• Title/Summary/Keyword: KOMPSAT 5호

Search Result 89, Processing Time 0.023 seconds

Accuracy Evaluation of DEM Produced by using KOMPSAT-5 InSAR Image (KOMPSAT 5호 InSAR영상을 이용한 DEM제작 정확도 평가)

  • Han, Seung-Hee
    • Journal of Cadastre & Land InformatiX
    • /
    • v.47 no.2
    • /
    • pp.39-47
    • /
    • 2017
  • The SAR payload of the KOMPSAT-5 is equipped with an X-band (9.66GHz) microwave-based sensor. Especially, since it has a fixed antenna that can be electronically steered with respect to the azimuth and elevation planes, various applications are expected. This study evaluates the production performance and the accuracy of the DEM by producing DEM using the HR and UH mode images of KOMPSAT-5. To evaluate the production performance of the DEM, the sensitivity of DEM was assessed through a baseline analysis and $2{\pi}$ ambiguity; it was found to have good production performance. In addition, to evaluate the accuracy of the produced DEM, 30 check points were compared with SRTM data. As a result, STDEV ${\pm}15-20m$ accuracy was obtained. If the accuracy of the DEM is improved by adjusting the parameters of the filtering method or phase unwrapping method in the future, it will be possible to widely use the KOMPSAT-5 image for environmental and disaster monitoring.

Analysis of the Collision Probability and Mission Environment for Space debris (아리랑 위성 2호와 5호의 우주파편에 대한 충돌확률 및 임무환경 분석)

  • Seong, Jae-Dong;Min, Chan-Oh;Lee, Dae-Woo;Cho, Kyeum-Rae;Kim, Hae-Dong
    • Journal of the Korean Society for Aeronautical & Space Sciences
    • /
    • v.38 no.11
    • /
    • pp.1144-1151
    • /
    • 2010
  • The increasing number of orbital debris objects is a risk for satellites because of past 50 years space activities. The LEO (low earth orbit) where KOMPSAT-2 and KOMPSAT-5 are operated is including about 84% of the total space debris. Thus, the space missions need to consider the space debris. In this paper, we analysis the orbit characteristics and spatial density of space debris about KOMPSAT-2 that is in activity and KOMPSAT-5 that will be launched in 2010. Analyzed probability damage and collision with space debris are also performed. ESA MASTER2005 and of NASA DAS2.0 are used to analysis KOMPSAT mission environment. As a result, it is noted that KOMPSAT-2's collision probability was far more than KOMPSAT-5 because KOMPSAT-2's orbit has high density composed space debris.

Design and Development of Polar Integrated Ingestion System for KOMPSAT-2/3/5 (KOMPSAT-2/3/5 극지 통합수신시스템 설계 및 개발)

  • Kim, Jiyoung;Seo, Jungwon;Chae, Taebyeong
    • Journal of Satellite, Information and Communications
    • /
    • v.10 no.3
    • /
    • pp.102-108
    • /
    • 2015
  • With the constantly increasing demand of domestic and oversea satellite images, there is also a growing demand to rapidly acquire images after the satellite image collection planning of KOMPSAT-2/3/5. Therefore, it has been increasing to use the korea ground station and oversea ground station to keep pace with increased demand. The KARI is operating Data Ingestion System of the KOMPSAT-2/3 in Svalbard, where the satellite images have been received at least four or six times a day. The KARI is planning to operate oversea receiving system for KOMPSAT-5/3A. This paper introduces the polar data ingestion system operating in Norway, and presents the process of design and development for Polar Integration receiving system in preparation of multiple satellite operation.

Orbit Analysis for KOMPSAT-2 During LEOP and Mission Lifetime (아리랑위성 2호 초기운용 및 임무기간 중 궤도 분석)

  • Kim, Hae-Dong;Jung, Ok-Chul;Kim, Eun-Kyou
    • Journal of the Korean Society for Aeronautical & Space Sciences
    • /
    • v.38 no.9
    • /
    • pp.914-924
    • /
    • 2010
  • In this paper, results on the orbit analysis for the KOMPSAT-2 satellite using a real orbit data during the LEOP and normal mission lifetime are presented. In particular, the preparation and performance of an orbit operations during the LEOP is emphasized and the effects of space environments (i.e., Solar activity) on orbit evolutions are investigated comparing to those of the KOMPSAT-1 satellite. The summarized results in this paper would be an important reference to improve the stability and effectiveness of satellite operations during the LEOP and normal mission lifetime in case of LEO satellites such as successors of KOMPSAT-2 (i.e., KOMPSAT-3, KOMPSAT-3A, KOMPSAT-5).

A Conceptual Design of Integrated Receiving end for Multi-Satellite Mission Data Processing (다중위성 운영을 위한 통합 자료처리 시스템의 개념적 설계)

  • Bae, Hee-Jin;Chae, Tae-Byeong;Oh, Seung-Hyeub
    • Journal of Korea Society of Industrial Information Systems
    • /
    • v.15 no.2
    • /
    • pp.17-22
    • /
    • 2010
  • Establishment of systematic platform is needed for technological progress of receiving of satellite image data with high quality and processing system for product generation and operation related with direct receiving system for satellite from abroad. Besides, it's necessary to develop the integrated data processing system to prohibit similar functions on developing (or being developed) for KOMPSAT-3, KOMPSAT-5 and to operate system efficiently. Therefore, conceptual design of the integrated data processing system is performed considering commercialization of KOMPSAT(Korea Multi-Purpose Satellite) series based on KOMPSAT-2 IRPE on operation in this paper.

Analysis of Collision Avoidance Maneuver Frequency for the KOMPSAT-2 and the KOMPSAT-5 (아리랑위성 2호, 5호의 우주파편 충돌회피기동 주기 분석)

  • Kim, Eun-Hyouek;Kim, Hae-Dong;Kim, Eun-Kyou;Kim, Hak-Jung
    • Journal of the Korean Society for Aeronautical & Space Sciences
    • /
    • v.39 no.11
    • /
    • pp.1033-1041
    • /
    • 2011
  • In this paper, a collision avoidance maneuver frequency for the KOMPSAT-2 and the KOMPSAT-5 is analyzed. For the statistical prediction of the avoidance maneuver frequency, mission orbits, responsive time, accepted collision probabilities, and positional uncertainties of primary and secondary objects are considered. In addition, the collision avoidance maneuver frequency of the KOMPSAT-2 is compared to the case that NORAD catalog during one year is used to calculate that of the KOMPSAT-2. As a result, the collision avoidance maneuver frequency is one per year on average and effective factors on the statistical prediction of the avoidance maneuver frequency are investigated. Efforts to improve its prediction accuracy are also discussed.

A Modified FSA Technique Using Full-aperture for SAR Spotlight Mode (SAR 집중조사모드를 위해 전 개구면을 사용하는 수정된 FSA 기법)

  • Jung, Young-Kwang;Ra, Won-Sang
    • Journal of the Korean Society for Aeronautical & Space Sciences
    • /
    • v.44 no.10
    • /
    • pp.921-932
    • /
    • 2016
  • In this paper, a modified FSA(Frequency Scaling Algorithm) is proposed for KOMPSAT-5 high-resolution SAR image generation. In order to enhance performance of azimuth compression, degraded in sub-aperture processing due to the imperfect geometric parameter of data acquisition, the full-aperture signal processing algorithm is designed based on the exact time-frequency analysis. In addition, an azimuth scaling function is newly devised to make the full-aperture processing algorithm suitable for KOMPSAT-5 sliding-spotlight mode. Different from the previous sub-aperture FSA schemes, the suggested technique could accommodate the merit of unified signal processing structure regardless of operational modes of KOMPSAT-5. Through the point target simulation, it is verified that the suggested algorithm provides superior performance of azimuth compression over the existing full-aperture processing methods. The experimental results using real data acquired by KOMPSAT-5 are also given to demonstrate the effectiveness of our scheme as well.

RETRIEVAL OF ELECTRON DENSITY PROFILE FOR KOMPSAT-5 GPS RADIO OCCULTATION DATA PROCESSING SYSTEM (아리랑위성 5호의 GPS 전파 엄폐 자료처리시스템 개발을 위한 전리층 전자밀도 산출)

  • Lee, Woo-Kyoung;Chun, Jong-Kyun;Cho, Sung-Ki;Park, Jong-Uk;Cho, Jung-Ho;Yoon, Jae-Cheol;Lee, Jin-Ho;Chun, Yong-Sik;Lee, Sang-Ryul
    • Journal of Astronomy and Space Sciences
    • /
    • v.24 no.4
    • /
    • pp.297-308
    • /
    • 2007
  • The AOPOD (Atmosphere Occultation and Precision Orbit Determination) system, the secondary payload of KOMPSAT (KOrea Multi-Purpose SATellite)-5 scheduled to be launched in 2010, shall provide GPS radio occultation data. In this paper, we simulated the GPS radio occultation characteristic of KOMPSAT-5 and retrieved electron density profiles using KROPS (KASI Radio Occultation Processing Software). The electron density retrieved from CHAMP (CHAllenging Minisatellite Payload) GPS radio occultation data on June 20, 2004 was compared with IRI (International Reference Ionosphere) - 2001, PLP (Planar Langmuir Probe), and ionosonde measurements. When the result was compared with ionosonde measurements, the discrepancies were 5 km on the $F_2$ peak height ($hmF_2$) and $3{\times}10^{10}el/m^3$ on the electron density of the $F_2$ peak height ($NmF_2$). By comparing with the Laugmuir Probe measurements of CHAMP satellite (PLP), both agrees with $1.6{\times}10^{11}el/m^3$ at the height of 365.6 km.

Change Detection of Urban Development over Large Area using KOMPSAT Optical Imagery (KOMPSAT 광학영상을 이용한 광범위지역의 도시개발 변화탐지)

  • Han, Youkyung;Kim, Taeheon;Han, Soohee;Song, Jeongheon
    • Korean Journal of Remote Sensing
    • /
    • v.33 no.6_3
    • /
    • pp.1223-1232
    • /
    • 2017
  • This paper presents an approach to detect changes caused by urban development over a large area using KOMPSAT optical images. In order to minimize the radiometric dissimilarities between the images acquired at different times, we apply the grid-based rough radiometric correction as a preprocessing to detect changes in a large area. To improve the accuracy of the change detection results for urban development, we mask-out non-interest areas such as water and forest regions by the use of land-cover map provided by the Ministry of Environment. The Change Vector Analysis(CVA) technique is applied to detect changes caused by urban development. To confirm the effectiveness of the proposed approach, a total of three study sites from Sejong City is constructed by combining KOMPSAT-2 images acquired on May 2007 and May 2016 and a KOMPSAT-3 image acquired on March 2014. As a result of the change detection accuracy evaluation for the study site generated from the KOMPSAT-2 image acquired on May 2007 and the KOMPSAT-3 image acquired on March 2014, the overall accuracy of change detection was about 91.00%. It is demonstrated that the proposed method is able to effectively detect urban development changes in a large area.

The Construction and Development of Support System for Satellite image Commercialization (위성영상 상용화 지원시스템 구축 및 개발)

  • Bae, Hee-Jin;Jeon, Gab-Ho;Jun, Jung-Nam;Kim, Min-A;Chae, Tae-Byeong
    • Current Industrial and Technological Trends in Aerospace
    • /
    • v.8 no.1
    • /
    • pp.25-32
    • /
    • 2010
  • Utilization of KOMPSAT-2 satellite image is growing, because the resolution of KOMPSAT -2 is improved 43.5 times than that of KOMPSAT-1. To support for satellite image commercialization, KOCUST(KOMPSAT Customer & User Support Team) was composed, operation process was established and defined and support system for satellite image Commercialization was constructed. Also the support system constantly is improved for various user. In this paper, organization and function of support system developed so far these days for commercial user and operations related with it were described. In addition, direction of development was discussed

  • PDF