• Title/Summary/Keyword: KOMPSAT MSC

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ACTIVITIES OF CALIBRATION AND VALIDATION FOR THE KOMPSAT-2 MSC DATA

  • Lee Dong-Han;Lee Sun-Gu;Seo Doo-Chun;Song Jeong-Heon;Shih Jae-Min;Kim Yongseung;Lim Hyo-Suk;Paik Hong-Yul
    • Proceedings of the KSRS Conference
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    • 2005.10a
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    • pp.620-623
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    • 2005
  • KARI has prepared Calibration and Validation activities for the KOMPSAT-2 (KOrea Multi-Purpose SATellite-2) MSC data that will be launched at the end of this year. Firstly, we divided the Cal/Val activities of it to four parts, Spatial, Spectral, Radiometric and Geometric, and defmed the detailed Cal/Val items from them. Secondly, Cal/Val targets have been defined and manufactured for the role of them. Thirdly, we have made the plan and the procedure for the Cal/Val items, developed the codes for them, studied more detailed method to do them, and trained the Cal/Val activities using the foreign satellite image data by ourselves. KARI has been now setting up the KOMPSAT-2 LEOP plan with the Cal/Val activities, and probably will finish the EOP Cal/Val activities for the KOMPSAT-2 MSC data by the next April or May.

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DEVELOPING FOREST TYPE CLASSIFICATION METHODOLOGY USING KOMPSAT IMAGE BASED ON TASSELED CAP TRANSFORMATION

  • Kim, Sung-Jae;Jo, Yun-Won;Jo, Myung-Hee
    • Proceedings of the KSRS Conference
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    • 2008.10a
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    • pp.358-360
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    • 2008
  • Recently there are many pilot studies for advanced application of first Korea national high resolution satellite image, which is called as KOMPSAT-MSC (Korean Multi-purpose Satellite-Multi-Spectral Camera), in Korea. In this study the forest type classification methodology is developed and its distribution map was constructed by applying high resolution satellite image, KOMPSAT-MSC, based on Tasseled Cap Transformation, especially through comparing the result of detailed filed surveying such as forest type, tree species, tree diameter, tree age and tree crown density in pilot study area.

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INITIAL GEOMETRIC ACCURACY OF KOMPSAT-2 HIGH RESOLUTION IMAGE

  • Seo, Doo-Chun;Lim, Hyo-Suk;Shin, Ji-Hyeon;Kim, Moon-Gyu
    • Proceedings of the KSRS Conference
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    • v.2
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    • pp.780-783
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    • 2006
  • The KOrea Multi-Purpose Satellite-2 (KOMPSAT-2) was launched in July 2006 and the main mission of the KOMPSAT-2 is a high resolution imaging for the cartography of Korea peninsula by utilizing Multi Spectral Camera (MSC) images. The camera resolutions are 1 m in panchromatic scene and 4 m in multi-spectral imaging. This paper provides an initial geometric accuracy assessment of the KOMPSAT-2 high resolution image without ground control points and briefly introduces the sensor model of KOMPSAT-2. Also investigated and evaluated the obtained 3-dimensional terrain information using the MSC pass image and scene images acquired from the KOMPSAT-2 satellite.

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KOMPSAT-2 MSC DCSU Operational Concept

  • Lee, Jong-Tae;Lee, Sang-Gyu;Lee, Sang-Taek
    • Proceedings of the KSRS Conference
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    • 2002.10a
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    • pp.821-826
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    • 2002
  • The KOMPSAT-2 DCSU(the data compression & storage unit) performs the acquisition of image data from cameras, the compression with requested compression rate, the storage with specified file ID on the mission command and the distribution to the assigned DLS(Data Link System) channels per the mission and operation requirements. The worldwide observation using the MSC is able to be achieved by this DCSU's behavior. This paper presents the features of KOMPSAT-2 DCSU and provides proper ground operation concept after launch.

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RELIABILITY ANALYSIS OF THE MSC SYSTEM

  • Kim, Young-Soo;Lee, Do-Kyoung;Lee, Chang-Ho;Woo, Sun-Hee
    • Journal of Astronomy and Space Sciences
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    • v.20 no.3
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    • pp.217-226
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    • 2003
  • MSC (Multi-Spectral Camera) is the payload of KOMPSAT-2, which is being developed for earth imaging in optical and near-infrared region. The design of the MSC is completed and its reliability has been assessed from part level to the MSC system level. The reliability was analyzed in worst case and the analysis results showed that the value complies the required value of 0.9. In this paper, a calculation method of reliability for the MSC system is described, and assessment result is presented and discussed.

Real-Time Software Design using VxWorks for MSC(Multi-Spectral Camera) on KOMPSAT-2

  • Heo, Haeng-Pal;Yong, Sang-Soon;Kong, Jong-Pil;Kim, Young-Sun;Youn, Heong-Sik
    • 제어로봇시스템학회:학술대회논문집
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    • 2001.10a
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    • pp.92.6-92
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    • 2001
  • MSC is being developed to be installed on KOMPSAT(Korea Multi-Purpose Satellite-II and to provide high resolution multi-spectral. MSC consists of three main subsystems. One is EOS(Electro-Optics Subsystem), another is PMU(Payload Management Unit) and the other is PDTS(Payload Data Transmission Subsystem). There is an SBC(Single Board Computer) in the PMU to control all MSC subsystems. SBC incorporates Intel 80486 as a main processor and VxWorks as a real-time operating system. SBC software consists of four main tasks and several modules to deal with all control information for imaging and all the state of health telemetrv data, and to perform interface with another MSC units. SBC software also has to handle a lot of commands in order for MSC to perform his mission. One mission command consists of a series of related commands, which are In be executed in the designated sequence, with a specified time ...

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Development of TPF Generation SIW for KOMPSAT-2 X-Band Antenna Motion Control

  • Kang C. H.;Park D. J.;Seo S. B.;Koo I. H.;Ahn S. I.;Kim E. K.
    • Proceedings of the KSRS Conference
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    • 2005.10a
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    • pp.485-488
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    • 2005
  • The 2nd KOrea Multi-Purpose Satellite (KOMPSAT -2) has been developed by Korea Aerospace Research Institute (KARI) since 2000. Multi Spectral Camera (MSC) is the payload for KOMPSAT -2, which will provide the observation imagery around Korean peninsula with high resolution. KOMPSAT-2 has adopted X-band Tracking System (XTS) for transmitting earth observation data to ground station. For this, data which describes and controls the pre-defined motion of each on-board X-Band antenna in XTS, must be transmitted to the spacecraft as S-Band command and it is called as Tracking Parameter Files (TPF). In this paper, the result of the development of TPF Generation S/W for KOMPSAT-2 X-Band Antenna Motion Control.

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SYSTEM TRADE-OFF STUDY AND OPTO-THERMO-MECHANICAL ANALYSIS OF A SUNSHIELD ON THE MSC OF THE KOMPSAT-2

  • Kim, Young-Soo;Lee, Eung-Shik;Woo, Sun-Hee
    • Journal of Astronomy and Space Sciences
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    • v.20 no.4
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    • pp.393-402
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    • 2003
  • The Multi-Spectral Camera (MSC) is the payload of KOMPSAT-2 which is designed for earth imaging in optical and near-infrared region on a sun-synchronous orbit. The telescope in the MSC is a Ritchey-Chretien type with large aperture. The telescope structure should be well stabilized and the optical alignment should be kept steady so that best images can be achieved. However, the MSC is exposed to adverse thermal environment on the orbit which can give impacts on optical performance. Solar incidence can bring non-uniform temperature rise on the telescope tube which entails unfavorable thermal distortion. Three ways of preventing the solar radiation were proposed, which were installing external mechanical shield, internal shield, and maneuvering the spacecraft. After trade-off study, internal sun shield was selected as a practical and optimal solution to minimize the effect of the solar radiation. In addition, detailed designs of the structure and sunshield were produced and analyses have been performed. The results were assessed to verify their impacts to the image quality. It was confirmed that the internal sunshield complies with the requirements and would improve image quality.

KOMPSAT-2 위성의 요각 계산방법 연구

  • Kim, Jong-Ah;Kang, Keum-Sil;Jang, Young-Jun;Yong, Sang-Soon;Kang, Song-Doug;Youn, Heong-Sik
    • Aerospace Engineering and Technology
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    • v.3 no.2
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    • pp.160-169
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    • 2004
  • In order to get the high resolution satellite image, MSC has TDI function in the KOMPSAT-2. So it is required to control the yaw angle of the attitude as operation concepts of KOMPSAT-2. This study was to explain the TDI function, to set up the geometric equation to satisfy the condition, and finally to determine the equation of yaw angle. The calculating program was developed and simulated with orbit and imaging attitude as input data, and the results were compared with the yaw steering values calculated in the on-board computer.

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MODTRAN 모델을 이용한 다목적 실용위성 2호 MSC의 입사복사량 계산

  • Kim, Yong-Seung;Kang, Chi-Ho
    • Aerospace Engineering and Technology
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    • v.1 no.1
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    • pp.173-176
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    • 2002
  • This report summarizes the results of MODTRAN model that are used for the calculation of input radiance of the KOMPSAT-2 Multispectral Camera (MSC). We have calculated the input radiances for four months: January 15, April 15, July 15 and October 15. Annual averages are the arithmetic mean of results from four months. We used the mid-latitude winter and summer for the month of January and July, respectively, while US standard atmospheres are used for April and October. The orbital characteristics of KOMPSAT-2 and the seasonal variations of solar zenith angle over the Korean peninsula were incorporated as inputs to the model. The tropospheric aerosol extinction (visibility = 50 km) was assumed. The surface albedo used in the model calculation represents the global annual mean clear-sky albedo. MSC contract values are found to be considerably greater in the MSC spectral range than the total radiances calculated with the above general conditions. From these results, it can be inferred that the forthcoming MSC images would be somewhat dark. We certainly need a countermeasure for this issue.

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