct-broadcast data almost for the first time among the AIRS directbroadcast community, special attention is needed to understand and verify the products. This includes the pixel-to-pixel verification of the direct-broadcast product with reference to the fullorbit product, which shows the difference of less than $10^{-3}$ K in IR Tb.